Axisymmetric vectoring exhaust nozzle thermal shield

Details Axisymmetric vectoring exhaust nozzle thermal shield Axisymmetric vectoring exhaust nozzle thermal shield

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/12 (2006.01) F02K 1/00 (2006.01) F02K 1/44 (2006.01) F02K 1/80 (2006.01) F02K 1/82 (2006.01)

Patent

CA 2065677

A thrust vectoring axisymmetric vectoring exhaust nozzle having universally pivoting divergent flaps is provided with a surrounding thermal shield of overlapping outer flaps and seals generally disposed in an aftwards converging conical arrangement and having a means for changing its shape from axisymmetrical to asymmetrical. Additional thermal and cooling protection is provided by a series of ejector slots located on the divergent universally pivotal flaps and adjacent interflap seals of the nozzle to both cool and thermally shield the flaps and seals.

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