Device to control a jet engine

Details Device to control a jet engine Device to control a jet engine

1978-09-18

1981-01-20

Garrett, Robert E.

Power plants

Reaction motor

Condition responsive thrust varying means

F02K 308, F02C 906

Patent

active

042454700

ABSTRACT:
A hydraulic pump combined with a pressure regulator driven by a low press shaft of the jet engine, supplies a hydraulic fluid at a constant pressure into a feed conduit of a volumetric hydraulic motor coupled with a volumetric pump, which supplies fuel to the injectors of the combustion chamber of the jet engine.

REFERENCES:
patent: 2649906 (1953-08-01), Neal et al.
patent: 2686561 (1954-08-01), Isreeli et al.
patent: 2932946 (1960-04-01), Smedley
patent: 2936028 (1960-05-01), Gatzemeyer
patent: 3022738 (1962-02-01), Krute
patent: 3023575 (1962-03-01), Haase et al.
patent: 3067693 (1962-12-01), Lambeck
patent: 3183957 (1965-05-01), Cowles et al.
patent: 3669572 (1972-06-01), King

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