F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/00 (2006.01) F01D 5/14 (2006.01) F01D 5/16 (2006.01) F01D 25/30 (2006.01)
Patent
CA 2365090
The pressure ratio .DELTA.P4S of a final stage moving blade is reduced. As a result, the Mach number in the final stage moving blade can be suppressed, and in the gas turbine operating at a pressure ratio of 20 or more, therefore, decline of turbine efficiency due to shock wave loss can be prevented securely.
Ito Eisaku
Uematsu Kazuo
Fetherstonhaugh & Co.
Mitsubishi Heavy Industries Ltd.
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