Method for automatic bypass operation

Power plants – Reaction motor – Method of operation

Patent

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Details

602263, F02K 304

Patent

active

051829053

ABSTRACT:
A bypass valve assembly for a gas turbine engine includes a frame defining a first flow channel in flow communication, second and third flow channels separated by a splitter. A plurality of circumferentially juxtaposed bypass doors are disposed in the second channel and are positionable between a closed position preventing airflow into the second channel and an open position providing for airflow into the second channel. Means for automatically positioning the doors in the open and closed positions provides differential pressure across the doors in the second channel, and include a spring which provides a closing torque on the door.

REFERENCES:
patent: 3316717 (1967-05-01), Castle et al.
patent: 3514952 (1970-06-01), Schumacher et al.
patent: 3910529 (1975-10-01), Putnam
patent: 3964257 (1976-06-01), Lardellier
patent: 4043121 (1977-08-01), Thomas et al.
patent: 4715779 (1987-12-01), Suciu
patent: 4791783 (1988-12-01), Neitzel

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