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1.发明授权公开(公告)号：US11752570B2
公开(公告)日：2023-09-12
申请号：US16283436
申请日：2019-02-22
申请人： STELIA AEROSPACE
发明人： David Chartier , Franck Darras , Yannick Wattiez
CPC分类号： B23K20/126 , B23C3/12 , B23K20/12 , B23K20/122 , B23P23/04 , B23Q3/002 , B23Q3/005 , B23Q11/005 , B23Q11/0042 , B23C2220/20 , B23C2220/40 , B23C2255/08 , B23Q3/02 , Y10T29/5176 , Y10T409/3042 , Y10T409/304144 , Y10T409/308624
摘要： Device for machining an end of an elementary panel for its subsequent friction stir welding, the elementary panel comprising a metal body defining two opposite faces, the machining device comprising a chassis, at least two guiding members configured to guide a first face of the elementary panel, at least one machining tool mounted on the chassis, the machining tool being positioned between the two guiding members and at least one pressure member mounted on the chassis and configured to exert a pressure on a second face of the elementary panel so as to press the elementary panel against the guiding members along the horizontal reference direction.
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公开(公告)号：US20220241922A1
公开(公告)日：2022-08-04
申请号：US17620305
申请日：2020-06-22
申请人： STELIA AEROSPACE
摘要： An automated mechanical machining system for machining a metal panel comprising a first face and a second face which is on the opposite side from the first face, the automated mechanical machining system comprising at least one machining tool, at least one holding tool, a control module configured to control the machining tool and the holding tool in a coordinated manner, a matching module configured to determine simple actual machining paths TRAJr1 from, on the one hand, predetermined simple theoretical machining paths TRAJt1 and, on the other hand, measurement of the actual surface SURFr of the second face and a slope management module configured to determine sloping actual machining paths TRAJr2 from sloping theoretical machining paths TRAJt2, the simple theoretical machining paths TRAJt1 and the simple actual machining paths TRAJr1.
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3.发明申请公开(公告)号：US20210237376A1
公开(公告)日：2021-08-05
申请号：US17054009
申请日：2019-05-22
申请人： Stelia Aerospace
发明人： Pierre Magnin
摘要： A device for shaping a blank for forming a thermoplastic structural part, the blank comprising reinforcing fibres embedded in a thermoplastic matrix, said shaping device comprising a support member for supporting a blank along a longitudinal axis, at least one heating member, at least one inclination member configured to modify the inclination of at least one part of the longitudinal portion of the blank at an angle of inclination that can be parameterised with respect to the horizontal plane in a plane transverse to the longitudinal axis, and a movement system from upstream to downstream along the longitudinal axis of the heating member and of the inclination member relative to the support member so as to successively modify the inclination of a part of each longitudinal portion of the blank.
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4.发明授权公开(公告)号：US11022236B2
公开(公告)日：2021-06-01
申请号：US16772315
申请日：2018-12-03
申请人： STELIA AEROSPACE
发明人： Daniel Perherin
摘要： The invention relates to a long tubular pipe comprising an outer tube, an inner fluid-transporting tube mounted in the outer tube, and a separating member designed to transmit bending efforts between said outer tube and said inner tube when said outer tube is bent, the separating member comprising means for the longitudinal passage of fluid between the inner tube and the outer tube, the separating member comprising a first edge and a second edge together defining an assembly slot, the first edge and the second edge respectively comprising a first connecting element and a second connecting element designed to cooperate mechanically on the outer periphery of the inner tube.
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公开(公告)号：US20200017038A1
公开(公告)日：2020-01-16
申请号：US16506031
申请日：2019-07-09
申请人： STELIA AEROSPACE
发明人： Jonathan PAY , Antony PAOLY
摘要： A support for overlengths of cable bundles, includes a rear wall by which the support is fixed, an almost-toroidal cavity, at least one axial indentation, and a cover. The almost-toroidal cavity is delimited by: the rear wall; an inner wall determining a small diameter of the almost-toroidal cavity; and an outer wall determining a large diameter, greater than the small diameter, of the almost-toroidal cavity. The cover is fixed removably such that: the almost-toroidal cavity is open, on the front side of the support, over a whole length of the almost-toroidal cavity when the cover is removed and forms an almost-circular groove; and the almost-toroidal cavity is closed, except for the at least one axial indentation, when the cover is fixed. A vehicle including such a support and a method for installing a cable bundle are also provided.
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公开(公告)号：US20190241094A1
公开(公告)日：2019-08-08
申请号：US15472491
申请日：2017-03-29
申请人： STELIA AEROSPACE
发明人： Benoît TRILLAUD
CPC分类号： B60N2/01 , B60N3/001 , B64D11/0601 , B64D11/0604 , B64D11/0605 , B64D11/0641
摘要： A set includes seats, each seat includes a chair and a lateral pedestal arranged laterally on one side of the chair. The chairs and the lateral pedestals are arranged in a staggered configuration in two parallel rows. Each seat has a covering shell determining a rear surface in a rear zone of the chair and determining a front surface in a front zone of the lateral pedestal. A space between a rear surface of a front seat and a front surface of a rear seat forms a passage for an occupant of the rear seat. In a vertical cross section the rear surface and the front surface have convex profiles facing one another, a width of the passage increasing in the direction of decreasing heights from a height of minimum width, and increasing in the direction of increasing heights from the height of minimum width.
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7.发明授权公开(公告)号：US11840027B2
公开(公告)日：2023-12-12
申请号：US17054009
申请日：2019-05-22
申请人： Stelia Aerospace
发明人： Pierre Magnin
CPC分类号： B29C70/506 , B29C53/84 , B29D99/0003 , B29C70/465 , B29C2791/001 , B29K2101/12 , B29L2031/3076
摘要： A device for shaping a blank for forming a thermoplastic structural part, the blank comprising reinforcing fibres embedded in a thermoplastic matrix, said shaping device comprising a support member for supporting a blank along a longitudinal axis, at least one heating member, at least one inclination member configured to modify the inclination of at least one part of the longitudinal portion of the blank at an angle of inclination that can be parameterised with respect to the horizontal plane in a plane transverse to the longitudinal axis, and a movement system from upstream to downstream along the longitudinal axis of the heating member and of the inclination member relative to the support member so as to successively modify the inclination of a part of each longitudinal portion of the blank.
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公开(公告)号：US20220017233A1
公开(公告)日：2022-01-20
申请号：US17312372
申请日：2019-12-03
申请人： STELIA AEROSPACE
摘要： Disclosed is an instrument panel designed to be integrated into an aircraft cockpit, the instrument panel comprising a main structure, extending longitudinally and having a concave shape defining a cavity, this cavity being configured to receive a plurality of navigation command and/or control units, and at least one inner wall, configured to delimit at least two recesses each intended to receive at least one of the plurality of navigation command and/or control units, the instrument panel being characterized in that the main structure is made from a single piece made from a composite material.
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9.发明申请公开(公告)号：US20210010619A1
公开(公告)日：2021-01-14
申请号：US16772315
申请日：2018-12-03
申请人： STELIA AEROSPACE
发明人： Daniel Perherin
摘要： The invention relates to a long tubular pipe comprising an outer tube, an inner fluid-transporting tube mounted in the outer tube, and a separating member designed to transmit bending efforts between said outer tube and said inner tube when said outer tube is bent, the separating member comprising means for the longitudinal passage of fluid between the inner tube and the outer tube, the separating member comprising a first edge and a second edge together defining an assembly slot, the first edge and the second edge respectively comprising a first connecting element and a second connecting element designed to cooperate mechanically on the outer periphery of the inner tube.
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公开(公告)号：US20190291362A1
公开(公告)日：2019-09-26
申请号：US16359074
申请日：2019-03-20
申请人： Stelia Aerospace
发明人： Pierre Magnin
IPC分类号： B29C70/42
摘要： Structural thermoplastic part production device, intended to be integrated to a primary structure of an aeroplane, said structural part being formed from a draft part comprising reinforcing fibres embedded in a thermoplastic matrix, production device comprising a member for supporting a draft part, at least one heating member, at least one cooling member, at least one main compression member configured to compress the local portion of the draft part against the support member so as to decrease the porosity thereof and a system for moving the heating member, the compression member and the cooling member so as to stiffen each local portion of the draft part successively.
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