Invention Grant
US07668627B2 Mechanical flight control auxiliary power assist system 有权
机械飞行辅助辅助辅助系统

Mechanical flight control auxiliary power assist system
Abstract:
A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and a booster means for connecting the upstream portion to the downstream portion. The booster means may comprise dual concentric valve actuators and/or a variety of system load limiting features.
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