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11. 发明申请

US20150082708A1 COVER PLATE AND DOOR ARRANGEMENT FOR A MEANS OF TRANSPORTATION 审中-公开
标题翻译：运输方式的盖板和门装置
公开(公告)号：US20150082708A1
公开(公告)日：2015-03-26
申请号：US14489017
申请日：2014-09-17
申请人： Airbus Operations GmbH
发明人： Wolfgang Eilken , Matthias Hegenbart , Memis Tiryaki , Dirk Elbracht , Leonard Rahmel
IPC分类号： B64C1/14
CPC分类号： B64C1/14 , B64C1/1407 , B64C7/00
摘要： A cover plate for covering a door clearance between a skin of a means of transportation and a door as well as a door arrangement with such a cover plate is proposed. The cover plate includes a mounting region for permanently fastening the cover plate on the door; a covering region for covering the door clearance; and a fastening device that is designed for fixing the covering region on the skin when the door is closed.
摘要翻译：提出了一种用于覆盖运输工具的皮肤和门之间的门间隙的盖板以及具有这种盖板的门装置。盖板包括用于将盖板永久地固定在门上的安装区域; 用于覆盖门间隙的覆盖区域; 以及紧固装置，其被设计成当门关闭时将覆盖区域固定在皮肤上。

12. 发明申请

US20140151504A1 Aircraft fuselage structure and method 有权
标题翻译：飞机机身结构与方法
公开(公告)号：US20140151504A1
公开(公告)日：2014-06-05
申请号：US14084692
申请日：2013-11-20
申请人： AIRBUS OPERATIONS GMBH
发明人： Magdalena Boyen , Wolfgang Eilken , Wolfgang Schulze
IPC分类号： B64C1/06 , B64F5/00
CPC分类号： B64C1/069 , B64C1/061 , B64C1/068 , B64C2001/0081 , B64F5/10 , Y10T29/49622
摘要： An aircraft fuselage structure having a first fuselage barrel section and a second fuselage section barrel which are joined by tension fasteners extending through frame holes. A shank diameter of the fasteners is smaller than a respective frame hole diameter. A first positive locking element and a second positive locking element is provided forming a form-fit area with the first positive locking element in the circumferential direction. A method for producing such an aircraft fuselage section is also provided.
摘要翻译：具有第一机身筒部和第二机身部筒的飞机机身结构，其通过延伸穿过框架孔的张力紧固件连接。紧固件的柄直径小于相应的机架孔直径。提供了第一正锁定元件和第二正锁定元件，其在圆周方向上与第一正锁定元件形成形状配合区域。还提供了一种生产这种飞机机身部分的方法。

13. 发明授权

US11685504B2 Shell arrangement for a fuselage of an aircraft and fuselage for an aircraft 有权
公开(公告)号：US11685504B2
公开(公告)日：2023-06-27
申请号：US16881819
申请日：2020-05-22
申请人： Airbus Operations GmbH
发明人： Wolfgang Eilken , Wolfgang Schulze , Christoph Schweim , Patrick Brusberg
IPC分类号： B64C1/06 , B29C65/00 , B64C1/12 , B29L31/30 , B64C1/00
CPC分类号： B64C1/069 , B29C66/1122 , B64C1/12 , B29L2031/3082 , B64C2001/0045
摘要： A shell arrangement for a fuselage of an aircraft includes a first shell portion extending in a curved manner in a shell peripheral direction and a second shell portion extending in a curved manner in the shell peripheral direction, wherein, in an overlapping portion of the shell arrangement, a first end region of the first shell portion and a second end region of the second shell portion overlap each other in the shell peripheral direction and a first outer face of the first shell portion and a second inner face of the second shell portion are adhesively bonded to each other by an adhesive layer, and wherein an edge of the first shell portion which terminates the first end region with respect to the shell peripheral direction extends in the overlapping portion in an undulating manner in a shell longitudinal direction which extends transversely relative to the shell peripheral direction.

14. 发明授权

US11623729B2 Method for producing a crossmember for a vehicle and a crossmember for a vehicle 有权
公开(公告)号：US11623729B2
公开(公告)日：2023-04-11
申请号：US16424315
申请日：2019-05-28
申请人： Airbus Operations GmbH
发明人： Torsten Noebel , Wolfgang Eilken , Wolfgang Schulze , Memis Tiryaki
IPC分类号： B64C1/18 , B64F5/10
摘要： A method for producing a crossmember for a vehicle prepares a workpiece having different thicknesses and a preliminary contour from a metal sheet of uniform thickness by flat roll forming to achieve different local thicknesses. The method cuts out the workpiece, and bending roll forms the workpiece to form a crossmember with a cross section having at least two flanges opposite one another, and a web situated between said flanges. The distance between the flanges is not constant along a longitudinal extent of the crossmember, and a thickness profile at least of the web is determined by the flat roll forming. The local thicknesses and the preliminary contour are such that a geometrical shape of the crossmember corresponds to a predetermined geometrical shape with different thicknesses and heights of the web and differently shaped regions of the flanges along the longitudinal extent of the crossmember.

15. 发明授权

US11052991B2 Fairing for an aircraft 有权
公开(公告)号：US11052991B2
公开(公告)日：2021-07-06
申请号：US15801536
申请日：2017-11-02
申请人： Airbus Operations GmbH
发明人： Wolfgang Eilken , Memis Tiryaki , Klaus-Peter Sanmann , Ghasem Moussavi
IPC分类号： B64C7/00 , F16J15/02 , B64C5/06
摘要： A fairing for an aircraft is disclosed in which the fairing comprises a first fairing portion configured to be fixedly attached to a first structural component and having a first edge; a second fairing portion configured to be fixedly attached to a second structural component and having a second edge, wherein the first edge and the second edge define an interface configured to enable relative movement between the first fairing portion and the second fairing portion.

16. 发明授权

US11034455B2 Rail systems for fixing fittings in a cabin of a vehicle 有权
公开(公告)号：US11034455B2
公开(公告)日：2021-06-15
申请号：US16574607
申请日：2019-09-18
申请人： Airbus Operations GmbH
发明人： Sven Werner , Andre Zybala , Wolfgang Eilken , Memis Tiryaki
IPC分类号： B64D11/06
摘要： A rail system for fixing fittings in a cabin of a vehicle includes a first elongate rail body with a fixing side for fixing to a vehicle structure, an opposite support side with a support surface for receiving fittings, and a rail cross-section extending between the fixing side and the support side, and several fixing inserts which can be fixed along the support surface. The rail cross-section has two mutually opposing legs which are spaced apart from each other and run perpendicularly to the support surface, and the fixing inserts are configured so as not to protrude beyond the support surface.

17. 发明申请

US20170096214A1 VORTEX GENERATOR ARRANGEMENT, FLOW CONTROL SYSTEM AND METHOD FOR CONTROLLING A FLOW ON A RUDDER SURFACE 审中-公开
公开(公告)号：US20170096214A1
公开(公告)日：2017-04-06
申请号：US15274197
申请日：2016-09-23
申请人： Airbus Operations GmbH
发明人： Bruno Stefes , Wolfgang Eilken , Erich Paul
IPC分类号： B64C23/06 , B64C13/16 , B64C5/06
CPC分类号： B64C23/06 , B64C5/06 , B64C9/02 , B64C13/16 , Y02T50/162
摘要： A vortex generator arrangement for an aircraft comprising a surface section forming a flow surface interacting with a flow surrounding the aircraft in operation, wherein the surface section comprises an opening, a vortex generator movable between a retracted position and an extended position, a retainer for holding the vortex generator in the retracted position, a biasing structure for biasing the vortex generator towards the extended position and a release for releasing the vortex generator from the retainer such that the vortex generator can be moved towards the extended position. Further, a sealing membrane is provided completely sealing the opening when the vortex generator is in the retracted position. The vortex generator is movable through the membrane from the retracted position to the extended position. Furthermore, a flow control system, an aircraft and a method of controlling flow are described and claimed.

18. 发明授权

US09567057B2 Aircraft fuselage structure and method 有权
标题翻译：飞机机身结构与方法
公开(公告)号：US09567057B2
公开(公告)日：2017-02-14
申请号：US14084692
申请日：2013-11-20
申请人： Airbus Operations GmbH
发明人： Magdalena Boyen , Wolfgang Eilken , Wolfgang Schulze
IPC分类号： B64C1/06 , B64F5/00 , B64C1/00
CPC分类号： B64C1/069 , B64C1/061 , B64C1/068 , B64C2001/0081 , B64F5/10 , Y10T29/49622
摘要： An aircraft fuselage structure having a first fuselage barrel section and a second fuselage section barrel which are joined by tension fasteners extending through frame holes. A shank diameter of the fasteners is smaller than a respective frame hole diameter. A first positive locking element and a second positive locking element is provided forming a form-fit area with the first positive locking element in the circumferential direction. A method for producing such an aircraft fuselage section is also provided.
摘要翻译：具有第一机身筒部和第二机身部筒的飞机机身结构，其通过延伸穿过框架孔的张力紧固件连接。紧固件的柄直径小于相应的机架孔直径。提供了第一正锁定元件和第二正锁定元件，其在圆周方向上与第一正锁定元件形成形状配合区域。还提供了一种生产这种飞机机身部分的方法。

19. 发明授权

US09511845B2 Aircraft frame 有权
标题翻译：飞机架
公开(公告)号：US09511845B2
公开(公告)日：2016-12-06
申请号：US14163406
申请日：2014-01-24
申请人： Airbus Operations GmbH
发明人： Magdalena Boyen , Wolfgang Eilken , Wolfgang Schulze
IPC分类号： B64C1/06 , B29C67/00 , B64C1/10
CPC分类号： B64C1/061 , B29C64/00 , B29C67/0051 , B64C1/064 , B64C1/069 , B64C1/10 , Y10T29/49826
摘要： An aircraft frame includes a first partial aircraft frame configured to be attached to a first aircraft fuselage segment, and a second partial aircraft frame configured to be attached to a second aircraft fuselage segment. The first and second partial aircraft frames include corresponding first and second stringer coupling sections. The first partial aircraft frame and the second partial aircraft frame are configured to be attached to each other via a first web and a second web. The first stringer coupling section is located between the first inner flange and the first outer flange and the second stringer coupling section is located between the second inner flange and the second outer flange. The first stringer coupling section includes a first wall which extends from the first web into the first section of the first partial aircraft frame, and the second stringer coupling section comprises a second wall, which extends from the second web into the second section of the second partial aircraft frame.
摘要翻译：飞机框架包括构造成附接到第一飞行器机身段的第一部分飞机框架和被配置为附接到第二飞行器机身段的第二部分飞机框架。第一和第二部分飞行器架包括对应的第一和第二纵梁联接部分。第一部分飞行器架和第二部分飞行器架被构造成经由第一腹板和第二腹板相互连接。第一纵梁联接部分位于第一内凸缘和第一外凸缘之间，第二纵梁联接部分位于第二内凸缘和第二外凸缘之间。第一纵梁联接部分包括从第一腹板延伸到第一部分飞行器框架的第一部分中的第一壁，并且第二纵梁联接部分包括第二壁，第二壁从第二腹板延伸到第二部分的第二部分部分飞机架。

20. 发明授权

US09279439B2 Attachment arrangement, a connecting device, and also a method 有权
公开(公告)号：US09279439B2
公开(公告)日：2016-03-08
申请号：US13662655
申请日：2012-10-29
申请人： Airbus Operations GmbH
发明人： Wolfgang Eilken , Memis Tiryaki , Daniel Sauer
IPC分类号： F16B7/00 , H02G3/30 , F16B5/06 , F16B21/09
CPC分类号： F16B7/00 , F16B5/0628 , F16B21/09 , H02G3/30 , Y10T29/49947 , Y10T403/32008
摘要： An attachment arrangement for attaching a component to a base item, with at least one fixing device for fixing one section of the component on a section of the base item. At least one connecting device with a connecting element and at least one receiving element are provided. One of the elements is arranged on a component section and the other of the elements is arranged on a base item section. The two elements detachably engage with one another in a form fit. Loads can be transferred at least in the direction of a first axis, and a relative movement is possible between the elements in the direction of a second axis, different from the first axis. A connecting device is disclosed for such an attachment arrangement. A method is disclosed for purposes of attaching a component to a base item by means of such an attachment arrangement.

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