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公开(公告)号:US11661173B2
公开(公告)日:2023-05-30
申请号:US16507470
申请日:2019-07-10
Applicant: Airbus Operations S.A.S.
Inventor: Alain Porte , Francois Pons , Arnaud Bourhis , Julien Sentier
Abstract: An aircraft nacelle air intake includes sectors each having a lip forming portion, an outer panel forming portion and an inner panel forming portion. The outer panel forming portions and lip forming portions are formed by a continuous one-piece wall. At at least one junction between two adjacent sectors, an opening and a hatch are provided between the outer panel forming portions of the sectors. The inner panel forming portions and the lip forming portions of the sectors are edge to edge and fixed to each other by fixing devices accessible from the inside of the sectors and invisible from outside of the sectors. A maintenance method in which, when a zone of a sector is damaged, the sector concerned is removed as a whole and is replaced by a new of “recycled” sector is also described.
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公开(公告)号:US20200017191A1
公开(公告)日:2020-01-16
申请号:US16507470
申请日:2019-07-10
Applicant: Airbus Operations S.A.S.
Inventor: Alain Porte , Francois Pons , Arnaud Bourhis , Julien Sentier
Abstract: An aircraft nacelle air intake includes sectors each having a lip forming portion, an outer panel forming portion and an inner panel forming portion. The outer panel forming portions and lip forming portions are formed by a continuous one-piece wall. At at least one junction between two adjacent sectors, an opening and a hatch are provided between the outer panel forming portions of the sectors. The inner panel forming portions and the lip forming portions of the sectors are edge to edge and fixed to each other by fixing devices accessible from the inside of the sectors and invisible from outside of the sectors. A maintenance method in which, when a zone of a sector is damaged, the sector concerned is removed as a whole and is replaced by a new of “recycled” sector is also described.
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公开(公告)号:US09651598B2
公开(公告)日:2017-05-16
申请号:US13782778
申请日:2013-03-01
Applicant: AIRBUS OPERATIONS (S.A.S.)
Inventor: Francois Pons
CPC classification number: G01R31/00 , G01R31/1263
Abstract: A method and a device for detecting an edge glow phenomenon in a composite panel, including at least one cable for introducing current into the said composite panel, at least one current return cable, at least one insulating panel bracketed to the composite panel, and means for detecting an edge glow on an outer surface of the said composite panel.
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