Stabilizing and control device for two-bladed helicopter rotors

Fluid reaction surfaces (i.e. – impellers) – With gyroscopic reference means for rotor control

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Details

416 31, B64C 2736, B64C 2774

Patent

active

041181433

ABSTRACT:
A stabilizer bar has an aerodynamically shaped member, such as a winglet, on opposite ends thereof, and the bar is connected to rotate on its longitudinal axis and is mounted to tilt about a pivot axis at right angles thereto connecting it to a rotor shaft that also carries a pair of rotor blades the pitch of which can be changed about their longitudinal axis, that is parallel with the stabilizer bar pivot axis. A pair of oppositely directed mixing levers on opposite sides of the rotor shaft and connected parallel with the stabilizer bar for tilting movement therewith are connected by first control linkages to diametrically opposite sides of a wobble plate assembly, and by second control linkages to vary the pitch of the pair of rotor blades. An arm attached to the stabilizer bar in the plane of the aerodynamically shaped members has an end disposed in alignment with the pivot axis of the stabilizer bar that is connected by a control rod to the wobble plate assembly 90.degree. from the connections of the first control linkages, for cyclic adjustments of the pitch of the aerodynamically shaped members.

REFERENCES:
patent: 2457429 (1948-12-01), Young
patent: 2534353 (1950-12-01), Hiller et al.
patent: 2631679 (1953-03-01), Hiller et al.
patent: 2827968 (1958-03-01), Sissingh et al.
patent: 3027948 (1962-04-01), Goland et al.
patent: 3213944 (1965-10-01), Nichols et al.
patent: 3228478 (1966-01-01), Edenborough
patent: 3520498 (1970-07-01), Murphy
patent: 4025230 (1977-05-01), Kastan

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