Low-vulnerability device for the control of helicopter rotor by

Fluid reaction surfaces (i.e. – impellers) – Sustained ancillary movement of rotary working member – Responsive to fixed actuator

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60403, 91216A, 91510, 91523, 91438, 91358A, B64C 2764

Patent

active

053103157

ABSTRACT:
The invention relates to a low-vulnerability device for the operation of a lifting and propulsing helicopter rotor by means of a cyclic plate mechanism, in which the non-rotating plate (5) is coupled at four points (1, 2, 3, 4) to four hydraulic actioning servocontrols each comprising a power jack (9), an anchoring system (10) and a servocontrol-distributor (41, 42), three servocontrols being used when normally working, the fourth being used in back-up in the event of a failure of one of the other three. Each power jack (9) is supplied by an independent hydraulic circuit which comprises the servocontrol-distributor (41, 42) operated by a mechanical input, connected to the cockpit by linkage (13), and a disengageable anchoring system. The mechanical inputs each comprise a system which, above a force threshold on a normally active servocontrol-distributor, neutralizes the servocontrol-distributor concerned, which initiates the starting up of the normally inactive servocontrol-distributor which then becomes operational in safeguard mode.

REFERENCES:
patent: 3256780 (1966-06-01), Riley et al.
patent: 3295420 (1967-01-01), Gleason
patent: 3640185 (1972-02-01), Korsak
patent: 4192218 (1980-03-01), Yamamoto
patent: 4413547 (1983-11-01), Devaud
patent: 4414881 (1983-11-01), Devaud

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