Fluid control system

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

91445, B64C 1342

Patent

active

039958000

ABSTRACT:
A fluid-powered control system of a type employing redundant control channels and multiple fluid signal amplifiers. Each fluid amplifier has two fluid outlets having communication with respective portions of a movable, force summing structure but having no communication with the other amplifiers. A respective, differential pressure monitoring device is connected between a source of fluid under pressure and each fluid amplifier and is operative to shut off fluid flow to the respective, associated, fluid amplifier upon the occurrence, across the outlets of the fluid amplifier, of a differential pressure exceeding a predetermined level.

REFERENCES:
patent: 3494256 (1970-02-01), Bioletti et al.
patent: 3540350 (1970-11-01), Heine
patent: 3561322 (1971-02-01), Gerstine et al.
patent: 3808947 (1974-05-01), Simmons et al.

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