Gas turbine and operating method of the same

Details Gas turbine and operating method of the same Gas turbine and operating method of the same

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/042 (2006.01) F02C 3/08 (2006.01) F02C 3/10 (2006.01) F02C 9/20 (2006.01)

Patent

CA 2043039

A gas turbine in which a centrifugal compressor which is driven by a high-pressure turbine and a variable inlet guide vane located at the inlet of the centrifugal compressor are provided, but an axial-flow compressor is not provided between the centrifugal compressor and the variable inlet guide vane, and an operating method of a gas turbine in which the output is varied by moving the variable inlet guide vane while keeping the number of rotation at a high level. It is possible to vary the output in a short period of time and durability of an engine is improve.

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