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.

公开(公告)号：US20180050824A1

公开(公告)日：2018-02-22

申请号：US15557705

申请日：2016-03-10

Applicant: BOMBARDIER INC.

Inventor： Laurent REGNAULT ,  Alexandros ILIOPOULOS ,  Sebastien SIROIS

IPC: B64F5/10 ,  G05B19/418

CPC classification number: B64F5/10 ,  G05B19/41805

Abstract: There are described herein methods and systems for manufacturing and/or assembling components having datum features thereon used to derive datum reference frames. The datum reference frames provided on the components may serve as both manufacturing and assembly datum reference frames.