Cooling circuit for turbine stator vane trailing edge

Details Cooling circuit for turbine stator vane trailing edge Cooling circuit for turbine stator vane trailing edge

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/08 (2006.01) F01D 5/18 (2006.01)

Patent

CA 2155375

A cooling circuit is provided for the second stage nozzle of a gas turbine. Cooling medium such as air is supplied into a chamber for flow through openings in an impingement plate for impingement cooling of the trailing edge. Convection air is supplied to the trailing edge for combining with the impingement flow. Both series and parallel arrangements of cooling circuits are provided for the aft portion of the vane.

Affiliated with

Also associated with

Rating

Cooling circuit for turbine stator vane trailing edge does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Cooling circuit for turbine stator vane trailing edge, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Cooling circuit for turbine stator vane trailing edge will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1704695