发明名称 Thrust vectoring and variable exhaust area for jet engine nozzle
摘要 A jet engine nozzle having a pair of pivoting extension arms and a pair of pivoting shells connected to a jet pipe is provided. The first extension arm is pivotally connected to the jet pipe at a first location, while the second extension arm is pivotally connected to the jet pipe at a second location. Each shell is pivotally connected at both the first and second locations. An axis of rotation associated with the first location is coaxial to an axis of rotation associated with the second location. Independent actuation means are provided to rotate the extension arms and the shells, thereby enabling adjustment of the thrust-vector angle or the exhaust area of the nozzle.
申请公布号 US2003159430(A1) 申请公布日期 2003.08.28
申请号 US20030379633 申请日期 2003.03.05
申请人 LAIR JEAN-PIERRE 发明人 LAIR JEAN-PIERRE
分类号 B64C15/02;F02K1/00;F02K1/04;F02K1/11;F02K1/12;F02K1/15;F02K1/54;F02K1/60;F02K1/70;F02K1/76;F02K1/80;(IPC1-7):F02K1/00 主分类号 B64C15/02
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