Axisymmetric vectoring exhaust nozzle

F - Mech Eng,Light,Heat,Weapons – 02 – K

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60/104

F02K 1/12 (2006.01) F02K 1/00 (2006.01) F02K 1/80 (2006.01)

Patent

CA 2013932

A thrust vectoring axisymmetric convergent divergent variable exhaust nozzle is provided with a universally pivoting joint between the divergent and convergent flaps and actuating and linkage means for changing said divergent nozzle section from axisymmetrical to asymmetrical by pivoting the divergent flaps in the radial and tangential directions with respect to the axisymmetric nozzle centerline in a controlled manner.

LandOfFree

Say what you really think

Search LandOfFree.com for Canadian inventors and patents. Rate them and share your experience with other people.

Rating

Axisymmetric vectoring exhaust nozzle does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Axisymmetric vectoring exhaust nozzle, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Axisymmetric vectoring exhaust nozzle will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-2000956

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.