Thrust vectoring nozzle assembly
申请公布号:US4993638(A)
申请号:US19900486851
申请日期:1990.03.01
申请公布日期:1991.02.19
发明人:LARDELLIER, ALAIN M. J.
分类号:B64C15/02;F02K1/00
主分类号:B64C15/02
摘要:An exhaust nozzle assembly for vectoring the thrust of the exhaust gases from a turbojet engine is disclosed wherein the exhaust gases are vectored by an assembly that is separate from the flaps that are utilized to adjust the cross-sectional area of the exhaust nozzle. The thrust vectoring exhaust nozzle assembly has a moveable thrust vectoring assembly comprised of inner and outer vectoring members, each of which have a generally annular configuration. The vectoring members are pivotally attached to the exhaust nozzle so as to pivot about an axis extending generally perpendicularly to the longitudinal axis of the exhaust duct.
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