A repair apparatus 78 for repairing the combustion chamber assembly 32 of a gas turbine engine 20 is disclosed. Various construction details are developed which increase the speed of the repair process and the structural integrity of the repaired combustion chamber assembly. In one particular embodiment, the repair =apparatus has a support assembly 82 which is adapted by locating pins 98 to engage the lug mountings 48 of the combustion chamber assembly 32.
申请公布号
DE69413402(D1)
申请公布日期
1998.10.22
申请号
DE1994613402
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