| 摘要 |
<p>A method of repairing a combustion chamber assembly (32) from an axial flow gas turbine engine (20) is disclosed. Various details are developped which facilitate repair of the combustion chamber assembly of the engine. In one detailed embodiment, a laser beam (80) separates 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.</p> |
