Mechanical flight control auxiliary power assist system

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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Details

C701S013000, C244S11700R

Reexamination Certificate

active

07668627

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.

REFERENCES:
patent: 4573125 (1986-02-01), Koenig
patent: 5060889 (1991-10-01), Nadkarni et al.

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