Cooling air manifold for a gas turbine engine

Details Cooling air manifold for a gas turbine engine Cooling air manifold for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

01

D

60/185

F01D 5/08 (2006.01) F01D 5/30 (2006.01)

Patent

CA 1275176

ABSTRACT COOLING AIR MANIFOLD FOR A GAS TURBINE ENGINE A manifold (20) includes a plurality of separate, identical flow channels (28) separated by flow dividers (46). The flow dividers (46) include a thickened boss section (54) for receiving a mounting bolt (50), and are skewed adjacent the manifold outlet for forming a plurality of tangentially directed nozzles (18).

550427

Affiliated with

Also associated with

Rating

Cooling air manifold for a gas turbine engine 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 air manifold for a gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Cooling air manifold for a gas turbine engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1303580