Axisymmetric vectoring exhaust nozzle thermal shield

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...

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23926519, 23926535, 23926539, 60228, 60230, B64C 1506

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054859590

ABSTRACT:
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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"Aircraft Gas Turbine Engine Technology"--Professor Irwin E. Treager Chapters 8 and 21, Exhaust Systems and General Electric J79.
Diagramatic Cross Section of J79-17 engine nozzle and 5 photographs showing secondary forward and aft cooling air slots on secondary flap.

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