Swash-plate device for controlling the pitch of rotor blades wit

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

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416115, 416116, 416134A, 416140, 416141, 416138, 74579R, 244 1725, B64C 27605

Patent

active

060331828

ABSTRACT:
The non-rotating plate of the device is stopped from rotating around the rotor axis by a stop arm with at least one rigid stop track extending substantially axially and secured to the structure of the rotor aircraft. The track works together with a stop pin, integral with the non-rotating plate to stop the latter from rotating. The track has two flanges between which the pin is engaged so as to follow on this track a straight trajectory, parallel to the rotor axis and a circular arc trajectory centered on this axis, in the case of variation in the collective and cyclic pitch respectively. The stop pin includes a pad sliding between the two flanges of a slide constituting the said track and hinged around its fastening axis on the non-rotating plate.

REFERENCES:
patent: 3738772 (1973-06-01), Parenti
patent: 4732540 (1988-03-01), Mouille
patent: 4952120 (1990-08-01), Aubry et al.
patent: 5135356 (1992-08-01), Sherperd
patent: 5209429 (1993-05-01), Doolin et al.
patent: 5340279 (1994-08-01), Cycon et al.
patent: 5599167 (1997-02-01), Daldosso
patent: 5906476 (1999-05-01), Arlton

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