发明名称 Thrust vector adjustment device
摘要 The present invention provides a robust means of adjusting the angular mounting of thrust producing devices such as airplane engines. The device provides independent adjustment of the thrust vector for each axis and offset adjustment to maintain the center line of the engine. A means of indicating the angle of adjustment is inherent in the design. The invention also provides for an opening along the centerline to accommodate power take-off shafts or to mount jet or ducted fan engines.
申请公布号 US2003178525(A1) 申请公布日期 2003.09.25
申请号 US20030394850 申请日期 2003.03.22
申请人 KRR ENTERPRISES, INC. 发明人 RAMER RONALD L.;DAVIS ROBERT E.
分类号 A63H27/26;(IPC1-7):F41G7/00 主分类号 A63H27/26
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