To investigate the effects of lift and propulsive force shares on flight performance,a com-pound helicopter model is derived.The model consists of a helicopter model,a wing model and a propeller model.At a low speed of 100 km/h,the Lift-to-Drag ratio(L/D)of the compound heli-copter is improved when the wing provides 20.2％of the take-off weight.At high speeds,the L/D can be improved when the propeller provides the total propulsive force.Lowering the main rotor speed increases the wing lift share,however,the maximum L/D increases first and then decreases.The maximum L/D increases with decreasing the blade twist of the main rotor.Decreasing the blade twist from-16° to-8° increases the maximum L/D by 2.3％,and the wing lift share is increased from 65.0％to 74.7％.When the main rotor torque is balanced by the rudder,the maximum L/D is increased by 2.2％without changing the wing lift share.The wing should provide more lift as increasing the take-off weight,which reduces the induced power of the main rotor and increases the L/D.When increasing the take-off weight from 9500 kg to 11000 kg,the maximum L/D is increased by 6.5％,and the wing lift share is increased from 74.7％to 80.2％.

Kelong YANG;Dong HAN;Qipeng SHI

Key Laboratory of Science and Technology on Rotorcraft Aeromechanics,College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China

中国航空学报（英文版）

[1]Kelong YANG;Dong HAN;Qipeng SHI-.Study on the lift and propulsive force shares to improve the flight performance of a compound helicopter)[J].中国航空学报（英文版）,2022(01):365-375

heli,copter,rudder

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