Method for repairing a turbine nozzle segment

Details Method for repairing a turbine nozzle segment Method for repairing a turbine nozzle segment

B - Operations, Transporting

23

P

B23P 6/00 (2006.01) F01D 9/02 (2006.01)

Patent

CA 2647767

A method for repairing a turbine nozzle segment (118) includes providing a turbine nozzle segment (118) having an enclosure (142) with an integral discourager (166), removing the enclosure (142) and/or the discourager (166) from the turbine nozzle segment (118) and attaching a new enclosure (142) and/or discourager (166) to the turbine nozzle segment (118).

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