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11.发明申请公开(公告)号：US20190262933A1
公开(公告)日：2019-08-29
申请号：US16283436
申请日：2019-02-22
Applicant: STELIA AEROSPACE
Inventor： David Chartier , Franck Darras , Yannick Wattlez
Abstract: 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：US10052976B2
公开(公告)日：2018-08-21
申请号：US14856532
申请日：2015-09-16
Applicant: STELIA AEROSPACE
Inventor： Bastien Atger , Laurent Cecinas
CPC classification number: B60N2/22 , B60N2/62 , B60N2/686 , B64D11/064
Abstract: A driving seat comprises a base and a back rest forming a support structure. The back rest is articulated onto the base about an axis of inclination of the back rest to provide an adjustable back rest inclination angle. The base comprises a rear base panel of fixed inclination and a front base panel with an adjustable base inclination angle relative to the rear base panel. The back rest comprises a lower back rest panel and an upper back rest panel with an adjustable raising angle relative to the lower back rest panel. In operation, the back rest inclination angle, the base inclination angle and the raising angle are adjustable to adapt the configuration of the seat to a working configuration, a standby configuration, a rest configuration or a crash configuration.
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公开(公告)号：US20170259318A1
公开(公告)日：2017-09-14
申请号：US15454896
申请日：2017-03-09
Applicant: STELIA AEROSPACE
Inventor： Damien Sireude , Daniel Perherin
IPC: B21D7/16
Abstract: Machine for bending at least one longitudinal cylindrical pipe, the bending machine having at least one heating module configured so as to heat a longitudinal cylindrical pipe and at least one deformation module configured so as to deform a longitudinal portion of a longitudinal cylindrical pipe in order to bend it, said heating module having a plurality of heating units, each heating unit can include a peripheral heating body defining an internal opening adapted to allow the passage of a longitudinal portion of a longitudinal cylindrical pipe to be heated.
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公开(公告)号：US11046020B2
公开(公告)日：2021-06-29
申请号：US16297336
申请日：2019-03-08
Applicant: STELIA AEROSPACE
Inventor： Romain Deruelle
Abstract: A system for producing at least one structural thermoplastic part, said structural thermoplastic part being formed from a rough part comprising reinforcing fibres immersed in a thermoplastic matrix, the structural thermoplastic part to be produced comprising an outer face and an inner face, opposite the outer face, the production system comprising at least one inflatable pressure member made of a material having a thermal resistance greater than the heating temperature, the inflatable pressure member being mounted between the first counter-mould and the second mould, the inflatable pressure member being configured to develop between the deflated idle state and an inflated state to flatten the rough part between the imprint of the first mould and the imprint of the first counter-mould so as to consolidate the rough part and to form the structural thermoplastic part.
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公开(公告)号：US10711934B2
公开(公告)日：2020-07-14
申请号：US15377739
申请日：2016-12-13
Applicant: Stelia Aerospace
Inventor： Damien Sireude
Abstract: A method for manufacturing a pipe is described, wherein the method comprises a step of fastening a second mechanical quick connection member to a rectilinear hollow tubular body, a step of positioning the rectilinear hollow tubular body in a bending machine so that the angular coding mechanism of the second mechanical quick connection member is in a reference angular position with respect to said bending machine, and a step of bending the rectilinear hollow tubular body as a function of said angular reference position.
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Patent Agency Ranking
公开(公告)号：US10647221B2
公开(公告)日：2020-05-12
申请号：US15472491
申请日：2017-03-29
Applicant: STELIA AEROSPACE
Inventor： Benoît Trillaud
Abstract: 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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17.发明申请公开(公告)号：US20190241269A1
公开(公告)日：2019-08-08
申请号：US16268998
申请日：2019-02-06
Applicant: STELIA AEROSPACE
Inventor： Gabriel MARTIN , Laurent TEXERAUD , Sylvain GONFALONE
IPC: B64D11/06
CPC classification number: B64D11/0641 , B64D11/0601 , B64D11/0604 , B64D11/0605 , B64D11/0636 , B64D11/0646
Abstract: A cabin of a vehicle for transporting passengers includes a plurality of units, each unit including a seat and a modular seat extension arranged staggered in the units. Each extension includes a shell having a front bottom and a rear opening determined by a hollow volume open towards the rear and a footrest area inside the hollow volume suitable for receiving the feet of a passenger. The shell of each extension includes an invariant portion and a modular portion located in front of the invariant portion. The modular portion making it possible during the fastening thereof to the invariant portion to obtain an extension with a length that can be modified between the opening and the bottom of the shell and, a width of passage towards the aisle between the seats and the extensions of the units is maintained constant during the use of the extensions by the passengers.
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公开(公告)号：US20190009304A1
公开(公告)日：2019-01-10
申请号：US16060898
申请日：2016-12-09
Applicant: STELIA AEROSPACE
Inventor： Antoine Voisin , Amaud Deleu , Philippe Baron
Abstract: The invention relates to a machine for measuring and sorting rivets comprising: a vessel for feeding rivets to be sorted, a plurality of trays for receiving sorted rivets, a device for conveying rivets to be sorted, optical means for acquiring images of each rivet to be sorted, a unit for processing images configured to provide at least one measurement of at least one structural feature of each rivet to be sorted, means for distributing each rivet towards a receiving tray, selected as a function of at least one measurement of at least one structural feature of said part supplied by said processing unit, each receiving tray being associated with a predetermined range of values of at least one structural feature for sorting the rivets.
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公开(公告)号：US20170297154A1
公开(公告)日：2017-10-19
申请号：US15514518
申请日：2015-09-17
Applicant: STELIA AEROSPACE
Inventor： Patrick Raballand , Mael Provin
Abstract: The invention relates to a device for clamping a blank part (10) to be machined, characterised in that it comprises a frame (20); means (21, 22, 23) for supporting the part to be machined; means (30, 31) for tightening said part (10) to be machined suitable for tightening said part (10) to be machined; controlled locking means (40, 41) with at least two states of said tightening means (30, 31), a locked state in which said tightening means (30, 31) are immobilised relative to the frame (20), and an unlocked state in which said tightening means (30, 31) are free to move relative to the frame (20), while keeping said part (10) to be machined tightened.
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公开(公告)号：US20160347438A1
公开(公告)日：2016-12-01
申请号：US15166763
申请日：2016-05-27
Applicant: STELIA AEROSPACE
Inventor： Nicolas Kawski , Olivier Vincent
CPC classification number: B64C1/064 , B64C1/08 , B64C3/182 , B64C2001/0081
Abstract: The invention relates to a single-piece stringer for an aeronautic structure, the stringer comprising a single-piece body including at least one hollow longitudinal portion so as to define an outer enclosure, said outer enclosure including a plurality of openings.
Abstract translation: 本发明涉及一种用于航空结构的单件纵梁，所述纵梁包括单件本体，所述单件本体包括至少一个中空纵向部分以便限定外壳，所述外壳包括多个开口。
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