公开(公告)号：US08454878B2

公开(公告)日：2013-06-04

申请号：US12906543

申请日：2010-10-18

Applicant: Marc Bochinger ,  Klaus Edelmann ,  Thomas Lange ,  Tanja Frese ,  Sven Sperling ,  Eugen Tschakrow ,  Tobias Wirtz

Inventor： Marc Bochinger ,  Klaus Edelmann ,  Thomas Lange ,  Tanja Frese ,  Sven Sperling ,  Eugen Tschakrow ,  Tobias Wirtz

IPC: B27N3/18

CPC classification number: B29C70/345 ,  B29C51/082 ,  B29C51/262 ,  B29C53/04 ,  B29C70/541 ,  B29K2101/12 ,  B29K2707/04 ,  B29L2031/3082 ,  Y02T50/43

Abstract: The invention relates to a device for the production of an angle for connecting a fuselage cell skin to an annular former and/or a stringer inside a fuselage cell structure of an aircraft, the angle taking place by the one-step deformation of an initially planar blank along at least three fold lines in a uniaxial compression molding device. A mounting frame with hinges is arranged in the compression molding device, the blank to be deformed being accommodated along the edges preferably by means of a plurality of peripherally arranged springs. A deformation of the blank into an auto-stabilized angle is possible in one step while simultaneously ensuring interlaminar slide. Due to the constructively conditioned auto-stabilization of the angle, additional components which increase the weight and the assembly effort (so-called “stabilos”) in the connection region between fuselage cell skin, stringers and annular formers inside a fuselage structure of an aircraft are unnecessary.

Abstract translation: 本发明涉及一种用于生产用于将机身细胞皮肤连接到飞机的机身单元结构内的环形成形器和/或纵梁的角度的装置，该角度通过初始平面的一步变形而发生 在单轴压缩成型装置中沿着至少三条折线的坯料。 具有铰链的安装框架布置在压缩模制装置中，待变形的坯件优选地通过多个外围布置的弹簧沿边缘容纳。 将坯料变形为自动稳定的角度是可能的，同时确保层间滑动。 由于角度的建构性调节自动稳定，在机身机身结构内的机身细胞皮肤，桁条和环形成形器之间的连接区域中增加了重量和装配力（所谓的“稳定”）的附加部件 是不必要的

公开(公告)号：US20110159229A1

公开(公告)日：2011-06-30

申请号：US12980405

申请日：2010-12-29

Applicant: Guenter Doehle ,  Klaus Edelmann ,  Hans-Juergen Weber

Inventor： Guenter Doehle ,  Klaus Edelmann ,  Hans-Juergen Weber

IPC: B32B3/08 ,  B05D7/24 ,  B05B5/025 ,  B82Y30/00

CPC classification number: F16J15/108 ,  B05B5/032 ,  B05D1/04 ,  C09D5/03

Abstract: A method for edge sealing a fiber-reinforced component formed from a carbon fiber-reinforced thermoplastic or duroplastic plastic material includes electrostatic coating of at least one section of an edge of the component with a thermoplastic powder so as to form a powder coating; and fusing and cross-linking the powder coating in a furnace so as to create a smooth edge seal.

Abstract translation: 用于边缘密封由碳纤维增强的热塑性塑料或塑性塑料材料形成的纤维增强部件的方法包括用热塑性粉末静电涂覆部件边缘的至少一部分以形成粉末涂层; 并在炉中熔融和交联粉末涂层，以形成平滑的边缘密封。

公开(公告)号：US20110155854A1

公开(公告)日：2011-06-30

申请号：US12980394

申请日：2010-12-29

Applicant: Patrick Bakker ,  Frank Brueggemann ,  Klaus Edelmann ,  Guenter Hoppe

Inventor： Patrick Bakker ,  Frank Brueggemann ,  Klaus Edelmann ,  Guenter Hoppe

IPC: B64C1/12 ,  B29C45/14 ,  B32B3/02

CPC classification number: B64C1/12 ,  B29C45/14221 ,  B29C45/14786 ,  B29C70/46 ,  B29C2045/14237 ,  B29K2105/12 ,  B29L2031/3082 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10T428/24488 ,  Y10T428/24777

Abstract: A method for the manufacture of a fiber-reinforced component includes heating a blank of a carbon-fiber-reinforced thermoplastic plastic material to at least a melting temperature of the thermoplastic plastic material; introducing the blank into an at least two-part moulding tool; forming the fiber-reinforced component by applying pressure on the blank using the moulding tool; and injecting a further thermoplastic plastic material into at least one edge region of the moulding tool so as to form an edge seal.

Abstract translation: 一种制造纤维增强部件的方法包括将碳纤维增强热塑性塑料材料坯料加热至至少热塑性塑料材料的熔化温度; 将坯料引入至少两部分的成型工具中; 通过使用成型工具对坯料施加压力来形成纤维增强部件; 以及将另外的热塑性塑料材料注射到所述模制工具的至少一个边缘区域中，以便形成边缘密封。

公开(公告)号：US07922853B2

公开(公告)日：2011-04-12

申请号：US12693794

申请日：2010-01-26

Applicant: Klaus Edelmann ,  Tanja Frese ,  Timo Stoeven ,  Tobias Wirtz

Inventor： Klaus Edelmann ,  Tanja Frese ,  Timo Stoeven ,  Tobias Wirtz

IPC: B29C53/06

CPC classification number: B29C53/04 ,  B29C70/222 ,  B29C70/345 ,  B29C2793/0081 ,  B29K2071/00 ,  B29K2081/04 ,  B29K2101/12 ,  B29K2277/10 ,  B29K2707/04 ,  B29K2709/08 ,  B29L2009/00 ,  B29L2031/3076 ,  Y02T50/43 ,  Y10T156/1036

Abstract: The invention relates to a method for producing a component for connecting a fuselage cell skin to an annular rib of an aircraft, wherein the component is formed by bending of a flat blank along at last two edge lines and wherein the blank is formed by a CFRP.According to the invention the interlaminar sliding of the fiber layers is largely completed in a first forming step, while in a second forming step a consolidation of the component takes place by the use of pressure from the press on all sides by means of an upper tool and a lower tool. This enables complex components with at least two edge lines to be produced, which edge lines run at angles of approximately, preferably at angles of 309° to 90°, to each other, and which edge lines also lie in at least two different planes.

Abstract translation: 本发明涉及一种用于生产用于将机身细胞皮肤连接到飞行器的环形肋的部件的方法，其中所述部件通过沿着最后两条边缘线弯曲扁平坯料而形成，并且其中所述坯料由CFRP形成 。 根据本发明，纤维层的层间滑动在第一成形步骤中大部分完成，而在第二成形步骤中，通过使用来自压力机的压力，通过上部工具 和一个较低的工具。 这使得能够产生具有至少两条边缘线的复杂部件，哪些边缘线彼此以大致角度（优选地为309°至90°）的角度延伸，并且哪些边缘线也位于至少两个不同的平面中。

公开(公告)号：US20100186882A1

公开(公告)日：2010-07-29

申请号：US12693794

申请日：2010-01-26

Applicant: Klaus Edelmann ,  Tanja Frese ,  Timo Stoeven ,  Tobias Wirtz

Inventor： Klaus Edelmann ,  Tanja Frese ,  Timo Stoeven ,  Tobias Wirtz

IPC: B29C53/06

CPC classification number: B29C53/04 ,  B29C70/222 ,  B29C70/345 ,  B29C2793/0081 ,  B29K2071/00 ,  B29K2081/04 ,  B29K2101/12 ,  B29K2277/10 ,  B29K2707/04 ,  B29K2709/08 ,  B29L2009/00 ,  B29L2031/3076 ,  Y02T50/43 ,  Y10T156/1036

Abstract: The invention relates to a method for producing a component for connecting a fuselage cell skin to an annular rib of an aircraft, wherein the component is formed by bending of a flat blank along at last two edge lines and wherein the blank is formed by a CFRP.According to the invention the interlaminar sliding of the fibre layers is largely completed in a first forming step, whilst in a second forming step a consolidation of the component takes place by the use of pressure from the press on all sides by means of an upper tool and a lower tool. This enables complex components with at least two edge lines to be produced, which edge lines run at angles of approximately, preferably at angles of 309° to 90°, to each other, and which edge lines also lie in at least two different planes.

Abstract translation: 本发明涉及一种用于生产用于将机身细胞皮肤连接到飞行器的环形肋的部件的方法，其中所述部件通过沿着最后两条边缘线弯曲扁平坯料而形成，并且其中所述坯料由CFRP形成 。 根据本发明，纤维层的层间滑动在第一成形步骤中大部分完成，而在第二成形步骤中，组件的固结是通过使用来自压力机的压力通过上部工具 和一个较低的工具。 这使得能够产生具有至少两条边缘线的复杂部件，哪些边缘线彼此以大致角度（优选地为309°至90°）的角度延伸，并且哪些边缘线也位于至少两个不同的平面中。

公开(公告)号：US06346057B1

公开(公告)日：2002-02-12

申请号：US09449374

申请日：1999-11-24

Applicant: Klaus Edelmann

Inventor： Klaus Edelmann

IPC: F16H712

CPC classification number: B65G23/12 ,  B65G15/02 ,  B65G2201/02 ,  B65G2201/04

Abstract: For securing the position of the conveyor belt when starting the belt under load, a belt tensioning device, has a circulating conveyor belt, carrying idlers arranged between the carrying run and the return run of the conveyor belt, a drive mechanism, a power transmission device for moving the conveyor belt, a gear ring and a toothed belt for power transmission, the gear ring being allocated to the power transmission device and the toothed belt being allocated to the conveyor belt, wherein a guiding component part adapted to the edge area of the circulating conveyor belt and a contacting component part for direct contact with the surface of the conveyor belt are provided, and wherein the contacting component part is arranged inside the guiding component part.

Abstract translation: 为了在负载下启动带时固定输送带的位置，带张紧装置具有循环输送带，承载惰轮设置在输送带和输送带的回程之间，驱动机构，动力传递装置 用于移动输送带，齿圈和用于动力传递的齿形带，齿轮环被分配给动力传递装置，齿形带被分配给传送带，其中，引导部件适合于 提供循环输送带和用于与输送带表面直接接触的接触部件，其中接触部件布置在引导部件内部。