公开(公告)号：US20180162540A1

公开(公告)日：2018-06-14

申请号：US15576996

申请日：2016-05-27

Applicant: BOMBARDIER INC.

Inventor： Alexandros ILIOPOULOS ,  Laurent REGNAULT ,  Marcin KULCZYK ,  Alain RICHER

IPC: B64D27/18 ,  B64F5/10 ,  G01M1/12

CPC classification number: B64D27/18 ,  B64C15/02 ,  B64F5/10 ,  G01M1/125

Abstract: 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.