Improvements in axisymmetric nozzles of variable geometry...

Details Improvements in axisymmetric nozzles of variable geometry... Improvements in axisymmetric nozzles of variable geometry...

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/12 (2006.01) F02K 1/00 (2006.01)

Patent

CA 2204078

Improvements in Spanish Patent No. 9,401,114, filed on May 20, 1994, covering improvements in axisymmetric nozzles of variable geometry and orientation of the flow which are intended for gas turbine engines. The nozzle comprises control means for adjusting the throat area A~ and vectoring the push, which means are formed by three rings concentric to the longitudinal axis of the engine, one inside, one intermediate, and one outside, and by a plurality of linear actuators; the outer ring including two ring segments biarticulate to each other, which limits the ability to swing to a single plane and, therefore, can vector the thrust only in the plane of pitch of the airplane. Use: On engines of twin-jet airplanes.

Affiliated with

Also associated with

Rating

Improvements in axisymmetric nozzles of variable geometry... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Improvements in axisymmetric nozzles of variable geometry..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Improvements in axisymmetric nozzles of variable geometry... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1943976