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公开(公告)号:US5174502A
公开(公告)日:1992-12-29
申请号:US698045
申请日:1991-05-10
CPC分类号: F02K1/1292 , F02K1/002 , F02K1/008 , F05D2250/31 , F05D2250/34 , Y02T50/671
摘要: 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 apparatus that provides for allowing two degree of freedom (2 DOF) pivoting or gimballing motion and axial translation of the vectoring ring.