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公开(公告)号：US10683097B2
公开(公告)日：2020-06-16
申请号：US15619722
申请日：2017-06-12
Applicant: Airbus Operations S.A.S.
Inventor： Eric Bouchet , Mélaine Chaix
Abstract: An aircraft strut includes a primary structure which includes: a top stringer, a bottom stringer, at least one transverse frame which links the top stringer to the bottom stringer, a front end wall which links a front end of the top stringer to a front end of the bottom stringer, a rear end wall which links a rear end of the top stringer to a rear end of the bottom stringer, two lateral frames arranged on either side of the transverse frame, each lateral frame having a lattice form. An aircraft includes at least one strut described herein.
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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
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.
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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
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.
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4.发明申请公开(公告)号：US20170361940A1
公开(公告)日：2017-12-21
申请号：US15619722
申请日：2017-06-12
Applicant: Airbus Operations S.A.S.
Inventor： Eric Bouchet , Mélaine Chaix
Abstract: An aircraft strut includes a primary structure which includes: a top stringer, a bottom stringer, at least one transverse frame which links the top stringer to the bottom stringer, a front end wall which links a front end of the top stringer to a front end of the bottom stringer, a rear end wall which links a rear end of the top stringer to a rear end of the bottom stringer, two lateral frames arranged on either side of the transverse frame, each lateral frame having a lattice form. An aircraft includes at least one strut described herein.
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