System for controlling the valves of a turbo jet shaft engine no

Power plants – Reaction motor – Condition responsive thrust varying means

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60 39183, F02K 112, F02K 115

Patent

active

046088229

ABSTRACT:
The invention concerns a system for controlling the flaps of a turbine engine nozzle. High-pressure air P4 is bled from the compressor of the turbine engine to feed a compressed-air engine. The shaft of the engine rotates a constant-capacity displacement pump which sends hydraulic liquid into a jack controlling the flap or flaps of the nozzle. The invention is applicable to the control of all movable flaps of turbine engine nozzles.

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patent: 3330289 (1967-07-01), Grace
patent: 3401520 (1968-09-01), Dineen
patent: 3537647 (1970-11-01), Camboulives et al.
patent: 3570101 (1971-03-01), Stead
patent: 3640068 (1972-02-01), Mann
patent: 3932058 (1976-01-01), Harner et al.

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