Variable gain synchrophasing

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416 34, 416 35, 60702, B64C 1150

Patent

active

050937910

ABSTRACT:
An aircraft engine propeller synchrophasing system (4) has a gain stage (8) which varies the gain of the system (4) according to the magnitude of the difference between the preferred propeller relative phase and the measured propeller relative phase.

REFERENCES:
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patent: 3689175 (1970-09-01), Hartzell et al.
patent: 4245955 (1981-01-01), Lambertson
patent: 4653981 (1987-03-01), Harner et al.
patent: 4659283 (1987-04-01), Niessen et al.
patent: 4900226 (1990-02-01), de Vries
patent: 4934825 (1990-06-01), Martin

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