Method for reshaping a gas turbine engine combustor part

Details Method for reshaping a gas turbine engine combustor part Method for reshaping a gas turbine engine combustor part

B - Operations, Transporting

23

P

26/150

B23P 15/02 (2006.01) B23K 13/00 (2006.01) B23P 6/00 (2006.01) F23R 3/00 (2006.01)

Patent

CA 1232433

Method for Reshaping a Gas Turbine Engine Combustor Part Abstract A used combustor liner (20) for a gas turbine engine is restored to its original dimensions by mechanical reforming wherein the part is selectively heated at two circumferential locations by an in- duction coil (64). When fuel nozzle support rings (34) are replaced as well, the reforming precedes the ring welding operation and compensates for the distortion which accompanies welding.

450114

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