Methods for making combustor liner replacement panels
A combustor and liner technology, applied in combustion methods, combustion chambers, combustion equipment, etc., can solve problems such as expensive and accurate dimensional relationship changes, time-consuming, etc.
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[0080] FIG. 1 is a schematic diagram of a gas turbine engine 10 including a low pressure compressor 12 , a high pressure compressor 14 and a combustor 16 . Engine 10 also includes a high pressure turbine 18 and a low pressure turbine 20 . Compressor 12 and turbine 20 are joined together by a first shaft 22 , while compressor 14 and turbine 18 are joined together by a second shaft 21 . In one embodiment, gas turbine engine 10 is a GE90 engine commercially available from General Electric Aircraft Engines of Cincinnati, Ohio. In another embodiment, the gas turbine engine 10 is a CF engine commercially available from General Electric Aircraft Engines of Cincinnati, Ohio.
[0081] In operation, air flows through the low-pressure compressor 12 and compressed air is supplied from the low-pressure compressor 12 to the high-pressure compressor 14 . The highly compressed air is delivered to the combustor 16 . Airflow from combustor 16 drives turbine 18 and turbine 20 and exits gas tu...
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