Hydrodynamic design of propellerbladesThe propeller blades are computer designed,based on advanced hydrodynamictheories, practical experienceand model tests at various hydrodynamicinstitutes.The blades are designed specially foreach hull and according to the operatingconditions of the vessel.High propulsion efficiency, suppressednoise levels and vibration behaviour arethe prime design objectives.<strong>Propeller</strong> efficiency is mainly determinedby diameter and the correspondingoptimum speed. To a lesser, butstill important degree, the blade area,the pitch and thickness distribution alsohave an affect on the overall efficiency.Blade area is selected according to requirementsfor minimum cavitation,noise and vibration levels.To reduce the extent of cavitation on theblades even further, the pitch distributionis often reduced at the hub and tip,fig 26.Care must be taken not to make excessivepitch reduction which will effectthe efficiency.Thickness distribution is chosen accordingto the requirements of theClassification Societies for unskewedpropellers.Pitch/diameter ratio1,401,201,000,800,600,40 0,60 0,80 1,00Dimensionless ratio of radii r/RFig 26: Pitch distribution along radiusCavitationCavitation is associated with generationof bubbles caused by a decreasein the local pressure below the prevailingsaturation pressure. The low pressurecan be located at different positionson the blade as well as in thetrailing wake.When water passes the surface of thepropeller it will experience areas wherethe pressure is below the saturationpressure eventually leading to generationof air bubbles. Further downstream the bubbles will enter a higherpressure region where the bubbles willcollapse and cause noise and vibrationsto occur, in particular if the collapseof bubbles takes place on the hullsurface.Three main types of cavitation exist –their nature and position on the bladescan be characterized as: Sheet cavitation on suction side(Fig 27)The sheet cavitation is generated at theleading edge due to a low pressurepeak in this region. If the extent of cavitationis limited and the clearance tothe hull is sufficient, no severe noise/vibration will occur. In case the cavitationextends to more than half of thechord length, it might develop into cloudcavitation. Cloud cavitation often leadsto cavitation erosion of the blade andshould therefore be avoided. Sheet cavitationin the tip region can develop intoa tip vortex which will travel downstream. If the tip vortex extends to therudder, it may cause erosion.2 03 93 91–1.0Fig 27: Suction side (sheet cavitation)V Bubble cavitation(Fig 28)In case the propeller is overloaded – iethe blade area is too small compared tothe thrust required – the mid chord areawill be covered by cavitation. This typeof cavitation is generally followed bycloud cavitation which may lead to erosion.Due to this it must be avoided inthe design.2 03 93 91–1.0Fig 28: Suction side (bubble cavitation) Sheet cavitation on pressure side(Fig 29)This type of cavitation is of the sametype as the suction side sheet cavitationbut the generated bubbles have a tendencyto collapse on the blade surfacebefore leaving the trailing edge. Thedanger of erosion is eminent and theblade should therefore be designedwithout any pressure side cavitation.By using advanced computer programmesthe propeller designs suppliedby MAN B&W Alpha will bechecked for the above cavitation typesand designed to minimize the extent ofcavitation as well as avoiding harmfulcavitation erosion.2 03 93 91–1.0Fig 29: Pressure side (sheet cavitation)VV20This document, and more, is available for download at <strong>Martin's</strong> <strong>Marine</strong> <strong>Engineering</strong> <strong>Page</strong> - www.dieselduck.net
For each condition and all angular positionsbehind the actual hull, the flowaround the blade is calculated. The extentof cavitation is evaluated with respectto noise and vibration, fig 30.Angle of attack (degrees)4Suction2ActualHigh skewTo suppress cavitation–induced pressureimpulses even further, a high skewdesign can be supplied, fig 31. By skewingthe blade it is possible to reduce thevibration level to less than 30% of anunskewed design. Because skew doesnot affect the propeller efficiency, it is almoststandard design on vessels wherelow vibration levels are required.Today, the skew distribution is of the“balanced” type, which means that theblade chords at the inner radii areskewed (moved) forward, while at theouter radii the cords are skewed aft. Bydesigning blades with this kind of skewdistribution, it is possible to control thespindle torque and thereby minimizethe force on the actuating mechanisminside the propeller hub, fig 32.0–2–4Pressure0.4 0.6 0.8 1.0Dimensionless ratio of radii r/RSpindle torque (kNm)420–2–40 90 180 270 360Angle (degrees)0.40 0.60 0.801.00r/R2 03 24 21–0.1Fig 31: High skew designSkew angleCentre lineshaft2 03 24 11–4.1Single bladeAll bladesFig 32: Spindle torqueFor high skew designs, the normalsimple beam theory does not apply anda more detailed finite element analysismust be carried out, fig 33.2 04 05 37–8.0Fig 30: Cavitation chart and extensionof sheet cavitation – suction side10 20 30 4050602 04 01 12–4.0ISO stress levels in N/mmFig 33: Finite element calculation ofpropeller bladeThis document, and more, is available for download at <strong>Martin's</strong> <strong>Marine</strong> <strong>Engineering</strong> <strong>Page</strong> - www.dieselduck.net21