- 专利标题： Method and system for aligning propulsion system and vehicle having such propulsion alignment
-
申请号： US15576996申请日： 2016-05-27
-
公开(公告)号： US11485505B2公开(公告)日： 2022-11-01
- 发明人: Alexandros Iliopoulos , Laurent Regnault , Marcin Kulczyk , Alain Richer
- 申请人： BOMBARDIER INC.
- 申请人地址： CA Dorval
- 专利权人： BOMBARDIER INC.
- 当前专利权人： BOMBARDIER INC.
- 当前专利权人地址： CA Dorval
- 代理机构： Norton Rose Fulbright Canada LLP
- 国际申请： PCT/IB2016/053152 WO 20160527
- 国际公布： WO2016/193890 WO 20161208
- 主分类号： B64D27/18
- IPC分类号： B64D27/18 ; B64F5/10 ; B64C15/02 ; 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.
公开/授权文献
信息查询
