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1.发明申请COMPONENT, REINFORCEMENT MEMBER, STRUCTURAL ARRANGEMENT, AIRCRAFT OR SPACECRAFT AND METHOD 有权组件，加固构件，结构安排，飞机或空间和方法公开(公告)号：US20130094898A1
公开(公告)日：2013-04-18
申请号：US13649203
申请日：2012-10-11
Applicant: Oliver SEACK , Alexander BRUNS
Inventor： Oliver SEACK , Alexander BRUNS
CPC classification number: B64C1/00 , B29C70/205 , B29C70/222 , B29C70/86 , D03D13/00 , Y02T50/43 , Y10T403/477
Abstract: A component for connecting structures to intersection regions of said component is disclosed, particularly for an aircraft or spacecraft, including a coupling element, including a first fibre which wraps around the coupling element so that the first fibre extends in a first plane in front of the coupling element and in a second plane behind the coupling element, the first and second planes intersecting, and including a second fibre which wraps around the coupling element so that the second fibre extends in a third plane in front of the coupling element and in a fourth plane behind the coupling element, the third and fourth planes intersecting, and with the first fibre portions of the first and second fibres crossing over in a first region and the second fibre portions of the first and second fibres crossing over in a second region.
Abstract translation: 公开了用于将结构连接到所述部件的交叉区域的部件，特别是对于包括耦合元件的飞行器或航天器，包括耦合元件周围的第一光纤，使得第一光纤在第一平面内延伸 耦合元件，并且在耦合元件后面的第二平面中，第一和第二平面相交，并且包括围绕耦合元件缠绕的第二光纤，使得第二光纤在耦合元件前面的第三平面中延伸，并且在第四 平面，耦合元件后面，第三和第四平面相交，并且第一和第二光纤的第一光纤部分在第一区域中交叉，第一和第二光纤的第二光纤部分在第二区域中交叉。
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2.发明申请公开(公告)号：US20150060607A1
公开(公告)日：2015-03-05
申请号：US14345054
申请日：2012-08-21
Applicant: Tamas Havar , Juan Perez-Sanchez , Tobias Ender , Oliver Seack
Inventor： Tamas Havar , Juan Perez-Sanchez , Tobias Ender , Oliver Seack
Abstract: A lift flap bearing apparatus is improved with respect to aerodynamics, construction space and assembly, for guiding and adjusting a first lift flap and a second lift flap. The lift flap bearing apparatus comprises a first guiding device for guiding the first lift flap and a second guiding device for guiding the second lift flap. The first and the second guiding devices each have a first curved guide rail and a second curved guide rail.
Abstract translation: 相对于空气动力学，建筑空间和组装，提升翼片轴承装置得到改进，用于引导和调节第一提升翼片和第二提升翼片。 提升板轴承装置包括用于引导第一提升挡板的第一引导装置和用于引导第二提升挡板的第二引导装置。 第一和第二引导装置各自具有第一弯曲导轨和第二弯曲导轨。
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公开(公告)号：US20130099062A1
公开(公告)日：2013-04-25
申请号：US13649218
申请日：2012-10-11
Applicant: Oliver SEACK , Alexander BRUNS
Inventor： Oliver SEACK , Alexander BRUNS
CPC classification number: B64C9/00 , B23P11/00 , B29C70/24 , B29C70/68 , B29L2031/3076 , B64C9/02 , D03D25/005 , D10B2505/02 , Y02T50/43 , Y10T29/49616
Abstract: The present invention pertains inter alia to a structural arrangement, comprising a box structure, a first fibre portion which extends in a first plane, a second fibre portion which extends in a second plane, the first and the second fibre portion being interconnected at a crossing point thereof, the first fibre portion comprising a first portion on one side of the crossing point and a second portion on the other side of the crossing point, the first portion being connected to a first portion of the box structure and the second portion being connected to a second portion of the box structure, the second fibre portion forming, on one side of the crossing point, an inner web inside the box structure and, on the other side of the crossing point, an outer web outside the box structure.
Abstract translation: 本发明特别涉及一种结构布置，包括盒结构，在第一平面中延伸的第一纤维部分，在第二平面中延伸的第二纤维部分，第一和第二纤维部分在交叉处互连 所述第一纤维部分包括所述交叉点的一侧上的第一部分和所述交叉点的另一侧上的第二部分，所述第一部分连接到所述盒结构的第一部分，并且所述第二部分被连接 在所述盒结构的第二部分中，所述第二纤维部分在所述交叉点的一侧上形成在所述盒结构内部的内腹板，并且在所述交叉点的另一侧上形成在所述箱结构外部的外腹板。
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4.发明授权公开(公告)号：US09452823B2
公开(公告)日：2016-09-27
申请号：US14345054
申请日：2012-08-21
Applicant: Tamas Havar , Juan Perez-Sanchez , Tobias Ender , Oliver Seack
Inventor： Tamas Havar , Juan Perez-Sanchez , Tobias Ender , Oliver Seack
Abstract: A lift flap bearing apparatus is improved with respect to aerodynamics, construction space and assembly, for guiding and adjusting a first lift flap and a second lift flap. The lift flap bearing apparatus comprises a first guiding device for guiding the first lift flap and a second guiding device for guiding the second lift flap. The first and the second guiding devices each have a first curved guide rail and a second curved guide rail.
Abstract translation: 相对于空气动力学，建筑空间和组装，提升翼片轴承装置得到改进，用于引导和调节第一提升翼片和第二提升翼片。 提升板轴承装置包括用于引导第一提升挡板的第一引导装置和用于引导第二提升挡板的第二引导装置。 第一和第二引导装置各自具有第一弯曲导轨和第二弯曲导轨。
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5.发明授权Component, reinforcement member, structural arrangement, aircraft or spacecraft and method 有权部件，加强件，结构布置，飞机或航天器及方法公开(公告)号：US08833697B2
公开(公告)日：2014-09-16
申请号：US13649203
申请日：2012-10-11
Applicant: Oliver Seack , Alexander Bruns
Inventor： Oliver Seack , Alexander Bruns
CPC classification number: B64C1/00 , B29C70/205 , B29C70/222 , B29C70/86 , D03D13/00 , Y02T50/43 , Y10T403/477
Abstract: A component for connecting structures to intersection regions of said component is disclosed, particularly for an aircraft or spacecraft, including a coupling element, including a first fiber which wraps around the coupling element so that the first fiber extends in a first plane in front of the coupling element and in a second plane behind the coupling element, the first and second planes intersecting, and including a second fiber which wraps around the coupling element so that the second fiber extends in a third plane in front of the coupling element and in a fourth plane behind the coupling element, the third and fourth planes intersecting, and with the first fiber portions of the first and second fibers crossing over in a first region and the second fiber portions of the first and second fibers crossing over in a second region.
Abstract translation: 公开了用于将结构连接到所述部件的交叉区域的部件，特别是对于包括耦合元件的飞行器或航天器，包括耦合元件周围的第一光纤，使得第一光纤在第一平面内延伸 耦合元件，并且在耦合元件后面的第二平面中，第一和第二平面相交，并且包括围绕耦合元件缠绕的第二光纤，使得第二光纤在耦合元件前面的第三平面中延伸，并且在第四 平面，耦合元件后面，第三和第四平面相交，并且第一和第二光纤的第一光纤部分在第一区域中交叉，第一和第二光纤的第二光纤部分在第二区域中交叉。
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Patent Agency Ranking
6.发明申请METHOD FOR PRODUCING A COMPONENT FOR JOINING STRUCTURES, COMPONENT AND STRUCTURAL ARRANGEMENT 有权用于生产用于接合结构，部件和结构布置的部件的方法公开(公告)号：US20130092794A1
公开(公告)日：2013-04-18
申请号：US13649213
申请日：2012-10-11
Applicant: Oliver SEACK , Alexander BRUNS
Inventor： Oliver SEACK , Alexander BRUNS
CPC classification number: D06C3/06 , B29B11/16 , B29C70/222 , B29D99/0003 , B64C1/00 , B64C3/187 , D04H3/07 , Y02T50/43
Abstract: The present invention provides a method for producing a component for joining structures at intersection regions thereof, comprising the following steps: forming a first fibre having a meandering shape which includes a plurality of first loops; forming a second fibre having a meandering shape which includes a plurality of second loops; and swivelling a first loop portion of a respective first loop and a first loop portion of a respective second loop such that a respective first loop and a respective second loop engage with one another.
Abstract translation: 本发明提供了一种用于在其交叉区域处连接结构件的部件的制造方法，包括以下步骤：形成包括多个第一回路的具有曲折形状的第一纤维; 形成具有曲折形状的第二纤维，其包括多个第二环路; 以及旋转相应的第一环的第一环部分和相应的第二环的第一环部分，使得相应的第一环和相应的第二环彼此接合。
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公开(公告)号：US08596585B2
公开(公告)日：2013-12-03
申请号：US13178533
申请日：2011-07-08
Applicant: Tamas Havar , Oliver Meyer , York C. Roth , Oliver Seack
Inventor： Tamas Havar , Oliver Meyer , York C. Roth , Oliver Seack
IPC: B64C3/50
CPC classification number: B64C9/24
Abstract: Embodiments of the invention relate to an aerodynamic body with an extension in the spanwise direction, wing chord direction and wing thickness direction for coupling to a wing of an aircraft. This aerodynamic body can here be used for a leading edge flap or slat of an aircraft wing. To improve the flow characteristics, the rear side of the aerodynamic body is provided with a skin section that can be molded between a convex curvature and concave curvature.
Abstract translation: 本发明的实施例涉及一种空气动力学主体，其在翼展方向上延伸，翼弦方向和翼厚度方向用于联接到飞行器的翼。 这种空气动力学体在这里可以用于飞机机翼的前缘皮瓣或缝翼。 为了改善流动特性，空气动力体的后侧设置有能够在凸曲率和凹曲率之间模制的皮肤部分。
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公开(公告)号：US20120061523A1
公开(公告)日：2012-03-15
申请号：US13178533
申请日：2011-07-08
Applicant: Tamas Havar , Oliver Meyer , York C. Roth , Oliver Seack
Inventor： Tamas Havar , Oliver Meyer , York C. Roth , Oliver Seack
CPC classification number: B64C9/24
Abstract: Embodiments of the invention relate to an aerodynamic body with an extension in the spanwise direction, wing chord direction and wing thickness direction for coupling to a wing of an aircraft. This aerodynamic body can here be used for a leading edge flap or slat of an aircraft wing. To improve the flow characteristics, the rear side of the aerodynamic body is provided with a skin section that can be molded between a convex curvature and concave curvature.
Abstract translation: 本发明的实施例涉及一种空气动力学主体，其在翼展方向上延伸，翼弦方向和翼厚度方向用于联接到飞行器的翼。 这种空气动力学体在这里可以用于飞机机翼的前缘皮瓣或缝翼。 为了改善流动特性，空气动力体的后侧设置有能够在凸曲率和凹曲率之间模制的皮肤部分。
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公开(公告)号：US20060113017A1
公开(公告)日：2006-06-01
申请号：US11017502
申请日：2004-12-20
Applicant: Oliver Seack
Inventor： Oliver Seack
CPC classification number: B60C17/06 , B60C17/01 , B60C17/065 , B60C2200/02 , Y10T152/10054 , Y10T152/10495
Abstract: This invention relates to a device for reducing the impact energy of tire and rim fragments, comprising a rim with pneumatic tire mounted thereto, whose cavity is filled with a gas volume, wherein a displacer connected with the rim is arranged inside the tire cavity, and the displacer does not come into contact with the tire.
Abstract translation: 本发明涉及一种用于减小轮胎和轮辋碎片冲击能量的装置，包括一个安装有充气轮胎的轮辋，其空腔充满气体体积，其中与轮辋连接的置换器设置在轮胎腔内，以及 置换器不会与轮胎接触。
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10.发明授权Method for producing a component for joining structures, component and structural arrangement 有权用于连接结构件，部件和结构布置的部件的制造方法公开(公告)号：US09523168B2
公开(公告)日：2016-12-20
申请号：US13649213
申请日：2012-10-11
Applicant: Oliver Seack , Alexander Bruns
Inventor： Oliver Seack , Alexander Bruns
CPC classification number: D06C3/06 , B29B11/16 , B29C70/222 , B29D99/0003 , B64C1/00 , B64C3/187 , D04H3/07 , Y02T50/43
Abstract: The present invention provides a method for producing a component for joining structures at intersection regions thereof, comprising the following steps: forming a first fiber having a meandering shape which includes a plurality of first loops; forming a second fibre having a meandering shape which includes a plurality of second loops; and swivelling a first loop portion of a respective first loop and a first loop portion of a respective second loop such that a respective first loop and a respective second loop engage with one another.
Abstract translation: 本发明提供了一种用于在其交叉区域处连接结构件的部件的制造方法，包括以下步骤：形成包括多个第一回路的具有曲折形状的第一纤维; 形成具有曲折形状的第二纤维，其包括多个第二环路; 以及旋转相应的第一环的第一环部分和相应的第二环的第一环部分，使得相应的第一环和相应的第二环彼此接合。
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