Mechanical Flight Control Auxiliary Power Assist System
作者： Carlos A. Fenny , Todd Walker , Sam Arjunan , Peter M. Shultz
DOI:
关键词: Control theory 、 Limiting 、 Auxiliary power unit 、 Booster (rocketry) 、 Automotive engineering 、 Concentric 、 Valve actuator 、 Engineering 、 Control system
摘要: A mechanical flight control system for a rotary-wing aircraft is disclosed. The comprises an upstream portion, downstream and booster means connecting the portion to portion. may comprise dual concentric valve actuators and/or variety of load limiting features.
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