公开(公告)号：US20170313430A1

公开(公告)日：2017-11-02

申请号：US15496183

申请日：2017-04-25

Applicant: Airbus Operations SAS

Inventor： Olivier Pautis ,  Jerome Colmagro ,  David EWENS

IPC: B64D27/12 ,  B64C11/30

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.