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.
申请公布号
DE69401958(T2)
申请公布日期
1997.06.12
申请号
DE1994601958T
申请日期
1994.07.13
申请人
UNITED TECHNOLOGIES CORP., HARTFORD, CONN., US
发明人
YAWORSKY, CHESTER, E., GLASTONBURY, CT 06033, US;REED, GALEN, H., COLCHESTER, CT 06415, US
