公开(公告)号：US08245975B2

公开(公告)日：2012-08-21

申请号：US12839845

申请日：2010-07-20

Applicant: Bengt Abel ,  Klaus Edelmann ,  Arne Hartwig ,  Klaus Hoppmann ,  Jens Wleting

Inventor： Bengt Abel ,  Klaus Edelmann ,  Arne Hartwig ,  Klaus Hoppmann ,  Jens Wleting

IPC: B64C1/14

CPC classification number: B64C1/1484 ,  Y02T50/43

Abstract: The invention relates to a vehicle window consisting of a transparent composite material, wherein the composite material comprises fibers and a matrix material such that the vehicle window is capable of withstanding structural loads occurring in the window region and can substantially provide the window function even in spite of damage to the vehicle window (damage-tolerant), the fibers and the matrix material being transparent and substantially having the same refractive index. The invention proposes vehicle windows which are damage-tolerant, load bearing, cost-saving, easy to handle and require less installation space than conventional vehicle windows.

Abstract translation: 本发明涉及一种由透明复合材料组成的车窗，其中复合材料包括纤维和基体材料，使得车窗能够承受在窗口区域中发生的结构载荷，并且甚至可以基本上提供窗口功能 对车窗的损伤（耐损伤），纤维和基质材料是透明的并且基本上具有相同的折射率。 本发明提出了车辆窗口，其耐磨损，承载，节省成本，易于处理，并且比常规车辆窗户需要较少的安装空间。

公开(公告)号：US08105523B2

公开(公告)日：2012-01-31

申请号：US11921606

申请日：2006-06-20

Applicant: Klaus Edelmann ,  Jens Bold

Inventor： Klaus Edelmann ,  Jens Bold

IPC: B29C70/30

CPC classification number: B29C70/205 ,  B29C70/48 ,  B29D99/0003 ,  B64C1/061 ,  B64C1/064 ,  B64C1/065 ,  B64C2001/0072 ,  Y02T50/43

Abstract: Disclosed is a reinforcement blank, in particular a curved ring frame segment for fuselage cells of aircraft, comprising a synthetic material that is reinforced by at least one fiber laminate. The fiber laminate includes at least one full-area layer with a first fiber direction and at least one full-area layer with a second fiber direction, wherein at least one further layer with a third fiber direction is arranged in a peripheral area of the fiber laminate. This results in an orientation of the fibers in the individual layers of the fiber laminate used to reinforce the reinforcement beam that is overall suitable for the applied load, so that the reinforcement beam withstands high mechanical loads at a minimum weight.

Abstract translation: 公开了一种加强坯料，特别是用于飞行器的机身单元的弯曲环形框架段，包括由至少一个纤维层压板增强的合成材料。 纤维层叠体包括至少一个具有第一纤维方向的全区域层和至少一个具有第二纤维方向的全区域层，其中至少一个具有第三纤维方向的另外的层被布置在纤维的周边区域中 层压板。 这导致用于增强整体适用于施加载荷的加强梁的纤维层压板的各层中的纤维的取向，使得加强梁以最小的重量承受高机械载荷。

公开(公告)号：US06564931B1

公开(公告)日：2003-05-20

申请号：US09856715

申请日：2001-05-25

Applicant: Klaus Edelmann

Inventor： Klaus Edelmann

IPC: B65G1502

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

Abstract: The invention relates to a belt conveyor comprising a revolving conveyor belt (1, 1′), carrying rollers (2, 2′) which are positioned between the upper strand (3) and the lower strand (4, 4′) of the conveyor belt (1), a drive device and a power-transmitting unit (5, 5′) for moving the conveyor belt (1). Damage to the surface of the conveyor belt of the belt conveyor by the power transmitting device is largely excluded by the fact that for power transmission a pair of elements (6, 6′, 7) is provided for which cooperate in a positive-fit and in that the one element (6, 6′) is assigned to the power-transmitting device (5, 5′) and the other element (7) to the conveyor belt (1).

Abstract translation: 本发明涉及一种带式输送机，其包括旋转输送带（1,1'），该输送带承载辊（2,2'），辊（2'，2'）位于输送机的上股线（3）和下股（4,4'）之间 皮带（1），用于移动传送带（1）的驱动装置和动力传递单元（5,5'）。 通过动力传递装置对带式输送机的传送带的表面的损伤在很大程度上被排除在以下事实之外：对于动力传递，提供一对元件（6,6'，7），其以正向配合和 因为将一个元件（6,6'）分配给动力传递装置（5,5'），另一个元件（7）分配给传送带（1）。

公开(公告)号：US08811654B2

公开(公告)日：2014-08-19

申请号：US13524354

申请日：2012-06-15

Applicant: Tanja Frese ,  Klaus Edelmann

Inventor： Tanja Frese ,  Klaus Edelmann

IPC: G06K9/00

CPC classification number: G01N21/95 ,  G01N2021/8427 ,  G01N2021/8472 ,  G01N2021/8477

Abstract: A non-destructive determination of material characteristics of an aircraft component is provided. To provide a simple determination of material characteristics, which can be implemented economically, it is provided to make available image data of a layer, which can be detected from outside using electromagnetic radiation, of a workpiece to be examined; to detect first areas having a first pixel characteristic using the image data; and to detect second areas having a second pixel characteristic using the image data; the first pixel characteristic being associated with a fiber inlay of a fiber composite layer; and the second pixel characteristic being associated with an at least part-crystalline thermoplastic polymer of the fiber composite layer, which thermoplastic polymer is in a crystalline state; and to determine a relationship of the first areas to the second areas.

Abstract translation: 提供了对飞行器部件的材料特性的非破坏性测定。 为了提供可以经济实现的材料特性的简单确定，提供了使得可以从外部使用电磁辐射检测待检测的工件的层的可用图像数据; 使用所述图像数据来检测具有第一像素特性的第一区域; 并且使用所述图像数据来检测具有第二像素特性的第二区域; 所述第一像素特性与纤维复合层的纤维镶嵌相关联; 并且所述第二像素特征与所述纤维复合层的至少部分结晶的热塑性聚合物相关联，所述热塑性聚合物处于结晶状态; 并确定第一个区域与第二个区域的关系。

公开(公告)号：US20110001010A1

公开(公告)日：2011-01-06

申请号：US12742206

申请日：2008-11-13

Applicant: Stefan Tacke ,  Thorsten Roming ,  Klaus Edelmann

Inventor： Stefan Tacke ,  Thorsten Roming ,  Klaus Edelmann

IPC: B64C1/06

CPC classification number: B64C1/061 ,  B64C1/069 ,  B64C2001/0081

Abstract: A coupling element for connecting stringers in the process of joining two fuselage sections by means of at least one transverse splicing plate, wherein in each case the fuselage sections on the inside comprise a multitude of stringers arranged on fuselage skins, as well as annular frame elements, wherein the coupling element comprises a base flange and a frame element flange, and by way of the coupling element in each case a connection between the opposing stringers, the annular frame element and the fuselage skins or the transverse splicing plate takes place so that the coupling element beyond a connection of the stringer base also supports the connection of stringers on the flank side.

Abstract translation: 一种用于在通过至少一个横向拼接板连接两个机身部分的过程中连接桁条的联接元件，其中在每种情况下，内侧的机身部分包括布置在机身外壳上的多个桁条以及环形框架元件 ，其中所述联接元件包括底部凸缘和框架元件凸缘，并且通过所述联接元件，在每种情况下，相对的纵梁之间的连接，所述环形框架元件和机身外壳或横向拼接板发生，使得 连接元件超过桁条基座的连接，也支撑在侧面上的桁条的连接。

公开(公告)号：US20100175966A1

公开(公告)日：2010-07-15

申请号：US12520228

申请日：2007-12-18

Applicant: Klaus Edelmann ,  Helge Ehrhardt-Caspers

Inventor： Klaus Edelmann ,  Helge Ehrhardt-Caspers

IPC: B65G47/64 ,  B65G47/80

CPC classification number: B65G47/648 ,  B65G47/71 ,  B65G47/80

Abstract: An apparatus for distributing goods delivered on one or more feeding conveyor belts onto two or more removal conveyor belts, wherein the feeding conveyor belts as well as the removal conveyor belts are subdivided into a plurality of individual conveyor belts which are arranged in parallel side by side and are driven jointly. A rotary table having an essentially circular contour and also comprising a plurality of parallel individual conveyor belts which are also allocated to a joint drive is positioned between the feeding and the removal conveyor belts, wherein the feeding and the individual removal conveyor belts each closely reach up to the individual conveyor belts of the rotary table and are, in essence, adjusted in their length to the circular contour of the rotary table

Abstract translation: 一种用于将在一个或多个进料输送带上输送的货物分配到两个或更多个去除输送带上的装置，其中进料输送带以及拆卸输送带被细分成多个单独的输送带，它们并排布置 并共同推动。 具有基本上圆形轮廓并且还包括多个平行的单独传送带（其也被分配到接合传动装置）的旋转台被定位在进给和移除输送带之间，其中进给和各个拆卸输送带各自接近 到旋转工作台的各个输送带上，其本质上被调整到旋转台的圆形轮廓

公开(公告)号：US07014806B2

公开(公告)日：2006-03-21

申请号：US10385286

申请日：2003-03-10

Applicant: Klaus Edelmann ,  Christian Weimer

Inventor： Klaus Edelmann ,  Christian Weimer

IPC: B29C70/24

CPC classification number: D04H1/4218 ,  B29C70/222 ,  B29C70/30 ,  B29C70/543 ,  B29L2031/005 ,  B64C1/1484 ,  D04C1/06 ,  D04H1/4242 ,  D04H1/44 ,  D04H13/00 ,  D10B2505/02 ,  Y02T50/43

Abstract: A closed ring fiber reinforced frame structure is produced by first preparing a prepreg. A section of the prepreg is formed into a flange preferably after impregnation by folding the flange section along a folding line. The folding line is formed by securing a deformable or drapable fiber ribbon material, for example by sewing or stitching to a carrier substrate which is preferably also a fiber material. The sewing seam or stitching line becomes the folding line. The ribbon material is so secured to the carrier substrate that the fiber orientation of the ribbon material is uniformly distributed all around a ring component that is formed of the ribbon material on the substrate. The impregnated ring component with its substrate is then cured after the folding of the flange to complete the ring frame structure.

公开(公告)号：US08895112B2

公开(公告)日：2014-11-25

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: B05D1/04 ,  B05D1/06 ,  F16J15/10 ,  C09D5/03 ,  B05B5/03

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：US08800928B2

公开(公告)日：2014-08-12

申请号：US13384033

申请日：2010-07-15

Applicant: Thorsten Roming ,  Hansjörg Horneber ,  Thorsten Schröer ,  Tobias Wirtz ,  Klaus Edelmann ,  Tanja Menken (Frese)

Inventor： Thorsten Roming ,  Hansjörg Horneber ,  Thorsten Schröer ,  Tobias Wirtz ,  Klaus Edelmann ,  Tanja Menken (Frese)

IPC: B64C1/12

CPC classification number: B64C1/061 ,  B64C1/068 ,  B64C1/12

Abstract: The invention concerns a shell segment for the purpose of manufacturing a fuselage cell section for a fuselage cell of an aeroplane, with at least one skin field and with a multiplicity of longitudinal stiffeners arranged thereon, in particular stringers, and also at least one transverse stiffening element running transverse to the longitudinal stiffeners, in particular at least one frame.In that the connection of the at least one transverse stiffening element to the at least one skin field is undertaken with at least one connecting bracket wherein the at least one connecting bracket has at least one corrugation, the supporting brackets for purposes of absorbing tilting moments of the frames, in forms of embodiment of shell segments of prior known art, can be omitted. By this means a considerable weight reduction is possible with, at the same time, a reduced production effort.

Abstract translation: 本发明涉及一种用于制造用于飞机的机身单元的机身单元部分的壳段，其具有布置在其上的至少一个皮肤区域和多个纵向加强件，特别是桁条，以及至少一个横向加强件 元件横向于纵向加强件，特别是至少一个框架。 由于至少一个横向加强元件与至少一个皮肤区域的连接是用至少一个连接支架进行的，其中至少一个连接支架具有至少一个波纹，所述支撑托架用于吸收倾斜力矩 可以省略以现有技术的壳段的实施例的框架。 通过这种方式，相当可观的重量减轻是可能的，同时减少了生产力。

公开(公告)号：US20120170051A1

公开(公告)日：2012-07-05

申请号：US13403386

申请日：2012-02-23

Applicant: Klaus Edelmann ,  Tanja Frese ,  Carsten Brandt ,  Jens Kethler ,  Christoph Von Kopylow

Inventor： Klaus Edelmann ,  Tanja Frese ,  Carsten Brandt ,  Jens Kethler ,  Christoph Von Kopylow

IPC: G01B11/30

CPC classification number: G01B11/25 ,  G01B11/303 ,  G01N15/088

Abstract: A method and a device for inspecting the quality of a formed thermoplastic fiber-reinforced plastic component wherein the component is tested by means of a sensor unit with a downstream electronic evaluation unit for analysis of the measuring result acquired by sensor technology by means of sample comparison, wherein by means of the optical sensor unit the surface roughness of the plastic component is measured after forming, which surface roughness is analyzed by means of the evaluation unit by a comparison with a stored reference pattern in such a manner that increased surface roughness is interpreted as increased internal materials porosity.

Abstract translation: 一种用于检查成形的热塑性纤维增强塑料部件的质量的方法和装置，其中通过具有下游电子评估单元的传感器单元测试该部件，用于通过样品比较来分析由传感器技术获得的测量结果 其中通过光学传感器单元，在成形之后测量塑料部件的表面粗糙度，通过与存储的参考图案进行比较，借助于评估单元来分析表面粗糙度，使得增加的表面粗糙度被解释 随着内部材料孔隙度的增加。