Ground mode control of aircraft propeller speed and pitch

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Details

36443107, 416 25, 416 35, 416 44, G06F 1548, B63H 310, B64C 1134, F01D 700

Patent

active

050290916

ABSTRACT:
A ground mode pitch position logic and control is shown and described in this invention. A method for scheduling and limiting the pitch actuator reference signal in accordance with the actuator commanded schedule, propeller overspeed and propeller underspeed.

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patent: 2980188 (1961-04-01), Allen, Jr. et al.
patent: 4711615 (1987-12-01), Rusu
patent: 4772180 (1988-09-01), Walker et al.
patent: 4904157 (1990-02-01), Pace et al.
patent: 4958289 (1990-09-01), Sum et al.

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