Flight control system

Motors: expansible chamber type – Relatively movable working members with one having motive... – With means interconnecting working members to cause relative...

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Details

91363A, 416114, 416115, 416162, F01B 100, F15B 1316

Patent

active

043620850

ABSTRACT:
A flight control system is provided for a helicopter furnishing safety feres, and providing back up control in the event of failure of controls of the rotary head swashplate of a helicopter. The swashplate is regulated by a series of actuators which are angularly positioned at particular settings around the swashplate. In the event of a control system failure, a supplemental system controls the selected settings for the swashplate, rotary head, and spar root and blade assemblies of the helicopter.

REFERENCES:
patent: 3256780 (1966-06-01), Riley et al.
patent: 3733970 (1973-05-01), Bosch
patent: 3841586 (1974-10-01), Broadley
patent: 4030404 (1977-06-01), Meijer
patent: 4243358 (1981-01-01), Carlock et al.

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