公开(公告)号：US10189575B2

公开(公告)日：2019-01-29

申请号：US15357106

申请日：2016-11-21

Applicant: Airbus Operations SAS

Inventor： David Ewens ,  Jonathan Blanc ,  Yves Belloc

IPC: B64D27/26 ,  B64C3/32 ,  B64D27/18

Abstract: An aircraft engine assembly including a set of rear engine attachments comprising a first shackle hinged on a bracket secured to the engine and on a bracket made as one piece with one of the two side panels, the shackle being oriented along a vertical direction, a second shackle hinged on a bracket secured to the engine and on a bracket made as one piece with the other one of the two side panels, the second shackle being oriented along the vertical direction, and a third shackle for transversally transmitting loads, inclined relative to the vertical direction and hinged on a bracket secured to the engine and on a bracket secured to the primary structure.

公开(公告)号：US10556699B2

公开(公告)日：2020-02-11

申请号：US15496183

申请日：2017-04-25

Applicant: Airbus Operations SAS

Inventor： Olivier Pautis ,  Jerome Colmagro ,  David Ewens

IPC: B64D27/14 ,  B64D27/20 ,  B64D27/26 ,  B64C11/30 ,  B64D27/12 ,  B64D27/00

Abstract: To reduce the overall mass of an engine assembly for aircraft, this assembly comprises a part of the fuselage of an aircraft, a turbomachine comprising an unfaired propeller, together with an annular row of unfaired after-guide vanes located aft of the propeller and rotationally fixed in relation to a longitudinal axis of the turbomachine, and a mounting pylon. At least part of the leading edge of the pylon is incorporated within the annular row between two after-guide vanes.

公开(公告)号：US20170152052A1

公开(公告)日：2017-06-01

申请号：US15357106

申请日：2016-11-21

Applicant: Airbus Operations SAS

Inventor： David Ewens ,  Jonathan Blanc ,  Yves Belloc

IPC: B64D27/26 ,  B64C3/32 ,  B64D27/18

CPC classification number: B64D27/26 ,  B64C3/32 ,  B64D27/18 ,  B64D2027/264 ,  B64D2027/266 ,  B64D2027/268

Abstract: An aircraft engine assembly including a set of rear engine attachments comprising a first shackle hinged on a bracket secured to the engine and on a bracket made as one piece with one of the two side panels, the shackle being oriented along a vertical direction, a second shackle hinged on a bracket secured to the engine and on a bracket made as one piece with the other one of the two side panels, the second shackle being oriented along the vertical direction, and a third shackle for transversally transmitting loads, inclined relative to the vertical direction and hinged on a bracket secured to the engine and on a bracket secured to the primary structure.