Combustor liner structure

Details Combustor liner structure Combustor liner structure

F - Mech Eng,Light,Heat,Weapons

02

C

126/111, 60/119,

F02C 3/14 (2006.01) F23R 3/08 (2006.01)

Patent

CA 1070964

Abstract of the Disclosure An air-cooled combustor liner is constructed of a continuous, constant-thickness, annular shell having a plurality of rings attached to the inner surface thereof to direct the flow of coolant air entering the shell by way of apertures formed therein, along the inner surface of the shell to provide a film cooling function. The rings are fabricated to desired dimensions sufficient to prevent significant thermal distortion which would cause flow restriction where the rings are secured to the inner surface of the shell by brazing or the like.

248966

Affiliated with

Also associated with

Rating

Combustor liner structure does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Combustor liner structure, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Combustor liner structure will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-66404