First-stage rotor blade for a combustion turbine

Details First-stage rotor blade for a combustion turbine First-stage rotor blade for a combustion turbine

F - Mech Eng,Light,Heat,Weapons

02

C

170/71

F02C 7/12 (2006.01) F01D 5/14 (2006.01)

Patent

CA 1210334

17 ABSTRACT OF THE DISCLOSURE A rotor blade for a land based combustion tur- bine includes an airfoil portion, a root portion, and a platform. The airfoil portion comprises a unique shape structured to minimize aerodynamic losses and maximize turbine efficiency.

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