Valve assembly for a gas turbine engine

Details Valve assembly for a gas turbine engine Valve assembly for a gas turbine engine

2008-09-02

2010-10-26

Look, Edward (Department: 3745)

Power plants

Reaction motor

Method of operation

C060S262000

Reexamination Certificate

active

07818957

ABSTRACT:
A method for channeling compressed air to a gas turbine engine augmentor is provided. The method includes coupling an annular slide valve to a gas turbine engine separation liner, coupling a valve seat to a gas turbine engine diffuser such that an airflow passage is defined between the annular slide valve and the valve seat, and channeling compressed air to the annular slide valve to facilitate regulating the quantity of fan bypass air channeled to the gas turbine engine augmentor.

REFERENCES:
patent: 4175384 (1979-11-01), Wagenknecht et al.
patent: 5287697 (1994-02-01), Johnson et al.
patent: 5343697 (1994-09-01), Johnson et al.
patent: 5694767 (1997-12-01), Vdoviak et al.

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