Turbofan with thrust reversal doors not submitted to bypass...

Details Turbofan with thrust reversal doors not submitted to bypass... Turbofan with thrust reversal doors not submitted to bypass...

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/70 (2006.01)

Patent

CA 2181857

A turbofan, preferentially with separated-flows or short nacelle, comprises two thrust reversal doors normally housed in casings formed in the nacelle and located totally outside the inner enclosure of the nacelle. When a thrust reversal effect is sought, the doors are directed in the prolongation of the fan channel, behind the rear end of the nacelle. Thus, the doors are not submitted to the engine bypass air of the jet engine when the aircraft is in flight and the inner enclosure of the nacelle presents neither leak nor discontinuity and may be totally anti-noise treated.

Affiliated with

Also associated with

Rating

Turbofan with thrust reversal doors not submitted to bypass... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbofan with thrust reversal doors not submitted to bypass..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbofan with thrust reversal doors not submitted to bypass... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1847496