Variable camber vane for a gas turbine engine

Details Variable camber vane for a gas turbine engine Variable camber vane for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

C

170/66

F02C 9/00 (2006.01) F01D 17/16 (2006.01)

Patent

CA 1064828

VARIABLE CAMBER VANE FOR A GAS TURBINE ENGINE ABSTRACT OF THE DISCLOSURE Apparatus for controlling the direction of flow of the working medium gases in the compression section of a gas turbine engine is disclosed. Vanes are disposed across the flow path for the medium gases to direct the flow to a preferred downstream angle. In one embodiment vanes are disposed across the compressor exit passage. The camber of the vanes at the compressor exit is variable in response to engine operating conditions to conform the flow to a fixed optimum angle of entry into the combustion section. -1-

260171

Affiliated with

Also associated with

Rating

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-232792