Repair of gas turbine blade tip without recoating the...

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

Patent

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Details

F01D 5/28 (2006.01) B23P 6/00 (2006.01) C22C 19/05 (2006.01) C22F 1/10 (2006.01)

Patent

CA 2530247

A damaged gas turbine blade (40) which has previously been in service, and which is made of a base metal, is furnished. Any damaged material is removed from the damaged blade tip (50). The damaged blade tip (50) is weld repaired with a nickel-base superalloy that is more resistant to oxidation resistance than is the base metal in the operating environment of the tip-repaired gas turbine blade (60). The method does not include any step of coating a lateral surface (80) of the repaired blade tip (62) with a non-ceramic coating after the step of weld repairing.

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