Method for repairing a combustion chamber assembly

Metal working – Method of mechanical manufacture – Impeller making

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Details

2940203, B23P 1500

Patent

active

054309352

ABSTRACT:
A method of repairing a combustion chamber assembly 32 from an axial flow gas turbine engine 20 is disclosed. Various details are developed which facilitate repair of the combustion chamber assembly of the engine. In one detailed embodiment, a laser beam 80 separated the bulkhead of the combustion chamber assembly from the remainder of the assembly to allow independent repair of the bulkhead and the remainder of the assembly.

REFERENCES:
patent: 4451979 (1984-06-01), Schuster
patent: 4741128 (1988-05-01), Reaves et al.
patent: 4936002 (1990-06-01), Silvestri, Jr. et al.
patent: 5205465 (1993-04-01), Bogard et al.
patent: 5267397 (1993-12-01), Wilcox

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