发明申请
US20080145221A1 Hybrid actuator for helicopter rotor blade control flaps 有权
用于直升机转子叶片控制翼片的混合致动器

Hybrid actuator for helicopter rotor blade control flaps
摘要:
A helicopter rotor blade that has a blade body and a control flap secured to the blade body. The rotor blade has a first primary mover capable of generating a first linear motion that is sufficient to generate a high amplitude, low frequency motion of the control flap; and a second primary mover capable of generating a second linear motion that is sufficient to generate a small amplitude, high frequency motion of the control flap. Further, the rotor blade has a coupling transmission for combining the first linear motion with the second linear motion that generates a cumulative linear motion; and a second transmission device that causes the cumulative linear motion to rotate the control flap.
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