Method and system to facilitate preferentially distributed...

Details Method and system to facilitate preferentially distributed... Method and system to facilitate preferentially distributed...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/14 (2006.01) F02C 7/18 (2006.01) F02K 1/38 (2006.01)

Patent

CA 2601612

A turbine nozzle and shroud assembly (300) for a gas turbine engine (108) is provided. The turbine nozzle and shroud assembly (300) includes a shroud segment (110) including a leading edge (133) defining a forward face and a radial inner surface (138), the shroud segment further defining a plurality of recuperated cooling openings (177) extending obliquely through the leading edge between the forward face and the radial inner surface, and a turbine nozzle (302) including an outer band including a trailing edge defining an aft face of the outer band (183), the turbine nozzle upstream from the shroud segment and coupled with the shroud segment such that a gap (182) is defined between the aft face (150) and the forward face, the gap configured to direct cooling fluid towards a hot gas flow path flowing through the gas turbine engine.

Affiliated with

Also associated with

Rating

Method and system to facilitate preferentially distributed... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method and system to facilitate preferentially distributed..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method and system to facilitate preferentially distributed... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1558320