Cooling structure for a gas turbine

Details Cooling structure for a gas turbine Cooling structure for a gas turbine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/12 (2006.01) F01D 5/18 (2006.01)

Patent

CA 2366726

In a cooling structure for a gas turbine, cooling air diffusion holes are formed from inner surface to outer surface of a platform so as to open from high pressure side blade surface of a moving blade offset in a direction toward low pressure side blade surface of adjacent moving blade confronting the high pressure side blade surface, in a direction of primary flow.

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