Ground mode control of aircraft propeller speed and pitch

G - Physics – 05 – D

Patent

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341/95

G05D 1/08 (2006.01) B64C 11/30 (2006.01)

Patent

CA 2014181

ABSTRACT OF THE DISCLOSURE 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. -20-

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