Gas turbine, gas turbine blade used therefor and...

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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F01D 5/28 (2006.01)

Patent

CA 2051133

A heavy-duty gas turbine includes a compressor; a combustion liner; a turbine blade in a single stage or multi-stages; and a turbine nozzle provided in correspondence to the turbine blade. The turbine blade has a dovetail secured to a turbine disk and has an overall length of not less than 180 mm, and it is made of a single-crystal Ni-base alloy whose .gamma. phase is a single crystal. Operating gas temperature is not less than 1400°C, and metal temperature of a first blade is not less than 1000°C under working stress.

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