- 专利标题： METHOD AND SYSTEM FOR ALIGNING PROPULSION SYSTEM AND VEHICLE HAVING SUCH PROPULSION ALIGNMENT
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申请号： US15576996申请日： 2016-05-27
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公开(公告)号： US20180162540A1公开(公告)日： 2018-06-14
- 发明人: Alexandros ILIOPOULOS , Laurent REGNAULT , Marcin KULCZYK , Alain RICHER
- 申请人： BOMBARDIER INC.
- 国际申请： PCT/IB2016/053152 WO 20160527
- 主分类号： B64D27/18
- IPC分类号： B64D27/18 ; B64F5/10 ; G01M1/12
摘要：
An aircraft (10) is described as including a reference axis extending along at least a portion of the aircraft, and a propulsion system having a thrust vector feature (43) defining generally a direction of thrust of the turbofan engine (18), the thrust vector feature (43) extending relative to a thrust vector axis, where the turbofan engine (18) is disposed on the aircraft with the thrust vector feature (43) oriented with respect to the reference axis of the aircraft.