Gas turbine blade having a monocrystalline airfoil with a...

Details Gas turbine blade having a monocrystalline airfoil with a... Gas turbine blade having a monocrystalline airfoil with a...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/28 (2006.01) B23K 35/30 (2006.01) B23P 6/00 (2006.01) B23P 15/04 (2006.01)

Patent

CA 2535092

A repaired gas turbine blade (20) has a monocrystalline airfoil (22) made of a first nickel-base superalloy, and a repair squealer tip (46) welded to a tip of the airfoil (22). The repair squealer tip (46) is made of a second nickel-base superalloy different from the first nickel-base superalloy and having less than about 0.15 weight percent total of carbon, boron, silicon, zirconium, and hafnium.

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