Gas turbine vane cooling air insert

Details Gas turbine vane cooling air insert Gas turbine vane cooling air insert

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/00 (2006.01) F01D 5/18 (2006.01)

Patent

CA 2079181

56,938 ABSTRACT A gas turbine stationary vane is provided having cooling air inserts and an impingement plate attached to the outer shroud of the vane. The inserts extend only a short distance above their mounting surface on the outer shroud so that there is adequate access for properly welding the inserts to the outer shroud. Insert extensions are disposed in the end of each insert so as to form cooling air inlets which project above the impingement plate. The insert extensions are installed after the insert has been welded to the outer shroud so as to not interfere with access to the weld area. The insert extensions are attached to the inserts and the impingement plate by flexible seal collars, allowing the collars to form positive seals between the components.

Affiliated with

Also associated with

Rating

Gas turbine vane cooling air insert does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine vane cooling air insert, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine vane cooling air insert will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1991228