Turbine engine with induced pre-swirl at compressor inlet

Details Turbine engine with induced pre-swirl at compressor inlet Turbine engine with induced pre-swirl at compressor inlet

F - Mech Eng,Light,Heat,Weapons

02

C

60/86

F02C 7/04 (2006.01) F01D 17/10 (2006.01) F02C 9/16 (2006.01) F04D 27/02 (2006.01) F04D 29/56 (2006.01)

Patent

CA 1093318

Abstract of the Disclosure A method and apparatus for utilizing bleed air taken interstage from a multi-stage compressor and passing the bleed air through hollow engine support struts in the inlet area of the compressor, the struts being formed such that a jet flap will be provided by the bleed air discharging from the strut to induce a pre-swirl in the air drawn into the compressor at low operating modes.

294739

Affiliated with

Also associated with

Rating

Turbine engine with induced pre-swirl at compressor inlet does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbine engine with induced pre-swirl at compressor inlet, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine engine with induced pre-swirl at compressor inlet will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-898441