Helicopter flight control and transmission system

Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes

Patent

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Details

244 1723, B64C 2782, B64C 2710

Patent

active

045316929

ABSTRACT:
A helicopter flight control system which eliminates the need for a cyclic pitch control and a power transmission which automatically balances the reactive torque forces imparted by counter-rotating lift rotors is disclosed.

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