公开(公告)号：US10351254B2

公开(公告)日：2019-07-16

申请号：US15292173

申请日：2016-10-13

Applicant: Airbus Operations S.A.S.

Inventor： Frederic Journade ,  Eric Bouchet ,  Gerard Coudouent ,  Bogdan Sina ,  Romain Terral ,  Sylvain Cros ,  Jerome Puech ,  Cyrielle Rogeron

IPC: B64D27/26 ,  B64C1/06

Abstract: An aircraft engine pylon includes two side panels and an upper stringer and a lower stringer assembled to form a strut assembly extending in a longitudinal direction (AX) corresponding to the direction in which the aircraft is moving and an internal reinforcement structure including a plurality of reinforcements. The pylon also includes a reinforcement zone on each side panel and a front housing to receive a main front center reinforcement and a rear housing to receive a main rear center reinforcement.

公开(公告)号：US20170106990A1

公开(公告)日：2017-04-20

申请号：US15292173

申请日：2016-10-13

Applicant: Airbus Operations S.A.S.

Inventor： Frederic Journade ,  Eric Bouchet ,  Gerard Coudouent ,  Bogdan Sina ,  Romain Terral ,  Sylvain Cros ,  Jerome Puech ,  Cyrielle Rogeron

IPC: B64D27/26 ,  B64C1/06

CPC classification number: B64D27/26 ,  B64C1/064 ,  B64D2027/264 ,  B64D2027/266

Abstract: An aircraft engine pylon includes two side panels and an upper stringer and a lower stringer assembled to form a strut assembly extending in a longitudinal direction (AX) corresponding to the direction in which the aircraft is moving and an internal reinforcement structure including a plurality of reinforcements. The pylon also includes a reinforcement zone on each side panel and a front housing to receive a main front centre reinforcement and a rear housing to receive a main rear centre reinforcement.