Hydrodynamic Aspects of Steerable Thrusters
Transcription
Hydrodynamic Aspects of Steerable Thrusters
Hydrodynamic Aspects of Steerable Thrusters Jie Dang & Hans Laheij Wärtsilä Propulsion Netherlands BV (WPNL), 30-09-2004 Dynamic Positioning Conference, Houston, USA © Wärtsilä Return to session directory Contents z Introduction J. Dang z Thruster configurations J. Dang z Propulsion Efficiency J. Dang Bollard pull efficiency Free sailing efficiency Pulling or pushing arrangement? z Matching with the engine / E-motor J. Dang z Interactions H. Laheij Thruster water jet Thruster-thruster interactions Thruster-hull interactions z LIPS® HR high efficiency nozzle H. Laheij z Applications for DP / DT vessels H. Laheij z Conclusions H. Laheij © Wärtsilä 2 Introduction z Developments New ideas, new concepts, new products - everyday Diesel-electrical drive and large AC E-motors - stimulating Consequence: More possibilities More suitable system for certain operation More confusing -positive -positive -negative z Guidelines Review of the development General guideline -van Terwisga (2001) -Deter (1997) z Restricting our discussion in: © Wärtsilä Azimuth thrusters with propellers FP, CP, Ducted, Counter-rotating Propellers Not including – water jet, pump jet, Voith Schneider Not including – Cavitation, noise, maneuvering, etc. 3 Thruster configurations (1) LIPS® Z-drive thruster with an open CP propeller © Wärtsilä LIPS® L-drive thruster with a FP propeller in LIPS® HR nozzle 4 Thruster configurations (2) Thruster with Z-drive and CRP installation LIPS® Z-drive thruster with open propeller (CPP) and pulling arrangement © Wärtsilä 5 1.2 Kt, 10Kq, Eta0 z Open water characteristics Kt, 10Kq, Eta0 Propulsion efficiency (1) Kt 10Kq Eta0 1 1.2 1 0.8 0.8 0.6 0.6 0.4 0.4 0.2 0.2 0 0 0.2 0.4 0.6 0.8 1 Kt 10Kq Eta0 0 1.2 0 0.2 0.4 0.6 0.8 1 a typical open propeller Kt, 10Kq, Eta0 1.2 J=V/nD J=V/nD typical counter-rotating propellers Kt, 10Kq, Eta0 1.2 Kt 10Kq Eta0 Ktn 1 0.8 Kt 10Kq Eta0 Ktn 1 0.8 0.6 0.6 0.4 0.4 0.2 0.2 0 0 0.2 0.4 0.6 0.8 1 J=V/nD a typical nozzle propeller in 19A nozzle © Wärtsilä 1.2 6 0 0 0.2 0.4 0.6 0.8 1 J=V/nD a typical nozzle propeller in LIPS® HR high efficiency nozzle Propulsion efficiency (2) z Slope of curves dKT sT = dJ and sQ = d (10 K Q ) dJ z Counter-rotating propellers sT CRP > sT OP and sQ CRP > sQ OP z Ducted propeller sQ nozzle _ propeller © Wärtsilä J =0 =0 7 z Bollard pull efficiency Merit coefficient ( KT / π ) ηd = KQ 3 2 Merit coefficient ηd Propulsion efficiency (3) 1.9 1.7 1.5 1.3 1.1 0.9 B4-70 Wageningen CRP series Ka4-70 in 19A nozzle Ka4-70 in HR nozzle 0.7 Comparison of bollard pull efficiency among different type of propulsors © Wärtsilä 0.5 0.5 8 0.7 0.9 1.1 1.3 1.5 propeller pitch ratio (front propeller for CRP) P/D z Bollard pull efficiency Merit coefficient ηd Ducted propeller (major influences): Blade contour Pitch distribution Trailing edge Merit coefficient ηd Propulsion efficiency (4) 1.9 1.7 1.5 2.0 1.3 1.8 1.6 1.1 1.4 1.2 0.9 1.0 Ka4-70 in 19A nozzle 0.7 0.8 B4-70 in 19A nozzle 0.6 0.9 1.0 1.1 1.2 Ptip / P0.7R Influence of tip loading on pull efficiency (propellers with Kaplan form blades in No. 19 nozzle, based on the model test results of van Manen, 1962) © Wärtsilä 9 1.3 0.5 0.5 0.7 0.9 1.1 1.3 1.5 propeller pitch ratio P/D Influence of tip chord length on pull efficiency 70 engine power [%] pull thrust [tons] Propulsion efficiency (5) 60 50 120% 100% Engine output limit 80% 40 60% 30 40% 20 blades with normal anti-sing edge on suction side 10 20% blades with large ''anti-sing edge'' on pressure side blades with large ''anti-sing edge'' on pressure side 0% 50% 0 0% 50% 100% 150% engine power [%] 60% 70% 80% 90% 100% 110% engine shaft speed [%] Full scale measured power-shaft speed relation for the same propeller with different ‘anti-sing edges’ Full-scale measurements of pull thrust vs. shaft power for a tug boat – Thetis, Iskes Sleepdiensten BV, IJmuiden, the Netherlands © Wärtsilä blades with normal anti-sing edge on suction side 10 Propulsion efficiency (6) 8 Kt Ct = π J2 JKT η0 = 2π K Q Open water efficiencyη0 z Free sailing efficiency 0.8 Open Propeller B4-70 P/D= Wageningen CRP series Ka4-70 in 19A nozzle 1.2 Ka4-70 in high efficient nozzle 0.7 1.0 1.0 1.3 0.8 1.1 1.2 0.6 1.0 0.5 0.4 0.0 © Wärtsilä 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 Thrust load coefficient Ct Comparison of the open water efficiency of different propulsors (where P/D is either the pitch ratio of the propeller or the pitch ratio of the front propeller for counterrotating propellers) 11 Propulsion efficiency (7) z Pulling or pushing arrangement? z Efficiency of pulling arrangement Two factors Friction losses – underwater housing in the slipstream of the propeller wake 2. Rotational energy recovery – due to the down stream strut and fins 1. For propeller with light load Rotational energy recovery > Friction losses pulling is better fast vessel For propeller with heavy load Friction losses > Rotational energy recovery pushing is better low speed vessel © Wärtsilä 12 Propulsion efficiency (8) z Based on systematic research at SVA Potsdam © Wärtsilä Grey area Ct=0.5 to 1.0 13 Propulsion efficiency (9) z Pulling or pushing arrangement? z Wake field differences A typical wake field at propeller disc for the pushing arrangement with one strut for a twin-screw vessel © Wärtsilä 14 A typical wake field at propeller disc for the pulling arrangement of a twin-screw vessel 120% FSAH FPP OPEN z Fixed pitch propeller or controllable pitch propeller FSAH CRP BAH FPP OPEN BAH FPP HR Max. BAH thrust (366kN) at Max. torque BAH CRP 100% 90% 80% Max. BAH thrust (311kN) at Max. torque FSAH FPP HR 110% Max. BAH thrust (515kN) at Max. torque Matching with the engine/E-motor (1) MCR Design Point power PB [%] 70% 60% 50% 40% 30% Comparison of three different propulsion concepts for an offshore supply vessel with diesel-electric drive propulsion systems (two azimuth thrusters per ship at the stern), here FSAH - free sailing ahead, BAH – bollard ahead 20% 10% 0% 0% 10% 20% 30% 40% 50% 60% 70% shaft speed N [%] © Wärtsilä 15 80% 90% 100% 110% 120% Matching with the engine/E-motor (2) z A typical semi-submersible PB[%] 160% Trial-(bow)Thuster Trial-(stern)Thuster Service-(bow)Thruster 140% Service-(stern)Thruster Bollard Vs=0kn Bollard Vs=-2kn 120% MCR 100% 80% Qmax 60% 40% The typical propeller curves for a semi-submersible with two pontoons and four azimuth thrusters with FPP in LIPS® HR nozzle, two thrusters at the bow and two at the stern 20% 0% 50% 60% 70% 80% 90% 100% 110% 120% N[%] © Wärtsilä 16 Thruster-thruster, thruster-hull interactions understanding the jet (1) z water jet of the thruster - the shape © Wärtsilä 17 Thruster-thruster, thruster-hull interactions understanding the jet (2) z water jet of the thruster - the position of the maximum speed Shape of jet of water behind a working thruster at zero speed (bollard condition) Line of maximum speed D Line of zero speed © Wärtsilä 18 Thruster-thruster, thruster-hull interactions understanding the jet (3) z water jet of the thruster - the maximum speed Maximum jet speeds for thruster in bollard pull condition © Wärtsilä 19 Thruster-thruster, thruster-hull interactions understanding the jet (4) z Maximum speed for water jet close to a flat plate Position of maximum speed does not stay on center line, but moves towards the plate Position of maximum speed goes to shaft center line at x/D = 4 (was 6 without plate) Flat plate at 0.75D below thruster center line Magnitude of maximum speed does not change compared to open water situation ! © Wärtsilä 20 Thruster-thruster, thruster-hull interactions thruster-thruster interaction (1) z 3 major different interactions in discussion D D x D x φ x © Wärtsilä 21 Thruster-thruster, thruster-hull interactions z Thrusters in tandem in free open water z Formula to calculate thrust ratio T / T0 = 1 − 0.8 2 ( x / D)3 Thrust ratio [%] . thruster-thruster interaction (2) 100% 80% 60% 40% Lehn(1980) Moberg(1983) 20% D x 0% 0 © Wärtsilä 22 5 10 15 20 25 30 Propeller distance ratio x/D Thruster-thruster, thruster-hull interactions z Thrusters in tandem under a flat bottom z Formula to calculate thrust ratio 2 ( x / D)3 T / T0 = 1 − 0.75 Thrust ratio [%] . thruster-thruster interaction (3) 100% 80% 60% 40% Nienhuis(1992) D Blaurock (1977) 20% x 0% 0 © Wärtsilä 23 5 10 15 20 25 30 Propeller distance ratio x/D Thruster-thruster, thruster-hull interactions thruster-thruster interaction (4) . Thrust ratio [%] z Steering angle on the thrusters can reduce the thrustloss z Larger angles reduce thrustloss z Formula to calculate the thrustratio 100% 90% 80% 70% 60% 50% 40% tφ = t + (1 − t ) φ3 30% 130 / t 3 + φ 3 20% Nienhuis (1992) x/D=2.0 Nienhuis (1992) x/D=4.0 Nienhuis (1992) x/D=8.0 Nienhuis (1992) x/D=16.0 Lehn (1980) x/D=3.0 Lehn (1980) x/D=6.0 10% 0% 0 D φ 10 15 20 25 30 steering angle of the forward thruster [degrees] x © Wärtsilä 5 24 35 Thruster-thruster, thruster-hull interactions thruster-thruster interaction (5) 100% Total thrust ratio of two thrusters [%] . z Interaction applicable to both bollard and free sailing condition z Important since DP thrusters are used for main propulsion as well 80% 60% 40% Blaurock (1977) J=0.00 Blaurock (1977) J=0.20 Blaurock (1977) J=0.36 20% 0% 0 © Wärtsilä 25 5 10 15 20 25 30 Propeller distance ratio x/D Thruster-thruster, thruster-hull interactions Thruster-hull interaction (1) z Water jet close to a flat plate z Reductions can be as high as 20-25%, z Thrusters in the bow are inefficient in the sailing direction © Wärtsilä 26 Thruster-thruster, thruster-hull interactions Thruster-hull interaction (2) z water jet along curved surface © Wärtsilä 27 Thruster-thruster, thruster-hull interactions thruster-hull interaction (3) z Coanda effect © Wärtsilä 28 Thruster-thruster, thruster-hull interactions Thruster-hull interactions (4) thrust deduction t z Thrust deduction depending on stern heeling angle z For astern thrust in practice two times larger than ahead Slope 0.12 0.11 0.1 0.09 0.08 0.07 0.06 0.05 0.04 0.03 10 12 14 16 18 20 22 24 stern heeling angle [degrees] © Wärtsilä 29 Thruster-thruster, thruster-hull interactions thruster-hull interaction (5) z Typical results of Thruster-hull interaction test 0 345 100% 15 90% 330 30 80% 315 45 70% 60% 300 60 50% 40% 30% 285 75 20% 10% 0% 270 90 255 105 240 120 225 135 210 150 195 165 180 © Wärtsilä 30 LIPS® HR Nozzle introduction - different nozzles (1) z Working principle of nozzle propellers Flow induced pressure difference creates positive thrust © Wärtsilä 31 LIPS® HR Nozzle introduction - different nozzles (2) z Different nozzles © Wärtsilä 32 LIPS® HR Nozzle introduction - different nozzles (3) z Different flow patterns at BAH and FSAH Free sailing (FSAH) Bollard condition (BAH) © Wärtsilä 33 LIPS® HR Nozzle background of HR nozzle z Designed to improve the flow around the nozzle z Designed to improve efficiency at high speed z Series tests done at German SVA Potsdam institute z Improved performance; 8 to 10% better than 19A Flow visualisation in cavitation tunnel © Wärtsilä 34 LIPS® HR Nozzle flow analysis - CFD (1) z Propeller in HR nozzle - StarCD® © Wärtsilä 35 LIPS® HR Nozzle flow analysis - CFD (2) z Comparison - 19A versus HR nozzle VELOCITY FIELD 19A Nozzle © Wärtsilä HR Nozzle 36 LIPS® HR Nozzle flow analysis - CFD (3) z Calculated flow pattern around HR nozzle rounded leading and trailing edge larger induced velocity more nozzle thrust and less resistance © Wärtsilä 37 LIPS® HR Nozzle flow analysis - CFD (4) z Comparison - calculated bollard pull thrust Bollard condition 19A 120% 100% HR 108% 103% 100% 100% 80% 60% 40% 20% 0% Model scale © Wärtsilä Full scale 38 LIPS® HR Nozzle flow analysis - CFD (5) Full scale Difference model to full scale Model scale © Wärtsilä 39 LIPS® HR Nozzle full scale experience Many HR-nozzles already sailing ! With: z CPP’s z FPP’s (4 and 5 bladed) z Steerable thrusters Up to 3.75 [m] Up to 5500 kW z Ranging from 0 to 18+ knots z Dmax. = 5.2 [m] with 12640 kW © Wärtsilä 40 Application of Thrusters z The largest pipe layer Solitaire z Vessel spec Length Transit speed Accommodation 300 13 420 [m] [kn] [men] z Thrusters © Wärtsilä 8 LIPS® azimuth thrusters partly bollard pull and partly free sailing design partly HR and partly special nozzle 5.55MW@199RPM propeller diameter 3.75m 41 Application of Thrusters z Heavy-lifting vessel - Thialf z Vessel spec Length Breadth Accommodation 201 88.4 736 [m] [m] [men] z Thrusters © Wärtsilä 6 LIPS® azimuth retractable thrusters bollard pull design (85 tons/unit) 19A nozzle 5.5MW@199RPM propeller diameter 3.4m 42 Application of Thrusters z Maintenance Service Support Accommodation Unit z vessel spec Length Breadth ~94 ~45 [m] [m] z thrusters 4 LIPS® azimuth thrusters bollard pull design (50 tons/unit) LIPS® HR nozzle 2.5MW @ 203RPM propeller diameter 3.2m Overspeed of driving motor for free sailing © Wärtsilä 43 Application of Thrusters z Largest Semi Submersible Heavy Lift Vessel Blue Marlin 2 x Retractable thrusters with HR Nozzle Propeller diameter 3.4 m 2 x 4500 kW Main propulsion upgraded with HR Nozzle Propeller diameter 5.2 m 1 x 12640 kW Resulting in more than 30% increase in bollard thrust Carrying largest offshore structures in the world © Wärtsilä 44 Application of Thrusters z Cable Ship CS Atlantic Guardian P=2 X 2200 kW Propellerdiameter 2.5 m Electric drive CPP thruster L-drive configuration Able to absorb full power at all conditions © Wärtsilä 45 Application of Thrusters z Cable Layer © Wärtsilä 46 CS- Knight Main propulsion 2 X 4500 kW Propellerdiameter 3.4 m Retractable 2 x 2000 kW Propellerdiameter 2.5 m Electric driven FP propellers Application of Thrusters z Anchor Handling Tug Supply Vessel © Wärtsilä Seabulk Badamyar P= 2 X 1440 kW Propellerdiameter 2.1 m 7.4% extra bollard pull due to HR Nozzle Bollard pull is 10% over charter requirements 47 Conclusions Hydrodynamic aspects of steerable thrusters z Mission profile determines the choice of the design point; off-design condition and its co-operation with the E-motor (or engine) are important z For low-medium speed applications (e.g. DP/DT) pushing propellers are more efficient than pulling propellers z Interactions among thrusters, hull, barge, etc should not be ignored in thruster design z High efficiency nozzles improve efficiency 8% extra bollard pull thrust 10% extra free sailing propulsion efficiency Propulsion Supplier should take all hydrodynamic aspects of thrusters into account to ensure a perfect match between thrusters and the vessel © Wärtsilä 48 Questions? Wärtsilä Propulsion Netherlands BV Jie Dang Jie.Dang@wartsila.com +31 416 388283 Hans Laheij Hans.Laheij@wartsila.com +31 416 388546 © Wärtsilä