Gas turbine engine with stepped inlet compressor

Details Gas turbine engine with stepped inlet compressor Gas turbine engine with stepped inlet compressor

F - Mech Eng,Light,Heat,Weapons

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F02C 9/00 (2006.01) F01D 5/04 (2006.01) F02C 6/20 (2006.01) F02C 9/20 (2006.01)

Patent

CA 1088767

GAS TURBINE ENGINE WITH STEPPED INLET COMPRESSOR Abstract of the Disclosure A gas turbine engine has an inlet compressor with a stepped centrifugal impeller and a double diffuser therefrom controlled by valve means and operative to supply air to com- bustion apparatus from whence motive fluid is directed through a turbine to drive the compressor. The turbine may drive the load or a second power turbine in series with the compressor drive turbine can be included. The discharge from the double diffuser is controlled to vary the mass flow of the engine for operation at idling and under light loads and operable to be completely open for higher power output of the engine.

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