Method for controlling augmentor liner coolant flow pressure in

Power plants – Reaction motor – Method of operation

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F02K 3075, F02K 310

Patent

active

049613120

ABSTRACT:
The present invention dicloses means and method for modulating the bypass flow in a mixed flow, variable cycle gas turbine engine. The engine includes means to vary the bypass flow and includes an augmentor and liner with coolant supplied by a portion of the bypass flow. The bypass flow pressure is modulated by sensing the pressure of the liner coolant and the pressure in the augmentor and varying the flow pressure as a function of P.sub.1, P.sub.2, or both.

REFERENCES:
patent: 3344606 (1967-10-01), Abernathy
patent: 3866417 (1975-02-01), Velegol
patent: 4010608 (1977-03-01), Simmons
patent: 4072008 (1978-02-01), Kenworthy et al.
patent: 4285194 (1981-08-01), Nash
patent: 4813229 (1989-03-01), Simmons

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