System for controlling the position of the anchorage point of th

Details System for controlling the position of the anchorage point of th System for controlling the position of the anchorage point of th

1975-06-02

1976-09-21

Blix, Trygve M.

Aeronautics and astronautics

Aircraft, heavier-than-air

Helicopter or auto-rotating wing sustained, i.e., gyroplanes

244 83G, B64C 2770

Patent

active

039814610

ABSTRACT:
The invention relates to the automatic stabilisation of aircraft, inter alia helicopters.
The position of the anchorage point of piloting channels, inter alia for roll and pitch, is determined by trim motors disposed inside mechanical relays. On the basis of data received from a control column and from an automatic pilot which acts on servo controls, a logic arrangement controls parallel electronic switches which by way of parallel lines permit energisation of the trim motors in a motor priority order determined by action on the bases of the electronic switches.

REFERENCES:
patent: 2961201 (1960-11-01), Sedgfield et al.
patent: 3051418 (1962-08-01), Ramsey
patent: 3570788 (1971-03-01), Cox
patent: 3584814 (1971-06-01), Murphy
patent: 3750984 (1973-08-01), Moutiet et al.

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