Active tip clearance control arrangement for gas turbine engine

Details Active tip clearance control arrangement for gas turbine engine Active tip clearance control arrangement for gas turbine engine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/14 (2006.01) F01D 11/24 (2006.01) F01D 25/12 (2006.01) F02C 7/18 (2006.01) F02K 3/075 (2006.01)

Patent

CA 2696623

An active tip clearance control (ATCC) apparatus of an aircraft gas turbine engine is situated within a pressurized core case of the engine. First and second portions of bypass air flow passing through the respective compressed core compartment and the ATCC apparatus, are isolated from one another in order to improve both the ATCC performance and bypass air duct performance.

Affiliated with

Also associated with

Rating

Active tip clearance control arrangement for 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 Active tip clearance control arrangement for gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Active tip clearance control arrangement for gas turbine engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1657253