Combustion chamber liner insert

Details Combustion chamber liner insert Combustion chamber liner insert

F - Mech Eng,Light,Heat,Weapons

23

R

60/164

F23R 3/06 (2006.01)

Patent

CA 1289368

COMBUSTION CHAMBER LINER INSERT ABSTRACT OF THE DISCLOSURE An air admission insert particularly adapted for air admission holes in a combustor liner in a gas turbine combustion system comprises a pair of sleeve members, one of which is inserted in the other in axial but eccentric relationship so that the sides of the sleeves contact each other with the intervening space between the sleeves being crescent shaped. The insert is positioned concentrically in a combustor liner air admission hole. Combustion air flows through the insert and into the combustor liner and axially through the crescent space to cool the insert as well as the liner hole perimeter.

585373

Affiliated with

Also associated with

Rating

Combustion chamber liner 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 Combustion chamber liner insert, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Combustion chamber liner insert will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1338407