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International Association of Classification Societies (IACS) FSA of Bulk Carriers Fore-end Watertight Integrity Annex 4 Hatch Cover Failure Scenarios 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Table of Contents 1 SUMMARY 1 2 INTRODUCTION 4 2.1 Background 4 2.2 Objective 4 2.3 Scope 4 2.4 Overall approach of study 5 2.5 Description of base case design 6 3 HAZARDS RELATED TO HATCH COVERS AND COAMINGS 7 4 RISK CONTRIBUTION FROM HATCH COVER FAILURES 9 4.1 Casualty data 9 4.2 Overall risk contribution based on casualty data 9 4.3 Casualty data broken down on location of water ingress and severity 11 4.4 Risk contribution from No. 1 hatch covers on capesize bulk carriers 12 5 COST EFFECTIVENESS ANALYSIS OF RISK CONTROL OPTIONS 13 5.1 General remarks 5.1.1 Risk model 1.1.2 Cost effectiveness calculations 1.1.3 Assumptions 13 13 14 14 1.2 New-building requirements for hatch cover design pressure 15 1.3 RCO No. 1; Replacement of ILLC 66 hatch covers 17 1.4 RCO No. 2; Replacement of IACS UR S21 hatch covers 19 1.5 RCO No. 3 Hydraulic hatch cover closure 20 6 DISCUSSION 23 7 RECOMMENDATIONS 24 8 REFERENCES 24 APPENDIX 1 INFORMATION FROM MACGREGOR APPENDIX 2 BREAK-DOWN OF CASUALTY DATA 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 APPENDIX 3 HATCH COVER HAZARDS APPENDIX 4 LOADS HATCH COVERS EXPOSED TO GREEN SEA IMPACT APPENDIX 5 IACS UNIFIED REQUIREMENTS S21 APPENDIX 6 ANALYSIS OF HATCH COVER CAPACITY APPENDIX 7 ANALYSIS OF HATCH COVER RELIABILITY APPENDIX 8 MARGINAL COST EFFECTIVENESS 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 1 Hatch Cover Failure Scenarios 1 SUMMARY The present annex is a part of the IACS study Formal Safety Assessment of Bulk Carriers, Fore end watertight integrity. The objective of this annex is to evaluate, by Cost Effectiveness Analysis, risk control options aiming at preventing water ingress scenarios due to hatch cover failures on bulk carriers. In the present evaluation, a representative capesize bulk carrier was studied to quantify the effects and costs related to hatch cover risk control options. A capesize carrier was selected primarily because it was, based on experimental results (MSC72/4/1/Add.1, MSC 72/4/1), suspected that the design loads for these bulk carriers might be in the lower range. The scenarios considered in this annex consist of the following events: 1. Significant water ingress through an opening in No. 1 hatch cover. Given an opening of the size of a hatch cover, the cargo hold may be completely flooded within matter of minutes, see e.g. DETR (1998). 2. In some of the cases there are progressive flooding of cargo holds, leading to total loss of ship and in most cases many fatalities. 3. In the remaining cases, the flooding is limited, resulting in serious casualty and not total loss, and few, if any, fatalities. In addition to evaluating the marginal cost effectiveness for hatch cover design loads, the following risk control options were studied: 1. IACS UR S21 for hatch covers replacing ILLC 66 implemented on existing ships 2. Hatch covers designed to a 30% increase in IACS UR S21 design loads to replace IACS UR S21 hatch covers on existing ships. 3. Hydraulic hatch cover closure system for No. 1 hatch cover The cost effectiveness of the different risk control options have been assessed by their Gross and Net Costs of Averting a (statistical) Fatality (CAF), defined as: ∆C GrossCAF = ∆R ∆C − ∆B NetCAF = ∆R where ∆C is the total costs, ∆B is the economic benefits, and ∆R is the number of fatalities averted by the risk control option. MSC 72/16 recommends a decision criterion of US$ 3 million for risk control options involving reduction in both number of fatalities and injuries, and US$ 1.5 million for risk control options involving a reduction in number of fatalities only. The latter is likely to be the case for casualties related to hatch covers. Higher values may be justified for risks that are just tolerable, and MSC70/WP.12, paragraph 30, refer to criteria in the range from US$ 1 to 8 million. Table 1 gives the results for the different hatch cover risk control options studied. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Table 1 Hatch Cover Failure Scenarios 2 Cost Effectiveness results for hatch cover risk control options. RCO description IACS UR S21 hatch covers to replace ILLC 66 hatch covers on existing capesize carriers 10 year old ships 15 year old ships 20 year old ships Hatch covers designed to a 30% increase in IACS UR S21 design loads to replace IACS UR S21 hatch covers on existing ships. 10 year old ships 15 year old ships 20 year old ships Hydraulic hatch cover closure system on No. 1 hatch cover 10 year old ships 15 year old ships 20 year old ships New-buildings 30% increase in IACS UR S21 design loads for new ships ∆R ∆C (fatalities (US$) averted per ship) ∆B (US$) 5.16E-02 - 105,000 – 175,000 1.71E-01 3.44E-02 - 105,000 – 175,000 1.14E-01 1.72E-02 - 105,000 – 175,000 5.71E-02 Gross CAF Net CAF (US$ (US$ million) million) 27,700 92,000 22,400 74,300 13,821 45,800 0.6 - 3.4 0.1 - 3.2 0.9 - 5.1 0.3 - 4.9 1.8 - 10.2 1.0 - 9.9 2.00E-03 1.34E-03 6.68E-04 120,000 – 200,000 120,000 – 200,000 120,000 – 200,000 1,100 870 540 60 – 100 90 – 150 180 – 300 60 - 100 90 – 150 180 - 300 1.95E-02 1.30E-02 6.49E-03 1.46E-02 - 58,000 58,000 58,000 58,000 - 10,500 8,450 5,210 8,550 - 2.97 4.46 8.91 3.97 86 2.43 3.81 8.11 3.39 When evaluating the risk control options involving retrofitting existing bulk carriers with reinforced hatch covers, low cost estimates were used, not accounting for costs related to design, strengthening of support structure, and replacing wheels, rails, wheel lifters, fittings, and driving equipment. Colman (2000) described the cost of reinforcing No. 1 and 2 hatch covers on existing capesize bulk carriers as unlikely to exceed £150,000, or US$225,000, and as unlikely to exceed £100,000, or US$ 150,000, for new-buildings. This is in excess of the costs used in the present evaluation, and would make the Gross and Net CAF estimates higher. The evaluations do not give robust conclusions for the average bulk carriers with hatch covers designed according to ILLC 66. However, it is possible that the hatch cover capacity varies to such an extent that the replacement of hatch covers on a subset of the fleet could be justified. If a screening of the relevant bulk carriers could identify individual ships with particularly high hatch cover risks, then the replacement of their No. 1 and 2 hatch covers could be justified from a cost-effectiveness perspective. Risk control option No. 3 implying an hydraulic hatch cover closure system on No. 1 hatch cover for existing ships and new buildings has been evaluated to have a Gross and Net CAF in excess of the decision criterion. The casualty data indicates that the capesize carriers are more at risk for hatch cover failure than the smaller ships. A reason for this may be their lengths being comparable to the wave lengths in severe sea states, giving increased sea loads on the hatch covers and hence increased probability of water ingress. The handysize carriers appear to be more exposed than the handymax and panamax, probably due to lack of damage survivability. In many cases, the flooding of one cargo hold is sufficient for these ships to suffer from lack of buoyancy. The 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 3 panamax bulk carriers may have an order of magnitude lower frequency of total loss due to hatch cover failure compared to the average risk for bulk carriers. Given hatch cover strengthening of panamax, handysize, and handymax carriers, the relative risk reduction is expected to be similar to the risk reduction estimated for the capesize carriers. The absolute risk reduction is expected to be 50% or less for the smaller bulk carriers compared to the capesize carrier. The costs of strengthening hatch covers are also expected to be lower. Hence, the cost effectiveness for smaller bulk carriers is expected to be of the same order of magnitude as the cost effectiveness estimated for the capesize bulk carrier, giving similar recommendations. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 2 2.1 Hatch Cover Failure Scenarios 4 INTRODUCTION Background The present annex is a part of the IACS study Formal Safety Assessment of Bulk Carriers, fore end watertight integrity. Serious concerns have been expressed about the safety of bulk carriers for some time particularly following a spate of losses in the early 1990s. IMO prompted an international programme of research and development culminating in the 1997 SOLAS Conference on Bulk Carrier Safety. Revised rules and standards relating to the design and operation of bulk carriers were included in a new Chapter XII to the 1974 International Convention for the Safety of Life at Sea (SOLAS 74). These measures were rightly targeted at those vessels seen as being most at risk. However, concerns have been expressed that these safety improvements are piecemeal. The possibility of unidentified or not fully identified hazards in bulk carriers has been acknowledged. It has further been acknowledged that an overarching review of the many inter-related facets of bulk shipping safety is required to assist IMO in the development of the international regulatory framework. 2.2 Objective The objective of this annex is to evaluate, by Cost Effectiveness Analysis, risk control options aiming at preventing water ingress scenarios due to hatch cover failures on bulk carriers. 2.3 Scope The scenarios considered in this annex consist of the following events, see Figure 1: 1. Significant water ingress through a hatch cover opening. Given an opening of the size of a hatch cover, the cargo hold may be completely flooded within matter of minutes, see e.g. DETR (1998). 2. In some of the cases there are progressive flooding of cargo holds, leading to total loss of ship and in most cases fatalities. 3. In the remaining cases, the flooding is limited, resulting in serious casualty and not total loss, and few, if any, fatalities. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios Escalation ? YES 5 Total loss of ship Substantial water ingress in forepeak or No. 1 cargo hold NO Serious casualty OR Side shell failure Figure 1 Hatch cover failure Failure of deck fittings Scenario investigated in the present annex. In the present evaluation, a representative capesize bulk carrier was studied to quantify the effects and costs related to hatch cover risk control options. A capesize carrier was selected primarily because it was, based on experimental results, suspected that the design loads for these bulk carriers might be in the lower range. In addition to evaluating the marginal cost effectiveness for hatch cover design loads, the following risk control options were studied: 1. IACS UR S21 for hatch covers replacing ILLC 66 implemented on existing ships. 2. Hatch covers designed to a 30% increase in IACS UR S21 design loads to replace IACS UR S21 hatch covers on existing ships. 3. Hydraulic hatch cover closure system for No. 1 hatch cover. 2.4 Overall approach of study In order to be able to cover the totality of the complex problem to a sufficiently detailed level, the work was carried out by a multi-disciplinary team covering: • environmental loads, • hydrodynamics, • structural analysis, • structural reliability, • FSA. In order to be able to evaluate the risk control options, the analysis was divided into the following steps: • • • • • analysis of historical casualty data to establish an average annual probability of hatch cover failure and the consequences given hatch cover failure, see Section 4 analysis of environmental loads and dynamic response, in order to establish a realistic probability distribution for the loading for No. 1 hatch cover, see Appendix 4. formulation of hatch cover capacity, see Appendix 6 structural reliability analyses to estimate the probability of failure for each hatch cover design, see Appendix 7 cost effectiveness analyses, given different costs of the risk control options, different probabilities of failure, and hence different risk, see Section 5. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 6 The structural reliability analysis was carried out for three different hatch cover designs. The three designs were established by deterministic design analyses: 1. Initial design, according to ILLC 66. 2. Modified design, according to UR S21. 3. Modified design, according to UR S21, but with a 30% increase in load. The reliability analysis uses probabilistic models for both load and capacity. The probabilistic loading model is the same for all three designs. The design modifications are reflected in the distribution for the capacity. The relative difference in probability of failure for the three different designs is used as input to the cost effectiveness analysis. 2.5 Description of base case design A typical hatch cover configuration for the first cargo hold of a capesize bulk carrier has been selected as base case. The length of the hatch cover is 15.59m and the breadth is16.68m. The structural system of the hatch consists of a top plate with longitudinal L-stiffeners, transversal and longitudinal girders. Typical dimensions are: − Plate thickness, 8mm and 10mm near the centre − Stiffeners, L profile 100x75x7, spacing 550mm − Transversal girders, 7 in total, height approximately 850mm at centre and ends, 450mm in between. Typical web thickness of 7mm, with lower flange of 240x25mm2 and 100x15 mm2 for the large and small size girders respectively. Girder spacing 2700 mm. − Longitudinal girders around 850mm height, web thickness of 7mm and lower flange of 375x40 mm2 for the two most heavily loaded ones. Girder spacing 2750mm. A finite element plot of the hatch cover is included in Figure 2, seen from the side underneath. The green and red colours are used the surface plate of 8 mm and 10 mm thickness respectively. Blue colour is used for the webs of longitudinal and transversal girders, and yellow is used for the vertical surfaces that rest on the coaming. Please note that the lower flanges of the girders and the stiffeners (parallel to the main girders) are omitted in the figure. Ship particulars are included in Table 13. The base case design has been found to comply with the ILLC 66, where load and capacity can be summarised as: • Design load given by 1.75 ton/m2 . (This represents cargo loading rather than water pressure) • Stress criterion defined as the ultimate stress divided by 4.25. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 7 Figure 2 Finite element plot of hatch cover, seen from the side underneath (excluding lower flanges and stiffeners) 3 HAZARDS RELATED TO HATCH COVERS AND COAMINGS Different Hazard Identification studies have been conducted, and Table 12 in Appendix 3 lists the hazards related to hatch covers and coamings as collected by MCA (2000). The causes of water ingress and major contributors to the risk are represented in Figure 3. Substantial water ingress due to failure of hatch covers or coamings OR Failure in heavy weather due to wastage caused by lack of maintenance Figure 3 Hatch covers open due to rolling in heavy weather Failure due to severe sea loads caused by inappropriate heading and speed for sea condition Failure in heavy weather due to design compromise Causes of hatch cover failure giving substantial water ingress Wastage of hatch covers and coamings is easily detected by the crew, during classificatio n surveys, and in port state controls, and is assumed to be a minor contributor to the risk. In the LMIS database, 20 serious casualties were identified involving hatch cover failure and water ingress, see Appendix 2. In one of these cases, poor maintenance is indicated as a cause. Hence a rough estimate of the fraction of serious casualties due to hatch covers caused by “Failure in heavy weather due to wastage caused by lack of maintenance” is taken as 5%. 5 of the casualties found in 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 the LMIS casualty database included Annex 4 Hatch Cover Failure Scenarios 8 statements like “hatch cover lost”. 3 of these were also checked in Lloyd’s Casualty Archive. In one of these cases it was specified that No. 1 hatch cover was blown off by ferocious winds, and in another that the hatch cover was lost at sea. The event “Hatch cover opens due to rolling in heavy weather” is taken to include the cases where the hatch covers are lost at sea, including other causes than merely rolling in heavy weather. It is then estimated that approximately 25% of the hatch cover failures resulting in severe flooding is related to “Hatch cover opens due to rolling in heavy weather” in the above figure. The background for looking at risk control options related to hatch covers is the international discussion that have been going on regarding design loads for hatch covers, see e.g. MSC/72/4/1, and DETR (1998). “Inappropriate heading and speed for sea condition” may be a contributing factor to hatch cover failure in heavy weather. However, to investigate the hypothesis that the design loads for hatch covers are too low, the remaining 70% of the serious casualties involving flooding and hatch cover failure were assumed related to “Failure in heavy weather due to design compromise” in the above figure. The assumed relative importance of the causes to hatch cover failure given in the above figure hence is: • “Failure in heavy weather due to wastage caused by lack of maintenance” accounts for 5% of the serious casualties attributed to hatch cover failure • “Hatch covers open due to rolling in heavy weather” is taken to include all cases where hatch covers are lost to sea, also for other reasons than rolling, and is assumed to account for 25% of the serious casualties • “Failure due to severe sea loads caused by inappropriate heading and speed for sea condition” is taken as negligible • “Failure in heavy weather due to design compromise” is taken to include the cases of hatch cover collapse assumed to result from excessive green sea loads on the hatch covers. The remaining 70% of the cases are assumed attributed to this failure mode. Several other failure mechanisms exist for hatch covers and coamings, but these are expected to cause smaller openings, and less water ingress. This water ingress may be sufficient to jeopardise the cargo but do not pose immediate threats to safety. A brief summary of some of these failure modes is given in Appendix 3. The causes of progressive flooding is believed to be one of the following: • Failure of bulkhead separating a flooded and not flooded cargo hold • Failure of hull girder • Failure of hatch cover of not flooded cargo hold • Cargo liquefaction and loss of stability • Side shell failure of not flooded cargo hold The implementation of SOLAS XII will prevent progressive flooding due to failure of bulkheads between any cargo holds on new ships and between No. 1 and 2 cargo holds on existing ships. It is in the risk analysis below assumed that progressive flooding in the future will take place with the same probability as in the past. This is clearly conservative, and causes the risk contribution from hatch cover failure to be over estimated. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 4 4.1 Hatch Cover Failure Scenarios 9 RISK CONTRIBUTION FROM HATCH COVER FAILURES Casualty data In the LMIS casualty database, April 1999 version, 195 serious casualties including total losses involving water ingress have been found in the period from 1978 to 1998. The data foundation represents 73,600 ship years for bulk carriers of 20,000+ DWT. In addition, there are 27 cases where it is not clear whether the casualties involved water ingress or not. In 75 of these 195 water ingress cases, no detailed information has been found regarding the cause of the water ingress to the cargo holds, whereas some of these contain information about which cargo holds suffered from water ingress. 27 cases were found where failure of hatch covers and water ingress or possible water ingress was reported. 20 of the cases were recorded as serious casualties, of which 9 were total losses. 8 accidents involved in total 246 fatalities. 7 cases were recorded as non-serious casualties. 4.2 Overall risk contribution based on casualty data The Potential Loss of Life (PLL) is taken as the average number of fatalities per ship year. The contribution to PLL from hatch cover failures is estimated to: PLLhatch covers = n 246fatalities = = 3.34 ⋅ 10 −3 fatalities per ship year m 73,600 ship years In Annex 2, Table 9 gives a loss matrix for generic bulk carrier accidents. Here, a generic serious casualty is estimated to cost US$ 5,608,000, and a total loss US$ 24,808,000. Given 9 total losses due to hatch cover failures and 11 serious casualties not leading to total losses, the economic losses due to serious casualties and total losses due to failure of hatch covers is estimated as: ELhatch covers = f totalloss due to hatch covers ⋅ C totalloss + f seriouscasualtydue to hatch cover ⋅ Cseriouscasualty = 9 11 ⋅ 24,808,000 + ⋅ 5,608,000 = $3,900 per ship year 73,600 73,600 This constitutes a lower bound of the risk contribution from hatch cover failure, as only the cases where this is explicitly stated are included in the data. At the same time, the bound is also considered as a best estimate, since hatch cover failure is one of the failure mechanisms easier to detect and hence more likely to be reported. Assuming that all 75 cases found, where the source of water ingress was not accounted for, are related to hatch cover failure, an upper bound of the frequency of water ingress due to hatch cover failure is found. 37 of the casualties were total losses, and in total the casualties involved 522 fatalities. Upper bounds for the risk contribution from hatch covers hence are given as: PLLu hatch cover = 246 + 522 = 1.04 ⋅10 − 2 fatalities per ship year 73,600 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 10 The upper bound hence represents an increase of a factor of 3.1 in the annual fatality rate due to hatch cover failure. If cost estimates are combined with the frequencies for total loss and serious casualty, the economic losses due to serious casualties and total losses due to failure of hatch covers is estimated as: ELu hatch cover = 9 + 37 11 + 38 ⋅ 24,808,000 + ⋅ 5,608,000 = USD19,200 per ship year 73,600 73,600 The upper bounds may be used to evaluate the robustness of the recommendations for risk control options considering hatch covers and coamings. However, hatch cover failure is believed to be a failure mechanism relatively easy to detect, and the probability that this is reported is hence believed to be larger than e.g. the probability that side shell failure leading to water ingress being reported. The risk estimates based on the reported cases are thus taken as best estimates. Figure 4 and Figure 5 show the distribution of the number of total losses, serious casualties and fatalities on age of ship at the time of the casualty. When looking at the number of total losses and fatalities, there is no apparent and strong correlation with the ship age. When looking at the number of serious casualties, the age category from 15 to 19 years appear to be somewhat over-represented. These results are highly uncertain due to statistical uncertainty caused by the low number of events. Due to the limited data and the vague trends, ageing effects have not been considered in the present study of water ingress scenarios due to hatch cover failure, i.e. hatch cover risks have been assumed as constant over the ship lifetime. 9 Number of casualties 8 Number of serious casualties Number of total losses 7 6 5 4 3 2 1 0 0-4 5-9 10-14 15-19 20-24 > 25 Age of ship Figure 4 Number of serious casualties and total losses vs. the age of the ship at the time of the casualty. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 11 80 Number of fatalities 70 60 50 40 30 20 10 0 0-4 5-9 10-14 15-19 20-24 > 25 Age of ship Figure 5 casualty 4.3 Number of fatalities plotted against the age of the ship at the time of the Casualty data broken down on location of water ingress and severity In Appendix 2, casualty data has been evaluated in detail. The casualty data analysis, based on a limited amount of data, gave strong indications that the hatch cover of No. 1 cargo hold is the most troubled. The No. 1 hatch cover may be tied to 244 out of 246 fatalities, 9 total losses, and approximately 8 serious casualties. The risk contributions from the No. 1 hatch cover as deduced from historical data are: PLLhatch cover1 = ELhatch cover1 = 244 = 3.32 ⋅ 10 −3 fatalities per ship year 73,600 9 8 ⋅ 24,808,000 + ⋅ 5,608,000 = US $3,600 per ship year 73,600 73,600 The annual fleet average probability of No. 1 hatch cover failure causing serious casualty or total loss is estimated to: 0.77 ⋅ 20 p f , hatch cover 1 = = 2.09 ⋅ 10 − 4 73,600 Upper bounds for the risk contribution are achieved by assuming that all 75 casualties not accounted for are due to hatch cover failures, and that all of them are related to No. 1 cargo hold: 244 + 522 PLLu hatch cover 1 = = 1.04 ⋅ 10 − 2 fatalities per ship year 73,600 ELu hatch cover 1 = 9 + 37 8 + 38 ⋅ 24,808,000 + ⋅ 5,608,000 = US $19,000 per ship year 73,600 73,600 The upper bound for the annual fleet average probability of No. 1 hatch cover failure causing serious casualty or total loss is estimated to: 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios p u f , hatch cover 1 = 4.4 12 0.77 ⋅ (20 + 75) = 9.94 ⋅ 10 − 4 73,600 Risk contribution from No. 1 hatch covers on capesize bulk carriers The base risk contribution from severe hatch cover failures for capesize bulk carriers was estimated based on historical data and is summarised below. In the below table, the serious casualties (including total losses) are distributed on bulk carrier size. Table 2 Comparison of different bulk carrier size categories BC category Relative Number of serious Expected number of serious part of casualties and total casualties if equal underlying fleet losses frequency handysize 0.48 11 9.6 handymax 0.24 4 4.8 panamax 0.19 1 3.8 capesize 0.09 4 1.8 Ratio of observations per expected outcome 1 0.8 0.3 2 Based on this very limited data foundation, it is assumed that the capesize bulk carriers are more at risk than the other size categories, and that the frequency of serious casua lty (including total losses) is a factor of 2 higher than the average serious casualty frequency. The estimated average probability of No. 1 hatch cover failure causing serious casualty or total loss for capesize carriers, p capesize f , hatch cover1 , estimated according to: p capesize f , hatch cover1 = p f , hatch cover 1 ⋅ k capesize where p f , hatch cover 1 was above found to be 2.09 ⋅ 10 −4 as a lower bound and 9.94 ⋅ 10 −4 as an upper k capesize bound is a correction factor for capesize carriers found to be 2, see Table 2. Splitting the risk on causes as assumed in Section 3, gives the results shown in Table 3. Table 3 Hatch cover failure probabilities for capesize bulk carriers split on causes. Cause Failure in heavy weather due to wastage caused by lack of maintenance Hatch covers open due to rolling in heavy weather Failure due to severe sea loads caused by inappropriate heading and speed for sea condition Failure in heavy weather due to design compromise Relative contribution (%) Annual probability, lower bound Annual probability, upper bound 5 2.1 ⋅ 10 −5 1.0 ⋅ 10 −4 25 1.1 ⋅10 −4 5.0 ⋅ 10 −4 - - - 70 2.9 ⋅ 10 −4 1.4 ⋅10 − 3 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios Total 5 13 100 4.2 ⋅ 10 −4 2.0 ⋅ 10 −3 COST EFFECTIVENESS ANALYSIS OF RISK CONTROL OPTIONS 5.1 General remarks 5.1.1 Risk model A simple risk model is used to predict the effect of hatch cover risk control options, as shown in the following event tree. YES NO Casualty severity Number of fatalities per event Total loss of ship n TL Serious casualty nSC Escalation? pf Serious water ingress due to hatch cover failure PEsc 1 - PEsc Figure 6 Risk model used to estimate risk reduction The risk contribution, in terms of PLL, from hatch cover failure leading to serious water ingress hence is given by: PLL = p f ⋅ ( PEsc ⋅ nTL + (1 − PEsc ) ⋅ nSC ) fatalities per ship year where pf is the probability of hatch cover failure, PEsc is the probability of the event escalation to a total loss, nTL is the average number of fatalities per total loss, and nSC is the average number of fatalities per serious casualty. The annual probability of hatch cover collapse, pf, has been calculated by Structural Reliability Analysis (SRA) for different hatch cover designs. The analyses are documented in Appendix 7. Structural analyses, see Appendix 6, to establish a formulation of hatch cover strength, and hydrodynamic analyses, see Appendix 4, to establish a loading formulation, provided input to the SRA. All risk control options evaluated in the following are aimed at reducing the probability of failure of hatch covers. The risk reduction, ∆R, implied by a risk control option hence is taken as: ∆R = ∆PLL ⋅ TExp = ∆p f ⋅ (PEsc ⋅ (1 − rSOLASXII ) ⋅ nTL + (1 − PEsc ⋅ (1 − rSOLASXII )) ⋅ n SC ) ⋅ TExp per ship Here, TExp is the expected time interval when the risk control option is effective, and ∆pf is the reduction in probability of hatch cover failure due to the risk control option. rSOLASXII is the expected risk reduction due to the implementation of SOLAS Chapter XII and was in Annex 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 14 2 estimated to 22% for existing bulk carriers and 65% for new-buildings. The casualty data evaluation of Appendix 2 gives: PEsc = 0.5 given No. 1 cargo hold flooding nTL = 244 fatalities = 31.7 fatalities per total loss given No. 1 cargo hold flooding 0.5 ⋅ (20 ⋅ 0.77 ) total losses n SC = 0 fatalities per serious casualty (excluding total loss), given No. 1 cargo hold flooding The economic benefits, ∆B, from a risk control option is estimated according to: ∆B = ∑ ∆Bi (1 + r )n − 1 = ∆ B ⋅ i (1 + r )i r (1 + r ) n = ∆p f ( 1+ r) n − 1 ⋅ ( PEsc ⋅ (1 − rSOLASXII ) ⋅ CTL + (1 − PEsc ⋅ (1 − rSOLASXII )) ⋅ C SC ) ⋅ r (1 + r )n where ∆Bi, is the reduced economic losses due to serious casualties and total losses per ship year, r is the discount interest rate, representing a corporate rate of return taken as 10% in the calculations below. CTL and CSC are the estimated costs of a total loss and serious casualty respectively, as given in Table 9 of Annex 2. 5.1.2 Cost effectiveness calculations In the following evaluations, the Gross and Net Cost of Averting a Fatality (CAF) have been used. They are defined as: ∆C ∆R ∆C − ∆B NetCAF = ∆R GrossCAF = where ∆C is the total costs, ∆B is the economic benefits, and ∆R is the number of fatalities averted by the risk control option. Since the Gross CAF only compares the risk control option costs and the implied risk reduction in terms of fatalities averted, it clearly identifies the risk control options, which can be justified from a safety perspective alone. If an risk control option implies large economic benefits but has no safety implications, it would display a high Gross CAF. As the Net CAF also accounts for economic benefits, it may also be used to identify which risk control options are justifiable from a commercial point of view or combined commercial and safety point of view. 5.1.3 Assumptions 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 15 In the following, the different assumptions made during the risk control option evaluations are described. The base risk as obtained from casualty data is assumed representative for bulk carrier hatch covers designed according to the ILLC 66. This is based on the assumption that bulk carriers with hatch covers designed according to the ILLC 66 constitute the majority of the total population in the period from 1978 to 1998. The part of the fleet sailing with stronger hatch covers during the period is assessed to less than 10%. The Enhanced Survey Programme (ESP) is assumed not to affect the base risk contribution from hatch cover collapse (“Failure in heavy weather due to design compromise”) or from hatch covers being washed away (“Hatch covers open due to rolling in heavy weather”). The objective of part of the study was to investigate risk control options related to hatch cover strength. In order to evaluate these risk control options, the starting hypothesis was that a 70% of serious casualties involving hatch covers were related to hatch cover collapse due to buckling. This is a conservative assumption, since some of the casualties may be related to other failure modes giving slower flooding. This gives too high risks related to the collapse (due to buckling) failure mode. For new buildings, the difference in the costs of hatch covers is assumed to be a function of steel weight alone. The number of working hours and other production (e.g. welding bar, oxygen, scaffolding, etc) costs are assumed to remain the same independent of whether the design is a UR S21 or a ILLC 66 design. The costs of maintenance are also assumed to be equal. Hence the added costs of UR S21 is related to the extra steel weight alone. The cost model is given as: ∆C = ∆T ⋅ c1 where ∆C is the added cost due to strengthened hatch covers, ∆T is the added amount of steel, and c1 is the cost per metric tonne of steel, including welding. For existing ships it is assumed that the hatch covers simply are replaced with strengthened hatch covers. The operation is assumed to take place during survey and hence does not imply extra off hire. The total costs thus are assumed equal to the costs of the new hatch covers, taken as the total steel weight of the hatch covers, T, multiplied by an average cost per tonne steel, c2 , including work, welding bar, oxygen, scaffolding etc: ∆C = T ⋅ c2 The life expectancy of an average bulk carrier is in the following taken as 25 years. 5.2 New-building requirements for hatch cover design pressure In order to estimate the marginal cost effectiveness of different design pressure levels for hatch cover, hatch cover costs, as achieved from the bulk carrier department of MacGregor (see Appendix 1), and annual probabilities of hatch cover collapse were used. Details are given in Appendix 8. The structural reliability results and cost data have been used to establish linear regression models for annual probability of hatch cover failure and hatch cover costs, as functions of the design pressure. Based on these, the marginal cost 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 16 effectiveness has been estimated as a function of the design pressure. 1.00E+08 IACS UR S21 Gross CAF (USD) 1.00E+07 1.00E+06 1.00E+05 1.00E+04 1.00E+03 Gross CAF 1.00E+02 Criterion 1.00E+01 1.00E+00 0 20 40 60 80 100 Hatch cover strength (kN/m2) Figure 7 Marginal Gross CAF as a function of hatch cover strength, prior to the implementation of SOLAS Chapter XII. The results are applicable for changes in new-building requirements at the time of the implementation of IACS UR S21, which shows that IACS UR S21 from a cost effectiveness perspective seems to be close to optimal. To evaluate an increase in the design loads today, the effect of SOLAS Chapter XII has to be incorporated, which has been done in Figure 8. 1.00E+09 Gross CAF (US$) 1.00E+08 UR S21 1.00E+07 Gross CAF 1.00E+06 Criterion UR S21+30% 1.00E+05 1.00E+04 1.00E+03 1.00E+02 1.00E+01 1.00E+00 0 20 40 60 80 100 Hatch cover strength (kN/m2) Figure 8 Marginal Gross CAF as a function of design pressure, given the implementation of SOLAS Chapter XII. Presently, an increase in the design loads and hence the strength of hatch covers of e.g. 30% is estimated to imply a Gross CAF of US$86 million, by far exceeding the recommended decision criterion. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 5.3 Hatch Cover Failure Scenarios 17 RCO No. 1; Replacement of ILLC 66 hatch covers Risk control option No. 1 implies replacing No. 1 and 2 hatch covers designed according to ILLC 66 with hatch covers designed according to IACS UR S21. Table 4 refers the estimated annual probabilities of hatch cover collapse as estimated by SRA, see Appendix 7. Table 4 Annual probabilities of hatch cover collapse. (For SRA estimates, see Appendix 7) Case Initial design, ILLC 66 UR S21 Probability of hatch cover collapse, estimated by SRA 9.35⋅10-4 1.16⋅10-5 Probability of hatch cover collapse, estimated from casualty data 2.9⋅10-4 - 1.4⋅10-3 - Note that the estimated annual probability of hatch cover collapse for the ILLC 66 design (9.35⋅10-4 ) is high compared to the estimates based on the casualty data (2.9⋅10-4 - 1.4⋅10-3 ), of which the lower bound is assessed to be the closest to the true hatch cover collapse probability. The relatively high SRA estimate may e.g. be due to: • uncertainty in the hatch cover loading model • the assumption about a uniform pressure level on the hatch cover • the weather routing in the data period being more effective than the weather routing during the time period when wave data was collected • the world-wide wave data not being representative for the typical capesize bulk carrier trades. In the calculations below, the lower probability of ha tch cover collapse as estimated from casualty data have been used to generate the lower limit for the risk reduction. The estimated annual probability of hatch cover collapse from SRA has been used to generate an upper limit for the risk reduction. To establish the lower estimate for the risk reduction and economic benefits, the difference between the lower estimate for the annual failure probability for the ILLC 66 design and the SRA estimate for the IACS UR S21 design is utilised: ∆p l f = 2.9 ⋅ 10 −4 − 1.15 ⋅10 − 5 = 2.8 ⋅ 10 −4 The lower bound for the number of fatalities averted per ship year by the measure compared to IACS UR S21 is estimated according to: ∆R l = ∆p l f ⋅ (PEsc (1 − rSOLASXII ) ⋅ nTL + (1 − PEsc (1 − rSOLASXII )) ⋅ n SC ) ⋅ TExp = 2.8 ⋅ 10 − 4 ⋅ (0.5 ⋅ (1 − 0.26 ) ⋅ 31.7 + 0 ) ⋅ TExp = 3.4 ⋅ 10 − 3 ⋅ TExp The lower bound for the economic benefits are estimated to: 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 ∆B = ∆p l Hatch Cover Failure Scenarios l f 18 n ( 1+ r) −1 ⋅ (PEsc ⋅ (1 − rSOLASXII ) ⋅ CTL + (1 − PEsc (1 − rSOLASXII )) ⋅ C SC ) ⋅ n r (1 + r ) = 2.8 ⋅ 10 - 4 ⋅ (0.5 ⋅ (1 − 0.22) ⋅ US$24,808,000 + (1 − 0.5(1 − 0.22 )) ⋅ US$5,608,000 ) ⋅ 1.1 Exp − 1 T 0.1 ⋅ 1.1 Exp T 1.1 Exp − 1 0.1 ⋅1.1TExp T = US $3,600 ⋅ Similarly, the upper estimates for the risk reduction and economic benefits are estimated from the difference in the annual failure probabilities as estimated from the SRA: ∆p u f = 9.35 ⋅ 10 −4 − 1.15 ⋅10 − 5 = 9.2 ⋅ 10 −4 The upper bound for the number of fatalities averted per ship year by the measure compared to IACS UR S21 is estimated according to: ∆R u = ∆p u f ⋅ (PEsc (1 − rSOLASXII ) ⋅ nTL + (1 − PEsc (1 − rSOLASXII )) ⋅ nSC ) ⋅ TExp = 9.2 ⋅ 10 − 4 ⋅ (0.5 ⋅ (1 − 0.26) ⋅ 31.7 + 0 ) ⋅ TExp = 1.1 ⋅10 −2 ⋅ TExp The upper bound for the economic benefits are estimated to: ∆B u = ∆p u f ⋅ (PEsc ⋅ (1 − rSOLASXII ) ⋅ CTL + (1 − PEsc (1 − rSOLASXII )) ⋅ C SC ) ⋅ (1 + r )n − 1 n r (1 + r ) = 9.2 ⋅ 10 ⋅ (0.5 ⋅ (1 − 0.22 ) ⋅ US $24,808,000 + (1 − 0.5(1 − 0.22)) ⋅ US $5,608,000 ) ⋅ -4 1.1 Exp − 1 T 0.1 ⋅1.1 TExp 1.1 Exp − 1 = US $12,100 ⋅ 0.1 ⋅1.1TExp T A cost per metric tonne steel in the range of US$1,500 to US$2,500 as suggested by MacGregor, see Appendix 1, is used to estimate the risk control option cost. MacGregor also indicated that hatch covers No. 1 and 2 designed according to UR S21 would weigh approximately 35 tonnes each. A lower and upper cost estimate hence is given by: ∆Clower = T ⋅ c 2 = 2 ⋅ 35tonnes ⋅ US $1,500 / tonne = US $105,000 ∆Cupper = T ⋅ c2 = 2 ⋅ 35tonnes ⋅ US $2,500 / tonne = US $175,000 Even the highest cost estimate may be in the lower range, as costs related to design, spare parts, operating equipment, transport and strengthening of the coaming etc, are excluded. The risk control option Gross and Net CAFs, which depend on the age of the ship at the time of implementation, are shown in the Table below. Table 5 Cost effectiveness results for exchanging LLC hatch covers with IACS UR S21 hatch covers 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios Age of ship at ∆ R time of (per ship) implementation ∆C (US$) 19 ∆B (US$) 10 years 5.16E-02 - 1.71E-01 105,000 - 175,000 27,700 - 92,000 15 years 3.44E-02 - 1.14E-01 105,000 - 175,000 22,400 - 74,300 20 years 1.72E-02 - 5.71E-02 105,000 - 175,000 13,821 - 45,800 Gross CAF (US$ million) 0.6 - 3.4 0.9 - 5.1 1.8 - 10.2 Net CAF (US$ million) 0.1 - 3.2 0.3 - 4.9 1.0 - 9.9 The above results indicate that the uncertainties in the results are large, and that no firm conclusions can be drawn for whether ILLC 66 hatch covers on existing bulk carriers should be replaced or not. However, the higher values are assessed to be the more realistic. Colman (2000) describes the cost of reinforcing No. 1 and 2 hatch covers on existing capesize bulk carriers as unlikely to exceed £150,000, or US$225,000. This is in excess of the costs used in the present evaluation, and would make all the Gross and Net CAF estimates become higher. 5.4 RCO No. 2; Replacement of IACS UR S21 hatch covers Risk control option No. 2 implies replacing No. 1 and 2 hatch covers designed according to IACS UR S21 with hatch covers designed to withstand a 30% increase in the design loads of IACS UR S21. Table 6 gives the estimated annual probabilities of hatch cover collapse for the relevant designs, as estimated by SRA, see Table 22 of Appendix 7. Table 6 Annual probabilities of hatch cover collapse, as estimated by SRA Case UR S21 30% increase in UR S21 design loads Probability of hatch cover collapse, pf 1.16⋅⋅10 -5 7.85⋅⋅10 -7 The relative difference in annual failure probability between the IACS UR S21 design and the design involving 30% increase in UR S21 design loads is estimated to: ∆p f = 1.15 ⋅ 10 −5 − 7.85 ⋅10 −6 = 1.07 ⋅ 10 −5 The number of fatalities averted per ship year by the measure compared to IACS UR S21 is estimated according to: ∆R = ∆p f ⋅ ( PEsc (1 − rSOLASXII ) ⋅ nTL + (1 − PEsc (1 − rSOLASXII )) ⋅ n SC ) ⋅ TExp = 1.07 ⋅ 10 −5 ⋅ (0.5 ⋅ (1 − 0.26 ) ⋅ 31.7 + 0 ) ⋅ TExp = 1.3 ⋅10 −4 ⋅ TExp The economic benefits are estimated to: 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 ∆B = ∆p f Hatch Cover Failure Scenarios 20 n ( 1 + r ) −1 ⋅ ( PEsc ⋅ (1 − rSOLASXII ) ⋅ CTL + (1 − PEsc (1 − rSOLASXII )) ⋅ CSC ) ⋅ n r (1 + r ) = 1.97 ⋅ 10 -5 ⋅ (0.5 ⋅ (1 − 0.22 ) ⋅ US $24,808,000 + (1 − 0.5(1 − 0.22)) ⋅ US $5,608,000) ⋅ 1.1 Exp − 1 T 0.1 ⋅ 1.1 TExp 1.1 Exp − 1 0.1 ⋅1.1TExp T = US $140 ⋅ Upper and lower bounds for the risk control option cost are: ∆Clower = T ⋅ c 2 = (2 ⋅ 40tonnes )US$1,500 / tonne = US $120,000 ∆Cupper = T ⋅ c 2 = (2 ⋅ 40tonnes )US $2,500 / tonne = US $200,000 The resulting Gross and Net CAFs are shown in the table below. Table 7 Cost effectiveness results for replacing IACS UR S21 hatch covers with hatch covers designed to 30% increase in IACS UR S21 loads Age of ship at time ∆ R of i mplementation (per ship) 10 years 15 years 20 years 2.00E-03 1.34E-03 6.68E-04 ∆C (US$) ∆B (US$) 120,000 - 200,000 120,000 - 200,000 120,000 - 200,000 Gross CAF (US$ million) 1,100 870 540 60 - 100 90 - 150 180 – 300 Net CAF (US$ million) 60 – 100 90 – 150 180 - 300 In the above table, it is indicated it is not cost effective to exchange No. 1 and 2 hatch covers on capesize carriers designed according to IACS UR S21 with new hatch covers designed according to a 30% increase in the IACS UR S21 design loads. The cost estimates used are also lower bounds of the true costs, giving a robust recommendation that IACS UR S21 hatch covers should not be exchanged on existing ships. Colman (2000) describes the cost of reinforcing No. 1 and 2 hatch covers on existing capesize bulk carriers as unlikely to exceed £150,000, or US$225,000. This is in excess of the costs used in the present evaluation, and would make the Gross and Net CAF estimates higher. 5.5 RCO No. 3 Hydraulic hatch cover closure Risk control option No. 3 implies fitting No. 1 cargo hold with a hydraulic hatch cover closure system. In Table 3, the annual probability of the failure mode “hatch cover No. 1 being washed overboard, or opening due to extensive rolling” was estimated to: p f = 1.05 ⋅ 10 −4 Assuming that hydraulic 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 hatch cover closure system on No. 1 Annex 4 Hatch Cover Failure Scenarios 21 hatch cover only is able to prevent all such failures from happening, the risk reduction over the remaining lifetime of an existing bulk carrier is estimated to: ∆R = ∆p f ⋅ ( PEsc (1 − rSOLASXII ) ⋅ nTL + (1 − PEsc (1 − rSOLASXII )) ⋅ n SC ) ⋅ TExp = 1.05 ⋅10 − 4 ⋅ (0.5 ⋅ (1 − 0.22 ) ⋅ 31.7 + 0 ) ⋅ TExp = 1.3 ⋅10 −3 ⋅ TExp The economic benefits are estimated to: ∆B = ∆p f n ( 1+ r) −1 ⋅ ( PEsc ⋅ (1 − rSOLASXII ) ⋅ CTL + (1 − PEsc (1 − rSOLASXII )) ⋅ C SC ) ⋅ n r (1 + r ) = 1.05 ⋅10 - 4 ⋅ (0.5 ⋅ (1 − 0.22 ) ⋅ US $24,808,000 + (1 − 0.5(1 − 0.22)) ⋅ US $5,608,000 ) ⋅ 1.1 Exp − 1 T 0.1 ⋅1.1 TExp 1.1 Exp − 1 = US $1,380 ⋅ 0.1 ⋅ 1.1TExp T For bulk carrier new-buildings, the risk reduction from SOLAS Chapter XII was estimated to 65%, giving: ∆R = ∆p f ⋅ ( PEsc (1 − rSOLASXII ) ⋅ nTL + (1 − PEsc (1 − rSOLASXII )) ⋅ n SC ) ⋅ TExp = 2.61 ⋅ 10 − 4 ⋅ (0.5 ⋅ (1 − 0.65) ⋅ 31.7 + 0) ⋅ 25 = 1.46 ⋅10 −2 fatalities averted The economic benefits are estimated to: ∆B = ∆p f n ( 1 + r) − 1 ⋅ ( PEsc ⋅ (1 − rSOLASXII ) ⋅ CTL + (1 − PEsc (1 − rSOLASXII )) ⋅ CSC ) ⋅ n r (1 + r ) = 2.84 ⋅10 ⋅ (0.5 ⋅ (1 − 0.65) ⋅ US$24,808,000 + (1 − 0.5(1 − 0.65)) ⋅ US $5,608,000 ) ⋅ -4 1.1 Exp − 1 T 0.1 ⋅1.1 TExp 1.1 Exp − 1 = US $940 ⋅ 0.1 ⋅ 1.1T Exp T A gross estimation of a hydraulic securing system for hatch covers envisages eight hydraulic pistons per hatch. Assuming the modification is made on a single hatch, the additional mechanical equipment, hydraulic piping, dedicated hydraulic unit and signalling system amounts to about US$ 24,000, not including the additional inspections during the periodical hatch cover surveys. In general, the maintenance costs of such systems may be significant, and these systems are also regarded as less flexible than quick-acting cleats, which are generally chosen. Assuming that the maintenance costs add up to 10% of the new-building cost per year, the cost of this risk control option is estimated to: 25 US $2,400 = US $58,000 1.05i i =1 ∆C = US $24,000 + ∑ In Table 8, the Gross and Net CAF for implementing hydraulic hatch cover closure on new and existing bulk carriers have been estimated. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 22 Table 8 Cost effectiveness results for introducing hydraulic hatch cover closure systems on No. 1 hatch cover Age of ship at time of ∆ pf implementation 10 year old ships 15 year old ships 20 year old ships New-buildings 1.05E-04 1.05E-04 1.05E-04 1.05E-04 ∆R ∆C (per ship) (US$) 1.95E-02 1.30E-02 6.49E-03 1.46E-02 ∆B (US$) 58,000 58,000 58,000 58,000 10,500 8,450 5,210 8,550 Gross CAF (US$ million) 2.97 4.46 8.91 3.97 Net CAF (US$ million) 2.43 3.81 8.11 3.39 If hydraulic hatch cover closure systems are implemented on several hatch covers, costs of order of magnitude US$ 100,000 are anticipated, excluding maintenance costs. The risk reduction would not increase accordingly since the majority of the fatalities are related to failure of No. 1 hatch cover. Hence, fitting all cargo holds with hydraulic hatch cover closure systems is expected to have Gross and Net CAFs by far exceeding the recommended decision criterion. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 6 Hatch Cover Failure Scenarios 23 DISCUSSION MSC 72/16 recommended a decision criterion of US$ 3 million for risk control options involving reduction in both fatalities and injuries and US$ 1.5 million for risk control options involving a reduction in fatalities only. The latter is likely to be the case for casualties related to hatch covers. The marginal Gross and Net CAF evaluation of hatch cover design load levels indicated that the IACS UR S21 design load levels are close to optimal compared to the recommended decision criterion of MSC 72/16. When evaluating the risk control options involving retrofitting existing bulk carriers with reinforced hatch covers, low cost estimates were used, not accounting for costs related to design, strengthening of support structure, and replacing wheels, rails, wheel lifters, fittings, and driving equipment. Colman (2000) described the cost of reinforcing No. 1 and 2 hatch covers on existing capesize bulk carriers as unlikely to exceed £150,000, or US$225,000, and as unlikely to exceed £100,000, or US$ 150,000, for new-buildings. This is in excess of the costs used in the present evaluation, and would make the Gross and Net CAF estimates higher. The estimated risk reductions are optimistic due to the assumptions that 70% of the serious casualties and total losses were caused by hatch cover collapse. In reality, some of them may have been caused by smaller leaks over a longer period of time, for which other risk control options than presently studied would have been relevant. Due to the costs being under-estimated and the risk reductions over-estimated, the risk control options of replacing hatch covers on existing ships tend to look more cost-effective than they actually are. Even under these assumptions, the evaluations do not give robust conclusions for whether the ILLC 66 hatch covers should be replaced on the average bulk carriers. However, it is possible that the hatch cover capacity varies to such an extent that the replacement of hatch covers on a subset of the fleet could be justified. If a screening of the relevant bulk carriers could identify individual ships with particularly high hatch cover risks, then the replacement of their No. 1 and 2 hatch covers could be justified from a cost-effectiveness perspective. The uncertainties in the results are considerable, for several reasons. The base case risk level was based on the assumption that the historical risk level was applicable for ILLC 66 hatch cover designs, whereas parts of the bulk carrier fleet have had hatch covers designed to stricter standards by individual class societies 1 . However, throughout the period from 1978 to 1998, less than 10% of the fleet is believed to have had stronger hatch covers. The statistical data is open to interpretation, and risk intervals were based on casualties reported as related to hatch covers and the SRA results. In addition, casualties have occurred for which little information is available, e.g. 6 total losses recorded as “missing”. If assigning all casualties with insufficient information available to the flooding scenarios due to hatch cover failure, the risks were estimated as a factor 3 above what is presently used. Under such assumptions, it would be cost-effective to replace ILLC 66 hatch covers. Risk control option No. 3 implying an hydraulic hatch cover closure system on No. 1 hatch cover was also found to display Gross and Net CAFs exceeding the recommended decision criterion. 1 DNV has had stricter requirements for hatch covers since the early 1970s. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 24 In the present evaluation, a representative capesize bulk carrier was selected, primarily because based on experimental test results it was suspected that the design loads for these bulk carriers were in the lower range. The casualty data indicates that the capesize carriers are more at risk for hatch cover failure than the smaller ships. A reason for this may be their lengths being comparable to the wave lengths in severe sea states, giving increased sea loads on the hatch covers and hence increased probability of water ingress. The handys ize carriers appear to be more exposed than the handymax and panamax, probably due to lack of damage survivability. In many cases, the flooding of one cargo hold is sufficient for these ships to suffer from lack of buoyancy. The panamax bulk carriers may have an order of magnitude lower frequency of total loss due to hatch cover failure compared to the average risk for bulk carriers. Given hatch cover strengthening of panamax, handysize, and handymax carriers, the relative risk reduction is expected to be similar to the risk reduction estimated for the capesize carriers. The absolute risk reduction is expected to be 50% or less for the smaller bulk carriers compared to the capesize carrier. The costs of strengthening hatch covers are also expected to be lower. Hence, the cost effectiveness for smaller bulk carriers is expected to be of the same order of magnitude as the cost effectiveness estimated for the capesize bulk carrier, giving similar recommendations. 7 RECOMMENDATIONS No risk control options related to flooding scenarios caused by hatch cover failure were identified, which were associated to Gross and Net CAFs clearly below the decision criterion as recommended in MSC72/16. Regarding the risk control option involving the replacement of ILLC 66 hatch covers, the Gross and Net CAF intervals are wide, reflecting considerable uncertainties. Hence no firm conclusion can be given for the implementation of this risk control option. However, it is possible that the variation in hatch cover capacity of ILLC 66 design is so large that the replacement of hatch covers on a subset of the fleet could be justified. If a screening of the relevant bulk carriers could identify individual ships with particularly high hatch cover risks, then the replacement of their No. 1 and 2 hatch covers could be justified from a cost-effectiveness perspective. Other alternative risk control options may also exist, like only replacing No. 1 hatch cover, and not both No. 1 and 2. Hence, it is recommended that such a risk control options be evaluated further. This study has assessed IACS UR S21 hatch cover designs to be significantly more reliable than ILLC 66 hatch cover designs with respect to hatch cover collapse caused by green seas on deck. The cost effectiveness assessment indicated that the design loads of IACS UR S21 are close to optimal. At present, IACS model tests are being carried out, increasing the knowledge about green loads on deck. When obtained, new information about hatch cover loading is recommended be included in UR S21, but as the requirements seem to have close to an optimal level of reliability, this is recommended be maintained. This would mean that the increased knowledge, when implemented in UR S21, would give less uncertainty and probably less variability between UR S21 hatch cover designs. 8 REFERENCES Bitner-Gregersen, E. M., 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 “Environmental Description for Annex 4 Hatch Cover Failure Scenarios 25 Long-Term Load Response of Ship Structures”, DVN Research Report No.: 94-2054, Rev. No. 1, 1995. Colman, The Honourable Mr. Justice Colman (2000), “Report of the re-opened formal investigation into the los of the MV Derbyshire”. In the High Court of Justice (Admirality Court). November, 2000. DETR (1998), “M.V. Derbyshire Surveys, UK/EC Assessors’ Report, A summary”, Department of the Environment, Transport and the Regions, UK, March 1998. DNV (1992), “PROBAN – General Purpose Probabilistic Analysis Program, Theory Manual,” Det Norske Veritas, report No. 92-7049. rev. No.01, Høvik. DNV (1994), “Wadam, Wave Loading by Diffraction and Morrison Theory”, User’s Manual, DNV Report No. 94-7100, December 1994. DNV (1995a), POSTRESP, Interactive Postprocessor for General Response Analysis, User’s Manual, DNV Report No. 95-7014, August 1995. DNV (1995b), DNV Classification Note 30.1, “Buckling Strength Analysis”, July 1995. Faulkner, D., Corlett, B. J., Romeling, J. U. (1996): “Design of hatch covers and coamings for abnormal waves”, the international conference on " Watertight Integrity and Ship Survivability" organised by the Royal Institute of Naval Architects (RINA) in London 21-22 November 1996. DNV (1997), “SWAN-2 Theory and Numerical methods”, DNV Research report No. 942030, revision 1, 18th of April 1997. DNV (1998), DNV Classification Note 30.7, “Fatigue Assessment of ship Structures”, September 1998. IACS (1997) “Evaluation of Scantlings of Hatch Covers of Bulk Carrier Cargo Holds”, IACS Requirements 1997, Volume 1, S21. International Conference on Load Lines (1966), “Final Act of the conference with attachments including the International Convention on Load Lines, 1966”, IMO London, 1981. MCA (2000), Hazard identification as circulated by MCA on 25 April 2000 (IACS message 0032_IAe). MSC 70/4, “Sensitivity of wetness and deck loads to bow height and forward buoyancy reserves in extreme weather conditions”, submitted by the United Kingdom. MSC 70/4/6, “Operational measures for avoiding dangerous situations in extreme weather conditions”, submitted by Greece. MSC 72/4/1 “Green sea loads on hatch covers and deck wetness derived from seakeeping model tests on a range of bulk carriers”, submitted by the United Kingdom. MSC 72/4/1/Add. 1: “Further green sea loads results of seakeeping model tests on a range of 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 26 bulk carriers”, submitted by the United Kingdom. MSC 72/16, “Decision Parameters including Risk Acceptance Criteria”, submitted by Norway. Nestegård, A., Krokstad, J.R. (2000), “Non- linear wave loading”, DNV Report No. 20003401, Høvik, 2000. Skjong, R., Bitner-Gregersen, E., Cramer, E., Croker, A., Hagen, Ø., Korneliussen, G., Lacasse, S., Lotsberg, I., Nadim, F., Ronold, K.O. (1996), “Guideline for Offshore Structural Reliability Analysis – General”. Det Norske Veritas Research Report No. 95-2018. DNV, Høvik, Norway. Østvold, T. K., Steen, E. (2001), “Non- linear finite element analyses of hatch covers”, DNV Report No. 2001-0391, DNV, Høvik, Norway. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 27 Appendix 1 Information from MacGregor regarding hatch cover costs, email of 8 October 2000. Dear Ms. Eknes, Thank you for involving us and giving us the opportunity to comment on your study. Both the LLC and UR S21 are everyday issues for us and those are easy to comment upon, but the new 40 % higher load seems quite a big challenge. We have no information of hatch cover failures for ships where the UR S21 is already considered. There might be reasons to increase the load, but this issue is not for us to comment upon. You do not explain which stress levels are considered for the 40 % higher loads so any estimates from our side is pure guess-work. You have only mentioned the load influences on Hatch 1. For most cape size bulk carriers also Hatch 2, being within the forward 25 % of the ship, is also subject to increased loads. However not of the same magnitude, but the corrosion additions applies here in the same way as for Hatch 1. The UR S21 loads are typically: for Hatch 1 6-6,5 t/m2 for Hatch 2 4-4,5 t/m2 Typical steel weights for an open web structure (square metre weights calculated on the area of top plate) are: Hatch cover 1, according to LLC only 185 kg/m2 Hatch cover 1, according to UR S21 270 kg/m2 Hatch cover 2, according to LLC only Hatch cover 2, according to UR S21 180 kg/m2 220 kg/m2 We have assumed that H.1 would be 15 x 17 m and H.2 would be 15 x 20 m. The corresponding panel weights would be: Hatch cover 1, according to LLC only 24 tonnes (net, without fittings) Hatch cover 1, according to UR S21 35 tonnes (net, without fittings) Hatch cover 2, according to LLC only 28 tonnes (net, without fittings) Hatch cover 2, according to UR S21 35 tonnes (net, without fittings) The average corrosion addition (included in the above weights) is some 17 % for an open web structure, slightly higher for a double skin structure. The fittings weight (within the normal load range) is some 10 % of the steel structure weight. A 40 % higher load would mean approximately a 10-15 % addition to above (UR S21) weights. As you can see from the above, the weight increase can be considerable and this would mean, that also the fittings and drive equipment would be bigger. Thus the size of wheels, rails, wheel lifters, hydraulic motors, support pads, guides and wedges would need to be increased. If we wish to keep the operation times the same, hydraulic pump unit and the hull piping should also be bigger. Today we try to harmonise the fitting range by using a higher amount of high tensile steel for the forward hatch covers in order to save weight. Thus we are able in most cases to use for instance hydraulic motors of one size throughout the whole vessel. We doubt this would be possible for an increased load giving the shipowner an additional range of fittings and thus an increased spare parts handling cost. For side rolling hatch covers to a newbuilding, the fabrication cost 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Hatch Cover Failure Scenarios 28 is in the magnitude of 1.200-2.000 US$/tonne, depending on where the hatch covers are produced (Asia-Europe). We have not even tried to estimate these costs for the bigger fittings, but the cost could be considerable. The cost for existing ships follows the above, but you need to consider, that in most cases the existing fittings cannot be reused. It is also doubtful, that the coamings are sufficiently strong. Have you considered the higher transversal forces due to increased vertical loads? There might also be a need to increase the size of transversal stoppers to such a magnitude, that today’s standard solutions cannot be used, requiring even a completely new hatch cover system. The cost for the steel structure when replacing one hatch for an existing ship would be approximately 1.500-2.500 US$/tonne, excluding design, spare parts, operating equipment, transport and strengthening of the coaming, of course depending on where the hatch covers are produced (Asia-Europe), and depending on the delivery time. We do not believe it feasible to strengthen existing hatch covers as most of the top plate should be renewed due to the stresses and due to buckling. We do hope the above clarifies the situation. Should you have any further queries, please do not hesitate to contact us again. We would be very interested in following the development of your studies. If a report would be published, please send one also to us. Best regards MacGREGOR (FIN) Oy Hatch Covers Torbjörn Dahl Senior Naval Architect, Bulk Ships Hallimestarinkatu 6 FIN-20780 KAARINA, Finland Telephone: +358-2-4121 313 Mobile phone: +358-40-524 4601 Fax: +358-2-4121 508 E-Mail: torbjorn.dahl@macgregor-group.com 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 Annex 4 Appendix 2 Hatch Cover Failure Scenarios 29 Break-down of Casualty Data Below the hatch cover casualty data are further investigated, in order detect trends and to attribute the casualties to different circumstances. The tree below illustrates the breakdown of 20 serious casualties on water ingress location, total losses, and fatal accidents. When trying to quantify the different branches of the tree, in many cases there are only 1 or perhaps 0 observations. This is of course not sufficient to make any reliable estimates for the different branch probabilities. The results from the tree is mainly used to estimate the risk contribution from No. 1 and 2 hatch covers, and this is also the branches to which the majority of the cases relate. Frequency Failure of at least no. 1 hatch cover P1 Loss of ship P4 Serious casualty P5 Flooding due to hatch cover failure Failure of at least no. 2 hatch cover, but not no.1 hatch cover P2 Loss of ship P6 P3 Fatalities P12 No fatalities P13 Fatalities P14 No fatalities P15 Fatalities P16 P7 No fatalities P17 Fatalities P18 No fatalities P19 Serious casualty P9 Figure 9 No fatalities P11 Serious casualty Loss of ship P8 Failure of any other hatch cover, and not n.1or n.2 hatch cover Fatalities P10 Fatalities P20 No fatalities P21 Breakdown of casualties on location of failed hatch cover, and consequences of casualty. Frequency of flooding due to hatch cover failure In the LMIS casualty database, for bulk carriers of 20,000 DWT and larger, 20 cases were found involving failure of hatch cover and water ingress. In 19 of the cases, water ingress was reported, while one case probably involved water ingress although not specified. An estimate of the frequency of serious casualty involving water ingress due to hatch cover failure hence is given as: 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 29 Annex 4 Hatch Cover Failure Scenarios 30 g 20 = = 2.7 ⋅ 10 −4 annual frequency of serious casualty or total loss involving water m 73,600 ingress due to hatch cover failure. f1 = Location of water ingress In 13 of the 20 serious casualties and total losses involving water ingress and hatch cover failure events, the location for the water ingress is given. The results are shown in the below table. Table 9 Number of casualties split on reported location of water ingress Location of water ingress No. 1 cargo hold n. 1 and 2 cargo holds n. 2 cargo hold n. 2 and 7 cargo holds n. 4 cargo hold Total reported unknown cases Total Number of occurrences 7 3 1 1 1 13 7 20 % of total 54 23 7.7 7.7 7.7 100 Based on the above table, the probability of the water ingress being related to No. 1 cargo hold is taken as: g 7 +3 P1 = = = 0.77 m 13 The probability of the water ingress involving No.2 cargo hold and not No. 1 is taken as: g 1+ 1 P2 = = = 0.15 m 13 Finally, the probability of the water ingress involving any other cargo hold, but not No. 1 or No.2 is taken as: g 1 P3 = = = 0.08 m 13 Probability of total loss given water ingress location Out of the 13 cases where the location of the water ingress was recorded, 5 were total losses while 8 were serious casualties. The table below gives the distribution between total losses and serious casualties. Table 10 Number of casualties split on serious casualties and total losses. Location of water ingress No. 1 cargo hold n. 1 and 2 cargo holds n. 2 cargo hold n. 2 and 7 cargo holds n. 4 cargo hold Total known cases Unknown Serious casualties 3 2 1 1 1 8 4 Total losses 4 1 0 0 0 5 3 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 30 Annex 4 Hatch Cover Failure Scenarios Total 12 31 8 Given water ingress in No. 1 cargo hold, the probability of total loss is taken as: P4 = g 4 +1 = = 0.5 m 3 + 2 + 4 +1 Based on the information extracted, it also seems that all the total losses may be attributed to water ingress in No. 1 cargo hold. The probability of serious casualty, given water ingress in No. 1 cargo hold is estimated to: P5 = g 3+2 = = 0.5 m 3+ 2 + 4+1 For water ingress in other cargo holds than No. 1, the probabilities of total loss based on the casualty data are estimated to: P6 = P8 = g 0 = =0 m 1 Consequently, the probabilities of serious casualty given water ingress in other cargo holds than No. 1 are estimated to: P7 = P9 = g 1 = =1 m 1 Probability of fatalities given water ingress location and casualty severity In total, there are 8 total losses among the identified relevant cases. 7 of the identified hatch cover and water ingress casualties involved fatalities. In 6 of these cases, the location of the water ingress was recorded. The below table gives the distribution of fatal and non- fatal casualties. Table 11 Number of fatalities split on serious casualties and total losses Location of water ingress n. 1 cargo hold n. 1 and 2 cargo holds n. 2 cargo hold n. 2 and 7 cargo holds n. 4 cargo hold Unknown Total Number of fatal accidents among the serious casualties 0 0 1 0 0 0 1 Number of fatal accidents among the total losses 4 1 0 0 0 1 6 If assuming that the fatal accident with no details regarding water ingress location, involved flooding of No. 1 cargo hold, the probability of fatal accident given total loss due to water ingress in No. 1 cargo hold caused by hatch cover failure is to: 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 31 Annex 4 P10 = Hatch Cover Failure Scenarios 32 g 6 = = 0.75 m 8 It is also assumed that the 2 remaining total losses with no information about water ingress location, follow the pattern of the 5 reported cases, hence involving water ingress in No. 1 cargo hold. In total there were 227 fatalities in the 6 total losses involving fatalities. The probability of non- fatal accident given total loss due to water ingress in No. 1 cargo is estimated to: P11 = g 2 = = 0.25 m 8 One of the serious casualties related to No. 2 cargo hold involved 2 crew members being swept over board, and the probability of fatal accident given serious casualty due to water ingress in No. 2 cargo hold is estimated to: P16 = g 1 = = 0.5 m 2 Similarly, the probability of non- fatal accident given serious casualty due to water ingress in No.2 cargo hold is estimated to: P17 = g 1 = = 0.5 m 2 For the remaining scenarios, no fatal accidents are recorded giving: P12 = P14 = P18 = P20 = 0 and P13 = P15 = P19 = P21 = 1 The above estimates based on very few or no observations are obviously encumbered with large uncertainties. However, this does not influence on the evaluations of the risk control options, since these are directed at No. 1 and 2 hatch covers, and the majority of the cases may be related to No. 1 hatch cover. In Figure 10 the above results are fitted into the tree as given above. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 32 Annex 4 Hatch Cover Failure Scenarios Failure of at least no. 1 hatch cover 0.77 Loss of ship 0.5 Serious casualty 0.5 2.7·10-4 Serious casualty involving water ingress due to hatch cover failure Failure of at least no. 2 hatch cover, but not involving no.1 hatch cover 0.15 Loss of ship 0 Fatalities 0.75 Frequency Fatalities per Total losses Serious ship year per ship year casualties per ship year 7.8·10-5 7.8·10-5 3.1·10-3 No fatalities 0.25 2.6·10-5 2.6·10-5 Fatalities 0 No fatalities 1 1.0·10-4 1.0·10-4 Fatalities 0 No fatalities 1 Serious casualty Fatalities 0.5 2.0·10-5 1 No fatalities 0.5 2.0·10-5 Loss of ship 0 Failure of any other hatch cover, and not no.1or no.2 hatch cover 0.08 33 2.7·10-5 2.0·10-5 2.0·10-5 Fatalities 0 No fatalities 1 Serious casualty 1 Fatalities 0 No fatalities 1 2.2·10-5 2.7·10 -4 2.2·10-5 3.1·10 -3 1.0·10 -4 1.6·10-4 Figure 10 Quantified breakdown of casualty data on water ingress location, loss of ship versus serious casualty, and whether the accidents involved fatalities. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 33 Annex 4 Hatch Cover Failure Scenarios 34 Appendix 3 Hatch cover hazards and failure modes Different Hazard Identification studies have been conducted, and Table 12 below lists the hazards related to hatch covers and coamings as collected by MCA (2000). Table 12 Ser. No. 1.2.1 1.2.2 1.2.3 1.2.4 1.2.5 1.2.6 1.2.7 1.2.8 1.2.9 1.2.10 1.2.11 1.2.12 1.2.13 1.2.14 1.2.15 1.2.16 1.2.17 1.2.18 1.2.19 1.2.20 1.2.21 1.2.22 1.2.23 Hazards related to hatch covers and coamings (MCA, 2000) Hazard Pha Effects Cause se Damage to cargo All Potential for ingress of Grab striking structure hatch cover and water Heavy item of cargo dropped coamings Cargo gear wires cutting grooves in coaming Low freeboard Port Potential for ingress of Damage due to operating in frozen water conditions Sea Potential for ingress of Poor design of cleaning systems water Hatch may become open Design compromise - insufficient hatch allowing ingress of water cover protection from breaking seas. Sea (substantial). Stability loads in excess of design criteria impaired, Stresses Opening hatch covers when ship rolling increased; Increased local Inappropriate heading and speed for sea loads due to sloshing conditions Wastage due to lack of maintenance Ingress of water into Design compromise - vessel type single hold vessel Design compromise - hatch cover rigid vessel twists in seaway Inappropriate loading techniques causing coamings to distort Low freeboard Foundering Loads in imposed by seas Design compromise - insufficient hatch cover protection Inappropriate heading and speed for sea conditions Wastage due to lack of maintenance Failure of cargo MI Potential for ingress of Inadequate maintenance management hatch closing water Faulty operation (crew error) mechanism Inadequate testing Failure of cargo MI Ingress of water Inadequate maintenance management hatch seals and Inadequate testing individual cleats 1.2.24 Individual cargo All Ingress of water hatch cleat or seal failure Mechanical Mechanical Mechanical Design Mechanical Design Design Operator Operator Wastage Design Design Operator Design Mechanical Design Operator Wastage Maintenance Operator Operator Maintenance Operator Design compromise - criteria does not meet Design operational requirements 1.2.87 Stress concentration All Crack on upper deck Design compromise - inattention to detail plate 1.2.88 at hatch opening Lack of maintenance corner 1.2.89 Stress concentration All Fatigue cracking at hatch Cyclic stress by wave load coaming end 1.2.90 at hatch coaming Lack of maintenance end bracket 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Cause Type Design Maintenance Mechanical Maintenance Revision 0 34 Annex 4 Hatch Cover Failure Scenarios 35 Quick acting cleats are used to keep the cover down as shown in Figure 11. These are manually operated. The following modes of failure are realistic for these cleats: 1. The cleats are often not used, since they may be damaged if they are locked and the hydraulic opening device (auto cleating) is used. 2. The flexible rubber ring is less flexible after a time in use and may fail due to fatigue. 3. The flexible rubber ring may be damaged due to high tension. 4. Pirate manufactures of the rubber ring exist and the quality varies. The washer or spunch shown in Figure 11 should keep the hatch cover watertight at 25% indentation. These spunches may also fail due to point 4 above. SPUNCH Figure 11 Cleat Some side-rolling hatches are mounted with closing cleats (dock bolts) on top of the hatch cover at centre line. These are often not used for the same reason as number 1 for the quick acting cleats. Horizontal forces on the front part of the hatch coaming/cover and vertical forces on deck may give a gap between the coaming and the cover itself as shown in Figure 12, Figure 13 and Figure 14. Large horizontal forces on the hatch cover may move the hatch cover if the stoppers on both front and aft part of the hatch cover are damaged, however this mode of failure is more relevant for plate covers (which do not have stoppers) on smaller vessels. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 35 Annex 4 Hatch Cover Failure Scenarios 36 Figure 12 Gap due to horizontal forces on the hatch coaming. Figure 13 Gap due to vertical forces on deck. Figure 14 Gap due to horizontal forces on the hatch cover itself, moving the hatch cover. Due to rolling seas and large container loads on top of the hatch cover fatigue cracks may be initiated at the side brackets as presented in Figure 15. This is often observed on open bulk carriers, but this is not regarded as a critical failure mode for ordinary bulk carriers. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 36 Annex 4 Figure 15 Hatch Cover Failure Scenarios 37 Observed cracks on open hatch bulk carriers. The hatch covers are often dimensioned for bending at the middle span, and the height at the girder ends may sometimes be reduced as shown in Figure 16. It has been indicated that the ends may not have enough shear capacity, but we do not have any documentation verifying this failure mode. Figure 16 Bending moment and shear force distribution for a simply supported girder exposed to even load distribution. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 37 Annex 4 Appendix 4 Hatch Cover Failure Scenarios 38 Hatch covers exposed to green sea impact loads Introduction The present section considers hatch cover loads. Following the Derbyshire investigation, there has been an international discussion concerning hatch cover loads, and in the following, common procedures and recent model tests on the topic have been reviewed, and hatch cover loads have been estimated. The green sea loading on deck is of a highly complex nature. The estimation of the impact loads on the hatch cover in this project has been performed utilising the state-of-the-art hydrodynamic tools for predicting seakeeping response and results from previous research. Common procedures International Convention on Load Lines, 1966 (ILLC 66) The load and strength criterion according to ILLC 66 is given in regulation 16 pt. 2, and is referred below: (2) Where weathertight covers are of mild steel the strength shall be calculated with assumed loads not less than 1.75 metric tons per square metre (358 pounds per square foot) on hatchways in position 2, and the product of the maximum stress thus calculated and the factor of 4.25 shall not exceed the minimum ultimate strength of the material. They shall be so designed as to limit the deflection to not more than 0.0028 times the span under these loads. Mild steel plating forming the tops of covers shall be not less in thickness than one per cent of the spacing of stiffeners or 6 millimetres (0.24 inches) if that be greater. IACS Unified Requirements S21 (UR S21) The UR S21 (IACS, 1997) apply to bulk carriers contracted for construction on or after 1 July 1998, and are for hatch covers on exposed decks. Other types of loading are also to be considered, if necessary. A load model is defined, taking into account a number of ship parameters, and leads to pressure loads significantly higher than that of ILLC 66. Furthermore, a strengt h criteria is given for normal and shear stress; i.e. no to exceed 0.8 and 0.45 times the yield strength respectively. In computing the section modulus of primary supporting members, a definition of the effective with of compression panel flanges is included. UR S21 is attached in Appendix 5. Review of recent model tests Investigations sponsored by the United Kingdom authorities The ship model tests reported in MSC 72/4/1 were performed at the Denny Tank, the SSRC model testing facility in Dumbarton. The Denny Tank is regarded as a conventional towing tank equipped with the latest computer systems for data acquisition and analysis and a range of sophisticated instrumentation. The investigation was initiated during 1998 and involved physical and numerical model testing of a model of the hull of the MV Derbyshire with different bow configurations in storm and hurricane sea states. The main aim was to estimate the sensitivity of deck wetness and green water loads to variations of forward buoyancy reserve and bow height. Further, the effects of flooding the bow spaces, forward speed, different heading angles, forecastles and breakwaters were also investigated. The following conclusions were reached: 1) deck wetness and green seas loads are very sensitive to bow height and forward speed 2) the standards of the ILLC 66 are clearly inadequate for the conditions tested 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 38 Annex 4 Hatch Cover Failure Scenarios 39 3) breakwaters tested proved to be ineffective in protecting the fore end of the ship. These model tests were presented at the IMO MSC 70, see MSC 70/4. Based on the findings from 1998, and the recommendations from similar research, it was decided to continue the study during 1999, and to extend the study to cover a range of sizes of bulk carriers of more modern design. The primary aim was to establish relationships between bow height and the level of wetness, and deck and hatch cover wave loading as a function of sea state. Further, the study should provide recommendations for minimum bow height and hatch cover design. A representative prototype of three bulk carrier types: Handy size, Panamax and Cape size, were investigated (32 case studies for each vessel size). The same Handy and Cape size prototype were investigated numerically by the National Technical University of Athens (NTUA) and are reported in MSC 70/4/6. The vessels were tested in: • Head sea (180° heading), bow sea (165° and 150°) and beam sea (90°). • 2 forward speeds (3.75 and 7.5 knots) and 0 speed. • Different bow height. The bow height was varied by fitting the bow with forecastles of different size while keeping the freeboard constant at midship. • Four sea states characterised by different combination of significant wave height, Hs, and spectral peak period, Tp, were tested: [Hs=7.50m, Tp=9.60s], [Hs=10,00m, Tp=11.51s], [Hs=12.78m, Tp=12.69s], and [Hs=13-14.99m, Tp>12.69s (exact value of Tp not given)]. • For the sea state 1 and 2 the JONSWAP spectrum for limited fetch was used. The sea state 3 was created by using a modified JONSWAP spectrum with the high frequency side proportional to ω−4 instead of commonly used ω−5 , while the parameters α, γ, and ωp were determined for the hurricane weather system as given in the literature (γ=5.05). The sea state 4 (sea state 3 plus a regular wave component) was designed to model hurricane waves containing “abnormal” individual waves of over 25 metres in height. The main conclusions of the study are as follows: 1) In the more severe sea conditions and at 7.5 knots forward speed, the No.1 and No.2 hatch cover peak impact loads for all vessels exceed the design loads assumed by the UR S21. 2) The experimental results indicate that Cape size vessels will experience peak impact loads at No.1 hatch cover larger than the design loads assumed in the UR S21. This situation is worsened if the vessel is making way at any significant speed. 3) The occurrence of wetness and green sea loads systematically increases with increasing vessel size. Only in the moderate storm (Hs=7.5m), the Handy size bulk carrier is more affected by wetness and green sea loads than the larger ships. Further, wetness and green sea loads systematically increases with severity of the sea, decreasing forward freeboard and increasing ship speed. 4) Forward speed is the most critical factor in terms of wetness and associated green water loads on deck. 5) During a wetness event associated with extreme peak loads, the measured load cell pressure on the No. 1 hatch cover of the Cape size ship was, generally, about 40% higher than the depth of green water measured by wave probes (with null forward speed). 6) Forecastles reduce deck wetness and frequency of hatch loads, but do not reduce peak loads on forward hatch covers sufficiently to bring the loads within current design standards. Comparison of MARIN and SSRC tests 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 39 Annex 4 Hatch Cover Failure Scenarios 40 As mentioned in MSC 72/4/1 a series of tests were carried out at MARIN (Wageningen, the Netherlands) in order to validate the work done at the SSRC, and in general the comparison has shown good agreement, indicating the validity of seakeeping model tests at the SSRC. These results will be reported to IMO separately. A preliminary documentation discussing correlation between the results was received by DNV and is summarised below. The basis (Derbyshire) hull and bow used by the SSRC was the same as tested in MARIN as well as the test setup (It is not specific mentioned what type of the wave spectrum was used by MARIN.). However, the size of the tank was different. Further, the MARIN tests and the SSRC tests had different duration. The MARIN test was longer than each of the SSRC tests. For the hurricane conditions the SSRC adopted a sea state Hs=13-14.99m, while MARIN used a sea state Hs=15m. The SSRC carried out 4 tests with the bow in intact condition for each of two sea states: Hs=12.78m (heading 180°) and Hs=13-14.99m (heading 180°). In order to obtain a longer record the tests for each sea state were added together prior to the analysis and compared with a MARIN test carried out for Hs=12.78m (heading 180°) and Hs=15.00m (heading 180°), respectively. Further, 2 tests of the hull with the bow in damaged condition (flooded) were carried out by SSRC in the sea state Hs=12.78m (heading 180°), and two tests in the sea state with Hs=13-14.99m (heading 180°). The same as for the intact condition for each sea state in order to obtain a longer record the tests were added together before the analysis and compared with the MARIN bow in damaged test with Hs=12.78m done at 225° heading and with Hs=15m (heading 180°). All the facts mentioned above can explain some small discrepancies between the SSRC and the MARIN test results. Summary Comments • • • • • In general a series of tests carried out at MARIN as well as numerical calculations carried out by NTUA (for the same Handy and Cape size prototype) show good agreement, indicating the validity of seakeeping model tests at the SSRC. The hull and bow used by MARIN as well as the test setup was the same as tested in the SSRC. However, number of tests is limited. It seems that further tests are necessary in order to reach a firm conclusio n concerning discrepancies between the model test results and the design loads assumed by the UR S21. The model test conditions should be further checked in order to confirm the validity of the investigations, e.g. wave reflections in the basin. The Cape size bulk carrier model used in phase 2 (1999) had a large bulb. Other bulk carrier designs should also be investigated. The highest sea state applied by the SSRC: Hs=13-14.99m (Tp>12.69s) is lower than the 20year extreme for the North Atlantic according to the DNV Classification Note 30.5 “Environmental Conditions and Environmental Loads” , Hs=15.63m (Tz=12.61s, Tz denotes zero-crossing wave period). The severe sea state 3 was created by using a modified JONSWAP spectrum with the high frequency side proportional to ω−4 instead of the high frequency side proportional to ω−5 , γ=5.05, while the parameters α, and ωp were determined for the hurricane weather system as given in the literature. Both the Pierson-Moskowitz spectrum and the JONSWAP spectrum decays according to ω−5 . Further, the standard JONSWAP spectrum uses γ=3.3 being less peaked than the spectrum with γ=5.05. The modified JONSWAP spectrum with the high frequency side proportional to ω−4 has much more energy in the high frequency tail. For 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 40 Annex 4 Hatch Cover Failure Scenarios 41 structures sensitive to the high frequency range a response is significantly increased by using the wave spectrum with the high frequency side proportional to ω−4 instead of ω−5 . For responses sensitive to the body of the spectrum the JONSWAP spectrum decaying according to ω−4 will lead to lower response values than obtained by using the standard JONSWAP spectrum. Furthermore, the model tests were carried out for unidirectional wave systems. Unidirectional waves tend to be larger than short crested waves leading to higher impact loads. It should be noticed that the UR S21 is based on the conventional JONSWAP spectrum, and uses short crested seas where the wave energy is spread around a dominant angle. The hydrodynamic analysis The green sea loading on deck are caused by water flooding, due to the fact that the water (wave) surface is above deck (freeboard). The relative motion between the water surface and the vessel has been calculated using existing models of a capesize bulk carrier. The main ship particulars and characteristics are presented in Table 13. Table 13 Main ship particulars in the hydrodynamic analysis (and structural analysis in parenthesis). Length between perpendiculars, Lpp [m] Water line length, L [m] Breadth moulded, B [m] Draught, T [m] Depth moulded, D [m] Displacement, ∆ [tons] Block Coefficient, CB [-] Metacentre height, GM [m] Radius of gyration in roll about COG, r44 [m] 275 (271) 283 (283) 47 (45) 16.8 (18.15) 24.8 (24.6) 184 800 (189197) 0.83 (0.85) 10.27 15.23 An existing capesize bulk carrier has been used as a case study in the structural analysis. This vessel is slightly different from the vessel used in the hydrodynamic analysis. The main ship particulars of the vessel used in the structural analysis are written in parenthesis in Table 13. The hydrodynamic models used in this analysis consist of a DNV-SWAN model (DNV, 1997) as shown in Figure 17 and a WADAM model (DNV, 1994). 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 41 Annex 4 Figure 17 Hatch Cover Failure Scenarios 42 The DNV-SWAN mesh used in the linear analysis of the relative motions. The WADAM model has been used to calculate: • Transfer functions for relative motion of a few points in the bow area based on an undisturbed incoming wave (input to PROBAN, (DNV, 1992)) • Transfer functions for relative motion of a few points in the bow area based on a disturbed wave • Acceleration in the bow area for use in a fatigue evaluation. The DNV-SWAN model has been used to calculate: • Transfer functions for relative motion of a few points in the bow area based on a disturbed wave used to establish design waves. • Time series of linear relative motion in head sea at No. 1 hatch cover based on a specific design wave • Time series of non- linear relative motion in head sea at No. 1 hatch cover based on the same specific design wave. The analysis is performed with zero speed. Head sea conditions are regarded to be worst with respect to deck wetness according MSC 72/4/1/Add. 1. In head sea, the realistic maximum speed in extreme weather conditions will be low (and even negative) and is here assumed to be zero. Less extreme weather conditions with significant forward speed may also give significant deck loads, but this is not further treated herein. According to MSC 72/4/1: “Forward speed is the most critical factor in terms of wetness and associated green water loads on deck”. Based on this conclusion, the DNV-SWAN model is used to briefly investigate the effect of forward speed as presented in Section 0. The effect of vessel size is investigated briefly in Section 0. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 42 Annex 4 Hatch Cover Failure Scenarios 43 Relative motion The locations where the relative motions are calculated are presented in the Table 14. Table 14 Point 1 2 3 4 5 6 Points for relative motion calculations Description Bow Middle of hatch, starboard Middle of hatch, port side Aft of hatch, port side Forward of hatch, port side Middle of hatch at CL x from aft perpendicular [m] 271 247 247 239 254 247 y from centre line [m] 0 -19.5 19.5 21.0 16.5 0 WADAM (DNV, 1994) and DNV-SWAN (DNV, 1997) have been used to assess the relative motion. In DNV-SWAN the relative motion has been calculated directly, while WADAM calculates the surface elevation. POSTRESP (DNV, 1995a) is then used to establish the transfer function of relative motion based on the difference between the vessel motion and the surface elevation. POSTRESP may also be used to calculate the relative motion based on an undisturbed wave. The latter is done for WADAM for the sake of comparison at the side of the vessel. Results for different environmental conditions The extreme relative motions at the different locations are presented in the Table 15. Relative motions with a return period of 20 years are given. Different analysis conditions have been used with respect to heading and directional wave energy spreading represented by cos2 function (also referred to as short crested sea, alternatively long crested sea if no spreading function has been used). In the long term joint environmental description, the direction variable is discretified into 12 sectors from 0° to 330°. The probability of occurrence for each sector is the same (1/12). UDD is an abbreviation of this uniform directional distribution. UDD with cos2 spreading is consistent with the way main design loads normally are derived by Classification Societies. For extreme sea states, wave spreading represented by cos2 is not likely. However, e.g. head sea sector with cos2 may be interpreted as a directional distribution with head sea as the main direction. Table 15 Relative motions with a return period of 20 years in the North Atlantic wave environment using Pierson-Moskowitz wave spectrum. Condition WADAM, head sea, long crested, disturbed WADAM, head sea, long crested, undisturbed SWAN, head sea, long crested, disturbed WADAM, head sea, cos2 , disturbed WADAM, head sea, cos2 , undisturbed SWAN, head sea, cos2 , disturbed WADAM, UDD, cos2 , disturbed WADAM, UDD, cos2 , undisturbed SWAN, UDD, cos2 , disturbed Point 1 27.8 23.5 28.0 27.5 23.2 27.6 25.2 21.3 25.3 Point 2 19.8 17.7 21.0 20.7 18.2 21.6 23.2 18.9 22.5 Point 3 19.8 17.7 21.0 20.7 18.2 21.6 23.2 18.9 22.5 Point 4 17.1 15.8 17.1 18.7 16.6 18.6 22.9 18.3 22.0 Point 5 22.3 19.6 22.9 22.8 19.8 23.2 23.7 19.6 22.9 Results for both disturbed and undisturbed relative motion are presented. Disturbed/undisturbed means that the diffracted wave due to the presence of the ship is/is not taken into account as shown schematically in Figure 18. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 43 Annex 4 Figure 18 Hatch Cover Failure Scenarios 44 Disturbed versus undisturbed wave. Table 15 is presented for the purpose of comparison between disturbed and undisturbed relative motion and WADAM and DNV-SWAN. The results of the extreme relative motions in the bow area show that: • Results from WADAM agree well with DNV-SWAN for zero speed • Relative motion is larger for the disturbed wave compared to the undisturbed wave • Long crested head sea and short crested head sea gave approximately the same values • Head sea gives larger relatives motion than the uniform directional distribution at centre line • Head sea gives less relative motions than the uniform directional distribution at the ship side (due to roll motion). The relative motion at the ship side will overpredict the loads on deck especially at the centre line, since the roll component and pile up of water at the side for short small waves becomes significant in the statistical calculations. In addition, it will not give a good estimate of the average pressure over the hatch cover at centre line. The undisturbed relative motion in centre line at middle of the No. 1 hatch is used instead to determine the deck loads. The disturbed wave can not be used at this position, since it is inside the vessel’s boundaries. The transfer functions for the undisturbed relative motion are shown in Figure 19. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 44 Annex 4 Figure 19 Hatch Cover Failure Scenarios 45 Transfer function of relative motion at the centre of No. 1 hatch cover (point 6). Head sea is 180°° . The relative motion in point 6 has been calculated for Pierson-Moskowitz (PM), Jonswap (JS) and two versions of the Gamma (G) wave spectrum (with ω-4 and ω-5 , which affects the tail behaviour). According to the Annex to MSC 72/4/1, ω-4 was found to fit relevant data for hurricane extreme waves better than ω-5 . With ω-5 , the Gamma wave spectrum should be practically the same as the PM for fully developed sea (provided that peakness parameter γ = 1). Undisturbed relative motion at the middle of the hatch cover has been calculated for the North Atlantic (NA) and World-Wide (WW) scatter diagram taken from (DNV, 1998). The applied wave spectrum has been used for all sea states in the scatter diagrams. The relative motion is calculated in short crested and long crested head sea conditions. The uniform directional distribution is calculated with short crested sea. The middle of the No. 1 hatch cover for point 6 is located approximately 0.91⋅Lpp from aft perpendicular. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 45 Annex 4 Table 16 Hatch Cover Failure Scenarios 46 Undisturbed relative motion at the centre of No. 1 hatch cover (point 6). Condition Point 6 PM 16.68 17.70 17.83 15.15 15.52 15.71 WADAM, UDD, cos2 , NA WADAM, head sea, long crested, NA WADAM, head sea, cos2 , NA WADAM, UDD, cos2 , WW WADAM, head sea, long crested, WW WADAM, head sea, cos2 , WW Point 6 JS, γ = 3.3 17.81 18.78 18.98 16.44 16.42 16.78 Point 6 Gamma, ω -5 16.78 17.76 17.91 15.25 15.57 15.78 Point 6 Gamma, ω -4 14.47 15.63 15.54 13.36 14.02 14.03 It is seen from Table 16 that: • The head sea condition is more severe than the uniform directional distribution with respect to water on deck (roll motion is not contributing at centre line). • Jonswap gives higher values than PM and Gamma • Gamma with ω-5 gives higher values than Gamma with ω-4 • Gamma with ω-5 gives the approximately the same values as PM The difference in relative motion with respect to the choice of wave spectrum is seen to be significant, and the relative difference of water head on deck is then even more significant. The Jonswap wave spectrum used in Table 16 is not realistic for all sea states. A better, but more time consuming process is to establish a specific γ parameter for each sea state. According to in-house experience with other scatter diagrams, the results are expected to be close to the PM results. In the development of the UR S21 (IACS, 1997), ω-5 has been used. Based on the above, it has been decided to use the PM wave spectrum herein. Bulk carriers trade all over the world, and the bulk carriers, which have been reported lost due to collapse of the hatch cover, have sunk in different parts of the world. To verify observed collapse frequencies of hatch covers, the WW scatter diagram has been chosen as the most representative for the extreme load calculations. UDD, PM and cos2 have been assumed. The possibility for the master to go up against the waves in extreme weather conditions has not been taken into account. The resulting load will be referred to as the verification load. To verify the observed accidents may be a different matter than establishing design loads. In order to establish design loads, the NA wave environment is recommended. The long-term distribution of the undisturbed relative motion at point 6 for the NA wave environment, UDD, PM and cos2 is presented in Figure 20. The long-term distribution may be represented by a 2-parameter Weibull distribution with: • • • Long term response period, TR, = 9.253 seconds Weibull slope parameter, h, = 0.9613 Weibull scale parameter, q, = 0.8233 The relative motion at No. 1 hatch cover with a return period of n years can then be calculated as: 1 n ⋅ 365 ⋅ 24 ⋅ 3600 h RELU 6 = q ⋅ ln TR n 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 46 Annex 4 Hatch Cover Failure Scenarios Figure 20 47 Long-term distribution of relative motion at the centre of No. 1 hatch cover. North Atlantic wave environment, UDD (blue line) and short crested waves are used. Short crested head sea is presented for comparison. Non-linear correction factor to relative motion in the bow area. A design wave approach is used to estimate a non- linear correction factor for the relative motion. The design wave amplitude is defined as the ratio between the 20 year design value and the maximum peak in the transfer function of the disturbed relative motion in head sea. The design wave amplitude was calculated for point 2 in Table 15 (disturbed relative motion at side shell at middle of No. 1 hatch, NA, PM, UDD and cos2 ): Adesign = rel 20 y 22.48 = = 12.42 trf rel max 1.810 The corresponding period was 11.0 seconds for the peak in the transfer function. A check of the steepness of this design wave is made. The steepness should be less than 1/7 = 0.14. S= 2 ⋅ Adesign 2 ⋅ 12.42 = = 0.131 g 9.81 2 2 ⋅T ⋅ 11 2 ⋅π 2 ⋅ 3.1415 < 0.14 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 47 Annex 4 Hatch Cover Failure Scenarios 48 The DNV-SWAN model was then run with this regular wave both linearly and non- linearly and the relative motions for point 2 (middle of the hatch at side) were compared. The non- linear correction factor was estimated to be: k nl = rel 2 nl = 0.91 rel 2 l This factor derived for point 2 will be used in the deck load calculations of the No. 1. hatch cover at point 6. Point 2 was used since this relative motion could be taken directly from the time series in DNV-SWAN, while relative motion in point 6 had to be established based on combined motions and waves in the non- linear analysis (which is more time consuming). Design load calculation The load model presented below is a simplified one. The green water impact pressure on top of the hatch cover is found by adjusting the static pressure based on relative vertical distance between the water surface and the hatch cover. Physics of green water motion is more complex, and further studies of the water impact on deck are discussed in (Nestegård and Krokstad, 2000). The pressure on top of the hatch cover may be calculated in the following way: ( ) P d = k dyn ⋅ ρ ⋅ g ⋅ k nl ⋅ relu 6 − (h − T ) [kN/m2 ] Where: kdyn knl ρ g h T relu6 = dynamic factor relative to static pressure height = non- linear factor on relative motion for point 2 = 1.025 tons/m3 = gravity, 9.81m/s2 = height from base line to hatch cover = draught at the hatch cover = linear relative motion in head sea at point 6 (middle of No. 1 hatch cover at CL) The kdyn is a dynamic factor, which takes into account the impact of water on the deck/cover. This factor is taken from comparison between loads on the No. 1 hatch cover based on model tests and the measured height of water on deck. The UK investigations (MSC 72/4/1) indicate a factor of 1.4. However, this factor will be dependent on the configuration in the bow area (e.g. with or without large bulb). It has been assumed that the impact pressure is evenly distributed over the whole hatch cover simultaneously. This is not correct due to the complicated nature of the water impact on deck of a pitching vessel, however this model should be suitable for this investigation. A comparison between the directly calculated pressure above and the UR S21 is presented in Section 0. Comparison study between directly calculated pressure and UR S21 The comparison is made for the capesize vessel chosen for the structural analysis. This vessel is regarded as typical. The vessel’s characteristics are given in Table 13 in parenthesis. The hatch coaming is 1.20m high at centre line, the hatch cover itself is 0.89m high and the deck chamber is 0.90m. The vessel has B-60 freeboard of 6.483m and a spring of 0.855m at the middle of the No. 1. hatch cover. This gives a height from base line to hatch cover of 28.478m. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 48 Annex 4 Hatch Cover Failure Scenarios 49 Using the expression for the dynamic pressure in Section 0 and assuming UDD, PM wave spectrum and short crested sea, the verification pressure is calculated to: P d = 1.4 ⋅1.025 ⋅ 9.81 ⋅ (0.91 ⋅ 15.15 − (28.48 − 18.15) ) = 49 kN/m2 for World-Wide While the design pressure is calculated to: P d = 1.4 ⋅ 1.025 ⋅ 9.81 ⋅ (0.91 ⋅16.68 − ( 28.48 − 18.15) ) = 68 kN/m2 for North Atlantic The UR S21 gives 52 kN/m2 for the same configuration. Even if these loads are calculated for one specific capesize vessel based on a slightly different hydrodynamic model, it indicated that the direct calculations may give significant higher pressures than the UR S21 standard based on the North Atlantic wave environment. The dynamic factor of 1.4 is connected with some uncertainties, however the pressure of 68 kN/m2 is proposed as the new design pressure in the structural assessment. This corresponds to an increase of ∼30% compared to UR S21. If e.g. the dynamic factor is reduced to 1.2 based on new model tests of capesize vessels, the proposed design pressure is reduced to 58 kN/m2 , which is an increase of 13% compared to UR S21. For ships wit h totally flat deck it is likely that the dynamic factor may be as low as 1.0. Horizontal loads on coamings from green sea The green sea loads on deck may cause large horizontal forces on the hatch coaming. In the paper by Faulkner et al (1996) following the Derbyshire accident, the horizontal load is given as: g ⋅T 2 2 1 1 λ 1 p h = ⋅ ρ ⋅ v 2 = ⋅ ρ ⋅ 1.2 ⋅ + U = ⋅ ρ ⋅ 1.2 ⋅ 2 ⋅ π + U 2 2 T 2 T 1 g = ρ ⋅ (0.6 ⋅ T + U ) 2 2 π Where: ρ = The density of water, 1.025 [tonns/m3 ] T = The wave period [s] λ = The wave length [m] v = The relative velocity [m/s] λ/T = Crest velocity [m/s] U = Vessel speed [m/s] 2 kN/m2 The expression inside the parenthesis represents the relative velocity between the wave and the vessel. The 1.2 factor “is to allow for flow channelling and wind augment” according to Faulkner et al (1996). The first term represents the propagating wave profile velocity, while the next term represents the speed of the vessel heading into the waves. This expression is rather theoretical assuming that the vessel and the object hit by the wave do not disturb the wave itself. It is interpreted as the average pressure due to the drag force for a small horizontal bracing moving into the waves, neglecting slamming effects. However, to our knowledge there exist no well established procedures for predicting this horizontal green water impact forces, and the present approach by Faulkner may be used as a first estimate. Schematically the impact is shown in Figure 21. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 49 Annex 4 Hatch Cover Failure Scenarios Figure 21 50 Horizontal impact between vessel and a propagating wave. From the design wave approach in the section 0, the peak in the transfer function was identified with a wave period of 11 seconds for zero vessel speed. The ship speed in extreme wave conditions will be low and is set to zero in this case, which gives a horizontal pressure of 218 kN/m2 based on the formula. The horizontal pressure may be applied to the front coaming and front part of the hatch cover in the finite element model in order to evaluate if the linear elastic stress gives a significant stress zone exceeding the yield stress. Yield followed by permanent deformations of the coaming and supporting structure might lead to a gap between the coaming and hatch cover. This may be a relevant failure mode related to water entry into the first cargo hold. Structures in way of the front hatch coaming may reduce the horizontal pressure significantly. Furthermore this pressure does not necessarily occur simultaneously with the vertical impact loads on deck and hatch cover. When the hatch is designed for cargo on top such as containers, it is common to use a wave breaker in front of the hatch to reduce the horizontal forces. Inertia force of the hatch cover and possible fatigue damage. POSTRESP is used to calculate the vertical acceleration from WADAM. The acceleration will induce stresses in the hatch cover due to the inertia forces. The resulting stresses are used in a simplified fatigue check. The accelerations are calculated at the middle of the hatch on port side at a probability level of exceedance equal to 10-4 (most probably largest response based on 10000 cycles, which corresponds to a return period of 1 day). The position and results are shown in Table 17. Table 17 Acceleration for fatigue evaluation calculated in NA wave environment with UDD, cos 2 directional energy spreading and PM wave spectrum. x from AP [m] y from CL [m] 247 5.0 Response period, TR [s] 11.2 Weibull slope parameter, h [-] 1.01 Acceleration at 10-4 level [m/s 2 ] 2.37 The maximum principal stress in the hatch cover is taken from the finite element model. Based on the eigenweight of the hatch cover times the acceleration above, the maximum principal stress was calculated to 5.3 MPa in the plate flange at centre line at the middle of the hatch cover. Assuming a local stress concentration factor of 2.5 (due to geometry and weld effects), the total stress range is 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 50 Annex 4 Hatch Cover Failure Scenarios 51 26.5 MPa. The maximum allowable stress from DNV Classification Note 30.7 [6] is 163 MPa based on: • • • • probability level of exceedance equal to 10-4 0.7⋅108 cycles (20 year design life) SN-curve for welded joints in corrosive environment Weibull parameter of 1.01 We can conclude that fatigue in the hatch cover plate flange due to inertia forces of the eigenweight is not a realistic failure mode. Effect of forward speed The Capesize model was run by DNV-SWAN in head sea for three different vessel speeds: • 0 knots • 3.75 knots • 7.5 knots. The transfer functions from the linear analysis was combined with PM wave spectrum and NA wave environment, and the 20 year values were calculated. Point 2 representing the disturbed relative motion at the side shell at the middle of the No. 1 hatch has been used as reference. The peak of the transfer function was identified and the design wave established. For the design wave, both a linear and a non- linear analysis was performed and the non-linear correction factor was determined. The non- linear factor is multiplied with the linear 20 year value and finally an estimate of the non- linear relative motion is derived as presented in Table 18. Table 18 Forward speed effect on relative disturbed motion at point 2 Speed Linear relative motion: NA, 20 year, head sea, long crested [m] Relative linear factor Peak period in transfer function, T [s] Peak relative motio n [m/m] Design wave, A [m] Non-linear factor Non-linear relative motion: Relative non- linear factor 0 knots 21.00 3.75 knots 24.25 7.5 knots 28.11 1.00 11.0 1.80 11.7 0.95 19.85 1.00 1.15 12.6 2.19 11.1 0.86 20.86 1.05 1.34 13.7 2.58 10.9 0.82 23.10 1.16 The relative motion increased with increasing speed. The design pressure on the hatch cover No. 1 will be affected accordingly. It is also noted that the linear analysis gave higher relative factors to the speed effect than the non-linear analysis. If we assume that the height from still water line to top of the hatch cover is the same as used previously (10.33m) the pressure will be increased by: • 11% increasing the speed from 0 to 3.75 knots • 34% increasing the speed from 0 to 7.5 knots This is a significant increase. According to the model test referred to in MSC 72/4/1 the increase from 0 to 7.5 knots gave an increase of 25% for hatch No. 1 and 50% for hatch No. 2. It remains to determine the realistic vessel speeds in different wave heights and different headings for typical bulk vessels. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 51 Annex 4 Hatch Cover Failure Scenarios 52 The effect of vessel size Four vessels with different dimensions have been run with WADAM in order to see if there is a significant difference in the relative motions at the No. 1 hatch cover based on the approach used for the Capesize vessel. The vessel’s characteristics are presented in Table 19. Table 19 Type Capesize Panamax Handymax Handymax Main ship particulars in the hydrodynamic WADAM analyses Lpp [m] B [m] 271 217 180 146 47.00 32.25 30.40 22.86 T [m] ∇ [m3 ] 16.83 13.75 11.62 10.35 180465 81471 51648 28002 GMT GML r44 [m] r55 [m] [m] [m] 10.27 349.6 15.2 67.9 6.47 292.9 9.2 57.3 3.75 223.6 11.3 43.6 5.00 167.3 8.6 36.0 The relative motion is calculate along centre line of the ship based on both North Atlantic and World-Wide scatter diagram. Pierson-Moskowitz wave specrum, cos2 directional wave energy spreading and uniform directional distribution is used. The results are shown in Figure 22 to Figure 25. In addition to the relative motions, the vertical distance between the still water line and the deck at centre line including forecastle, poop, shear and bulwarks are indicated and referred to as “freeboard”. Based on the figures the following is observed: • The relative motions all along the vessel increase with increasing vessel length. • The difference between North Atlantic and World-Wide wave environment increase with increasing vessel size. Based on the formula in Section 0, the pressure on top of the No. 1 hatch cover based on the North Atlantic wave environment is calculated to: • 68.2 kN/m2 for the Capesize (middle of No. 1 hatch cover at 0.91Lpp ) • 59.2 kN/m2 for the Panamax (middle of No. 1 hatch cover at 0.90Lpp ) • 46.5 kN/m2 for the large Handymax (middle of No. 1 hatch cover at 0.86Lpp ) and • 34.1 kN/m2 for the small Handymax bulk carrier (middle of No. 1 hatch cover at 0.84Lpp ) Hence, the No. 1 hatch cover pressure increases for increasing vessel size. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 52 Annex 4 Hatch Cover Failure Scenarios 53 Linear relative motion at centre line with a return period of 20 years, uniform 2 directional distribution and cos spreading for a CAPESIZE 22,0 20,0 18,0 16,0 14,0 North Atlantic 12,0 World Wide 10,0 Freeboard 8,0 6,0 4,0 2,0 0,0 0,0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8 0,9 1,0 1,1 Distance from AP/L pp Figure 22 Relative motion for a Capesize bulk carrier. Linear relative motion at centre line with a return period of 20 years, uniform 2 directional distribution and cos spreading for a PANAMAX 22,0 20,0 18,0 16,0 14,0 North Atlantic 12,0 World Wide 10,0 Freeboard 8,0 6,0 4,0 2,0 0,0 0,0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8 0,9 1,0 1,1 Distance from AP/Lpp Figure 23 Relative motion for a Panamax bulk carrier. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 53 Annex 4 Hatch Cover Failure Scenarios 54 Linear relative motion at centre line with a return period of 20 years, uniform 2 directional distribution and cos spreading for a large HANDYMAX 22,0 20,0 18,0 16,0 14,0 North Atlantic 12,0 World Wide 10,0 Freeboard 8,0 6,0 4,0 2,0 0,0 0,0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8 0,9 1,0 1,1 Distance from AP/Lpp Figure 24 Relative motion for a “large” Handymax bulk carrier. Linear relative motion at centre line with a return period of 20 years, uniform 2 directional distribution and cos spreading for a small HANDYMAX 22,0 20,0 18,0 16,0 14,0 North Atlantic World Wide 12,0 10,0 Freeboard 8,0 6,0 4,0 2,0 0,0 0,0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8 0,9 1,0 1,1 Distance from AP/Lpp Figure 25 Relative motion for a “small” Handymax bulk carrier. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 54 Annex 4 Hatch Cover Failure Scenarios 55 Appendix 5 IACS Unified Requirements S21 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 55 Annex 4 Hatch Cover Failure Scenarios 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 56 Revision 0 56 Annex 4 Hatch Cover Failure Scenarios 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 57 Revision 0 57 Annex 4 Hatch Cover Failure Scenarios 58 Appendix 6 Analysis of Hatch Cover Capacity and Approximate Formulation for Pressure Capacity of Hatch Cover 7.1 Finite Element Model A linear finite element analysis of the hatch, including coaming and supporting structure has been carried out. The hatch cover is divided at the ship centre line, and rolls sideways to open. When closed, it rests on support pads along the coaming. The support pads are assumed to transfer vertical loads only, whereas fixation stoppers are used to prevent horizontal movement of the hatch. Two stoppers are used in the transverse direction relatively near the centre line of the ship, whereas a single stopper is used in the longitudinal direction aft position. With such support conditions, each half of the hatch can be assumed simply supported along three edges, and free along CL. Shell elements (8-nodes) have been used in combinations with beam elements representing plate stiffeners and flanges. Symmetry has been assumed, and only the port side has been modelled. Boundary conditions ensuring symmetry has been applied at the centre line. The model is shown in Figure 26, where the direction of the coordinate system is included, positive x-directions towards the bow. Blue colour is used for the hatch itself, and yellow is used for the coaming and adjacent part of the ship structure; i.e. deck plating and transverse bulkhead. The main purpose of this model is to: − − − − Enable stress checks in the hatch cover for different combinations of loading. Enable stress checks in the hatch coaming and adjacent deck structure for different combinations of loading. Due to model simplifications, such stresses should only be used as an indication of potentially highly utilised areas. Estimation of transversal stresses in the hatch cover, to be used as input for the computation of effective flange in the capacity evaluations. Estimation of fatigue stresses. A linear finite element analysis is, however, not considered adequate for ultimate capacity calculations, and has not been used directly with regards to the capacity formulation in the reliability analysis. This is because considerable load redistribution due to plastic deformation can take place, and because buckling needs to be considered. Capacity formulations are further discussed in section 0. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 58 Annex 4 Hatch Cover Failure Scenarios 59 Seen from above Hatch cover Coaming Ship deck Bukhead, aft, beam model z "Cantilever", supporting coaming Bukhead, fore x y Hatch cover, webs of girders z y Seen from underneath Figure 26 down). x Finite element model (if the figures are hard to read, try to turn them upside 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 59 Annex 4 7.2 Hatch Cover Failure Scenarios 60 Capacity model In the assessment of the hatch cover girder strength, the contribution from the panel stiffeners, including the attached flange, to the girder section modulus was deducted. Further in the assessment, the strength contribution from the girder adjacent to the hatch side was disregarded. The effectiveness of the attached flange of the top plate has been determined in accordance with UR S21. The hatch cover strength was assessed by a simplified grillage model where the transverse girders of the transverse girders of the hatch covers are assumed rigid. The strength contribution by the axial girders has been determined as an equivalent girder located at the center line. q1 q2 q3 p s1 Figure 27 s2 s3 Hatch cover model used The capacity has been estimated as outlined below. An equivalent section modulus, Zeq, was estimated as: 2 Z eq = Z1 + Z 2 3 where Z1 , is the section modulus of girder No. 1, and Z2 is the section modulus of girder No. 2. The hatch cover loading was represented as an equivalent line load model acting at the center line: q= 11 2 1 q1 + q 2 + q3 12 3 3 where q1 = p ⋅ s1 q2 = p ⋅ s2 q3 = p ⋅ s3 where p is the pressure acting on the hatch cover, and s1 , s2 , and s3 are indicated in the above figure. The required section modulus is given by: q ⋅l2 Z= 8 ⋅σ y where l is the span length between the supports, found to be 15.7 m, and σy is the yield stress. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 60 Annex 4 Hatch Cover Failure Scenarios 61 An estimated collapse line load and hence critical hatch cover pressure, pc, may be achieved according to: pc = 8 ⋅ Z ⋅σy l 2 ⋅ 1 11 2 1 s1 + s 2 + s 3 12 3 3 The model gave ultimate capacities for the investigated design as shown in the table below. Table 20 Structural analysis results Strength (kN/m2 ) Case ID Base case (ILLC 66) UR S21 UR S21 + 30% 35.8 65 84.5 The base case design was assessed by non- linear structural analysis, which gave an ultimate capacity of 35 kN/m2 (Østvold, 2001), see the figure below. 2 35 p [kN/m ] 30 25 20 15 10 5 0 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 w (mid span)/0.0056L Figure 28 Lateral pressure versus scaled mid-span lateral displacement of the centre hatch cover longitudinal girder (Østvold, 2001). 7.3 Capacity Evaluations, Initial Design 7.3.1 ILLC 66, capacity check Although the initial design presumably complies with the ILLC 66, a check based on loads and allowable stress has been performed. The design load is 1.75 tonn/m2 . This is representative for cargo loads on top of the hatch, and is not specified as a water on deck load case. The eigenweight of approximately 200 kg/m2 has been included. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 61 Annex 4 Hatch Cover Failure Scenarios 62 A stress check is specified, where the calculated stress multiplied by the factor of 4.25 should not exceed the ultimate stress. The ultimate stress for the steel is between 440MPa and 570MPa. Assuming the ultimate stress in the middle between these values, the calculated stress should (conservatively) be checked against 440/4.25=104MPa. A simple hand-calculation, considering a simply supported beam, confirms that the design comply with ILLC 66. (A Von Mises stress plot from the finite element analysis for the top plate is included in Figure 29 for information only. The plot indicates a slight violation of the stress criterion in a local area at the centre of the hatch.) Figure 29 7.3.4 Stress check, ILLC 66, allowable stress of 104 MPa. Evaluation of stresses in sub-structure The finite element model has been used to evaluate the overall stress level in the hatch coaming and adjacent deck plating. Both horizontal and vertical loading has been considered. A vertical load has been applied on the hatch and deck plating, and a horizontal load of 218 kN/m2 (see Appendix 4) has been applied to the front coaming and over the height of the hatch cover front. The model is not sufficiently refined to give detailed stress results, but is used to get an indication of the stress level. The Von Mises stress has been considered and evaluated against a criterion of 0.8 times the yield stress. The overall stress level is well below this threshold, but relatively high utilisation is seen at the lower flange of the cantilever spanning from the transverse bulkhead at the front to the coaming. High stresses are also obtained at the single hatch stopper for horizontal load in the longitudinal direction, located at the aft coaming. Plated buckling has not been evaluated. A potential increase in the load requirement must be considered also in the design of the supporting structure. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 62 Annex 4 Hatch Cover Failure Scenarios 63 Appendix 7 Analysis of hatch cover reliability Introduction The reliability analysis as presented here is intended to be representative for typical Capesize bulk carriers operating world-wide and designed according to the ILLC 66 (International Conference on Load Lines, 1996). The failure criterion is formulated as a limit state function: g = pc − pd Where the failure domain is g < 0 . Failure occurs when the pressure load p d on the hatch exceeds the pressure load capacity p c related to moment failure at the centre of the longitudinal girders. The main purpose of the analysis is to quantify the relative change in probability of failure as a consequence of a design modification. As indicated in section 2.4, the reliability analysis is carried out for three different designs as basis for the cost effectiveness analysis: 1. Base case, initial design according to ILLC 66 2. Design according to Unified Requirements S21. 3. Design according to Unified Requirements S21, with a load increase of 30%. The annual probability of failure has been calculated for each case, and effort has been made in order to apply appropriate physical models and realistic uncertainty modelling. It is evident that the absolute level of the failure probability is rather sensitive to the distribution input and the analysis models used. In our case, however, only the relative change in probability of failure is used as input to the cost effectiveness analysis, and the accuracy of the absolute values of failure probability therefore becomes somewhat less critical as long as the results are at a realistic level. The calculated annual probability of failure for the base case has been compared with the empirical probability of failure from historical data, and this comparison serves to some extent as a verification of the model. Although the failure data has been sorted to the extent possible, it is not realistic to believe that all incidents are related to the failure mode applied in the reliability analysis. There may be failures due to gross errors during design, fabrication, installation and operation, and distribution models representative for ordinary conditions cannot model such failures. The empirical data may also include other failure modes than the one applied in the reliability analysis, but this may not necessarily be a problem if the load and capacity models for such failures are comparable with the ones used. The robustness of the conclusions from the cost effectiveness analysis should be interpreted with this in mind. Load pressure model The load model is essentially based on the conclusions in Appendix 4. The probabilistic analysis program PROBAN (DNV, 1992) uses the transfer function for the relative motion between the wave elevation and the centre of the hatch cover. The short term response is calculated using the Pierson-Moskowitz wave spectrum and short-crested sea with a cos2 distribution. All headings are considered, with equal probability of occurrence. A sensitivity analysis has been carried out assuming head sea only and long-crested sea. A Gumbel extreme value distribution in a random sea state is formulated based on the assumption of Rayleigh distributed maxima. Further, the annual extreme value distribution of the relative motion between the wave elevation and the centre of the hatch cover is calculated assuming independence between sea-sates. The contribution to the failure probability is limited to the loaded condition, with minimum freeboard, which is assumed to be representative for 25% of the time in 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 63 Annex 4 Hatch Cover Failure Scenarios 64 the average case (DNV, 1998). The relationship between the relative motion and the pressure load on the hatch cover is taken from section 0, and it is assumed uniformly distributed over the whole hatch surface. ( ) P d = k dyn ⋅ ρ ⋅ g ⋅ k nl ⋅ relu 6 − (h − T ) [kN/m2 ] Where: kdyn = dynamic factor relative to static pressure height, set to 1.0 in the reliability analysis, see note. ρ = 1.025 tons/m3 g = gravity, 9.81m/s2 nl k = non- linear correction factor (=0.91, ref. section 0) relu6 = linear relative motion in head sea at middle of No. 1 hatch cover at CL h = height from base line to hatch cover (=28.48m) T = draught at the hatch cover (=18.15m) Note: The factor of 1.0 corresponds to ships with flat deck, and factors as high as 1.4 may also be relevant, see section 0. The factor of 1.0 may be optimistic, however, for the present purpose where quantifying the relative difference in failure probabilities for different designs, one would like the calculated probability of failure for the base case to be near the observed empirical value. This is obtained using a factor of 1.0. To be physically more realistic, one could chose to increase kdyn , and introduce other factors accounting for such as "bad weather avoidance" and possibly some reserve strength in the capacity formulation. This has not been done. The probability of failure increases with an order of magnitude is kdyn is set to 1.4, however, the relative difference in probability of failure between designs is only slightly reduced compared results for k dyn =1.0. Capacity Model The capacity formulation is discussed in Appendix 6. Uncertainty Modelling The uncertainty modelling is summarised in Table 21. It should be emphasised that the capacity formulation involves interaction between several failure modes, and the associated uncertainty is difficult to quantify. Similarly, the physics of the water on deck loading is very complex, and the uncertainty in the predictions will be a matter of discussion. At the same time, one sho uld remember that the main result of the present reliability analysis is the relative change in failure probability as a consequence of an implemented risk control option in terms of structural strengthening of the hatch cover. The confidence in this rela tive change is higher than in the absolute magnitude of the calculated annual failure probabilities. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 64 Annex 4 Hatch Cover Failure Scenarios 65 Table 21 Uncertainty modelling Variable Distribution type Comment Significant wave height 3-parameter Weibull, (see below for parameters) Zero-crossing wave period Lognormal (see below for parameters) Representative for worldwide conditions (BitnerGregersen, 1995) Conditional on the significant wave height (Bitner-Gregersen, 1995) Conditional on sea state Extreme relative vertical Gumbel, derived from short motion, hatch – sea surface term statistices Model uncertainty, pressure load Normal: (Mean=1.0, CoV=0.05) Yield stress Lognormal: (Mean=360MPa, CoV=0.08) Model uncertainty, pressure Normal: capacity (Mean=1.0, CoV=0.05) Assumed (Skjong et al, 1996) Assumed The parameters used in the formulation of the joint environmental model are included below, based on Bitner-Gregersen (1995). The parameters are representative for a random 3-hour sea-state. Significant wave height, Hs : Modelled by a 3-parameter Weibull-distribution β−1 hs − γ β β hs − γ f Hs (h s ) = exp − α α α with scale parameter α=2.387, slope parameter β=1.470 and location parameter γ=0.385. Zero-crossing wave period: Modelled with a log- normal distribution, conditional on the significant wave height (ln t z − µ) 2 1 f Tz | Hs (t z | hs ) = exp 2 2πσt z 2σ where and µ = E (ln T z ) = −1.010 + 2.847 hs 0.075 σ = Var (ln Tz ) = 0.161 + 0.146 e −0.683hs Additional comments to the uncertainty modelling: − Uncertainty in material strength, yield stress to be modelled with a Lognormal distribution with a CoV of 8%. The yield stress is specified to 315 MPa, and assuming this to be 5% fractile, the mean value is 360 MPa. − The uncertainty in the capacity formulation is difficult to quantify due to complexity in the interaction between failure modes. The uncertainty in the combined plate/stiffener buckling stress is applied in terms of an uncertainty factor with a mean value of 1.16 and a CoV of 16%, (Skjong et al, 1996). The uncertainty factor has been applied to σun . − Uncertainties in geometrical measures have been ignored Results Results in terms of the annual probability of failure are included for the three different designs. Results using a uniformly distributed wave heading together with short-crested sea should be used, 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 65 Annex 4 Hatch Cover Failure Scenarios 66 and the results considering long-crested head sea are included for comparison. The results are summarised in Table 22. Both First and Second Order Reliability Method (FORM and SORM) have been used in the reliability analysis. The difference between FORM and SORM is important when the heading is modelled as a uniformly distributed variable; i.e. The FORM probability of failure is typically a factor of 4 times the SORM result. FORM does not properly account for the response variation with heading when integrating the probability. The difference between FORM and SORM is small when the heading is fixed. Table 22 Annual probability of hatch cover failure using SORM Case Initial design UR S21 UR S21 + 30% load pf 9.35⋅⋅10 -4 1.16⋅⋅10 -5 7.85⋅⋅10 -7 Colman (2000) reports the re-opened formal investigation into the loss of the M/V Derbyshire in 1980. Derbyshire was a capesize OBO carrier with hatch covers designed to ILLC 66. The report gives a No. 1 hatch cover capacity of 42 kN/m2 and predicts a capacity of 83 kN/m2 if the hatch covers had been designed according to IACS UR S21. If the 35.8 kN/m2 capacity of the ILLC 66 design used above was replaced by the 42 kN/m2 in the above reliability analyses, the probability of failure of No. 1 hatch cover would be reduced. The estimated probability of No. 1 hatch cover failure would then become lower the probability of hatch cover failure conservatively deduced from casualty data, which would not be unreasonable. If replacing the estimated strength of the UR S21 design, of 65 kN/m2 with 83 kN/m2 , the estimated probability of failure of the UR S21 design would be lower than 10-6 . 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 66 Annex 4 Hatch Cover Failure Scenarios 67 Appendix 8 Marginal Cost Effectiveness When deciding upon design pressures for hatch covers on new buildings, infinitely many outcomes exist, since the design pressure is a continuous variable. To be able to evaluate different design pressure levels by Cost Effectiveness Analysis, the marginal costs and risk reductions need to be evaluated. This implies that the cost effectiveness of a design pressure is found by looking at marginal changes of the design pressure. Structural reliability analyses were carried out for a capesize No. 1 hatch cover design, believed to be representative for capesize bulk carriers. 5 points were established as shown in the Table below. Table 23 Structural Reliability results Capacity (kN/m2 ) Case ID Base case (ILLC 66) UR S21 UR S21 + 30% 35.8 65 84.5 Annual probability of failure, Pf 9.35E-04 1.16E-05 7.85E-07 Figure 29 below shows the negative logarithms of the probabilities of failure, together with a linear regression, as function of the design pressure. 7 Linear regression 6 Structural reliability results -log(pf) 5 4 UR S21+30% UR S21 3 ILLC 66 2 1 0 0 20 40 60 80 100 Hatch cover strength (kN/m2) Figure 30 Annual probability of failure (-log(Pf)) as a function of hatch cover strength The linear regression is described by the following equation: − log ( p f ) = 0.0628 ⋅ p c + 0.796 where pf is the annual probability of hatch cover collapse and pC is the hatch cover strength in kN/m2 . Similarly, a linear regression was made based on the cost data, as shown in Figure 30. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 67 Annex 4 Hatch Cover Failure Scenarios 68 180000 160000 UR S21+30% Costs (US$) 140000 UR S21 120000 100000 Linear fit ILLC 66 80000 Cost data 60000 40000 20000 0 0 20 40 60 80 100 Hatch cover strength (kN/m2) Figure 31 Cost data shown together with linear regression line. The linear regression for the costs is described by the following equation: C = 1166 ⋅ pc + 62,720 where C is the cost in US$ and pc is the hatch cover strength in kN/m2 . Based on the regression lines, the marginal Gross CAF was estimated as a function of the design pressure, as given in Figure 31. 1.00E+09 Gross CAF (US$) 1.00E+08 1.00E+07 UR S21 Gross CAF Criterion 1.00E+06 UR S21+30% 1.00E+05 1.00E+04 1.00E+03 1.00E+02 1.00E+01 1.00E+00 0 20 40 60 80 100 Hatch cover strength (kN/m2) Figure 32 Marginal Gross CAF as a function of hatch cover strength, new-building requirements. For a further 30% increase in IACS UR S21 loads, the marginal Gross CAF is estimated to US$86 million. 20010225_Annex 4Hatch Cover Failure Scenarios.doc,28 February, 2001 Revision 0 68