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Vibration attenuating suspension system for rotary-wing aircraft rotors
Vibration attenuating suspension system for rotary-wing aircraft rotors
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机译:旋翼飞机旋翼的减振悬挂系统
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摘要
A suspension system is disclosed for reducing vibration between the rotor and the structure of a rotary-wing aircraft having a reduction-gear train coextensive with the shaft of the lift rotor. The housing of said gear train is supported by tie-rods and by a flexible beam having its mid- point attached to said housing and its extremities attached to the aircraft structure through the medium of flexible blocks. The beam may be made of metal or a composite material.
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