Turbine nozzle segment and repair method

Details Turbine nozzle segment and repair method Turbine nozzle segment and repair method

F - Mech Eng,Light,Heat,Weapons

01

D

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

Patent

CA 2623675

A method of repairing a turbine nozzle segment (10) having at least one vane (12) disposed between outer (14) and inner (16) bands. The method includes using an salvageable part, such as honeycomb backing strip (18) remnant, from a nozzle segment (10) that is unrepairable, and joining the honeycomb backing strip (18) to a replacement casting. The replacement casting includes a tenon (20) formed on the inner band (16) that mates with a mortise (22) formed on the back side of the honeycomb backing strip (18). A nozzle segment (10) and nozzle segment casting used in connection with the method is also disclosed.

Affiliated with

Also associated with

Rating

Turbine nozzle segment and repair method does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbine nozzle segment and repair method, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine nozzle segment and repair method will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1469807