Gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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60/150

F02C 7/22 (2006.01)

Patent

CA 1168881

ABSTRACT A recuperated gas turbine engine fuel control valve and method which controls fuel flow during engine accelera- tion as a preselected empirical function of combustor gauge pressure and combustor inlet temperature, and which can also control fuel flow during deceleration without interruption of the combustion process.

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