发明名称 Two-axis thrust vectoring nozzle
摘要 A nozzle for a jet engine generally includes a nozzle rim and a bendable duct for communicating an exhaust flow generated by the engine to the nozzle rim. A gimbal joint pivotably couples the nozzle rim to supporting structure. The gimbal joint allows the nozzle rim to be pivoted about a first axis and a second axis, thereby allowing changes to the vector at which the exhaust flow is discharged from the nozzle rim.
申请公布号 US7216476(B2) 申请公布日期 2007.05.15
申请号 US20030731368 申请日期 2003.12.09
申请人 THE BOEING COMPANY 发明人 FINK LAWRENCE E.
分类号 F02K9/84;F02K1/00 主分类号 F02K9/84
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