Aircraft propeller pitch control

Fluid reaction surfaces (i.e. – impellers) – Having positive means for impeller adjustment – Motor bodily rotatable with impeller hub or shaft

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Details

416 5, B64C 1144

Patent

active

042278600

ABSTRACT:
The pitch of a rotating propeller blade is adjusted to selectively increase the pitch of the blade or to selectively decrease the pitch of the blade. The blade is connected to a rotating hub by bearings that allow the blade to change pitch. A two-direction D.C. motor mounted on the rotating hub is selectively energized to increase or decrease the pitch of the blade. A pair of sensors are mounted on the rotating hub at different distances from the hub's axis of rotation. The first sensor is adapted to generate a signal for energizing the motor in a first direction and increase the pitch of the blade. The second sensor is adapted to generate a signal for energizing the motor in a second direction and decrease the pitch of the blade. An energy source spaced from the rotating blade selectively directs a first beam of energy onto said first sensor thereby causing said first sensor to generate a signal and energize the motor and selectively directs a second beam of energy onto said second sensor thereby causing said second sensor to generate a signal and energize the motor.

REFERENCES:
patent: 1181458 (1916-05-01), Iskols
patent: 1374787 (1921-04-01), Walker
patent: 1425922 (1922-08-01), Wesnigk
patent: 1747230 (1930-02-01), Duprey
patent: 2612228 (1952-09-01), Forsyth
patent: 2869535 (1959-01-01), Horrell
patent: 3070173 (1962-12-01), Toulmin
patent: 3573520 (1971-04-01), Dorshimer
patent: 3589832 (1971-06-01), Harris et al.
patent: 3689175 (1972-09-01), Hartzell et al.
patent: 3701498 (1972-10-01), Ferrara

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