Gas turbine engine component repair

Metal working – Method of mechanical manufacture – Impeller making

Patent

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Details

298897, 2940207, 2940218, 228119, 21912166, 21912185, B23P 1902, B23K 2600, B23K 3100

Patent

active

051427788

ABSTRACT:
A procedure is described for the repair of gas turbine engine turbine components which involves the repair of cracks and other defects and the replacement of worn or eroded material followed by the laser melting of a thin layer of metal on the surface of the component in those areas requiring reconfiguration to return to the original dimensions. The reconfiguration by laser melting is also useful for new articles which are out of tolerance, and generally for shaping objects from metal sheet or plate.

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