Support for a translating nozzle vectoring ring

Details Support for a translating nozzle vectoring ring Support for a translating nozzle vectoring ring

F - Mech Eng,Light,Heat,Weapons

02

K

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

Patent

CA 2065650

The present invention provides support for a vectoring ring used to pivot flaps in a gas turbine engine thrust vectoring nozzle. The ring support transfers at least a portion of the side loads acting generated by a gas turbine engine thrust vectoring nozzle to a relatively stationary portion of the engine. The support includes a means for allowing two degree of freedom (2 DOF) pivoting or gimballing motion and axial translation of the vectoring ring.

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