公开(公告)号：EP2390514B1

公开(公告)日：2015-12-16

申请号：EP11178811.3

申请日：2008-08-12

申请人： The Boeing Company

发明人： Keener, Steven G

IPC分类号： F16B33/00 ,  B29C65/00 ,  B29C65/56

CPC分类号： F16B33/006 ,  B29C65/562 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72143 ,  B29C66/7392 ,  B29C66/73921 ,  B29C66/7394 ,  B29C66/73941 ,  B29C70/545 ,  B29K2023/06 ,  B29K2027/12 ,  B29K2027/18 ,  B29K2031/00 ,  B29K2063/00 ,  B29K2067/00 ,  B29K2067/006 ,  B29K2071/00 ,  B29K2075/00 ,  B29K2077/10 ,  B29K2079/085 ,  B29K2081/04 ,  B29K2081/06 ,  B29K2101/10 ,  B29K2101/12 ,  B29K2105/0079 ,  B29K2277/10 ,  B29K2307/00 ,  B29K2307/02 ,  B29K2309/02 ,  B29K2309/08 ,  B29K2707/04 ,  B29K2709/02 ,  B29K2709/08 ,  B29L2031/3076 ,  B29L2031/727 ,  B64F5/10 ,  F16B39/02 ,  Y10T29/49622 ,  Y10T29/49885 ,  Y10T29/49906 ,  Y10T29/49952 ,  Y10T29/49964 ,  Y10T29/4997 ,  Y10T29/53 ,  Y10T29/53709 ,  B29K2307/04

公开(公告)号：EP2578651A2

公开(公告)日：2013-04-10

申请号：EP12006945.5

申请日：2012-10-08

申请人： Airbus Operations GmbH

发明人： Schulze, Wolfgang ,  Kruse, Thomas

IPC分类号： C09J5/06 ,  B29C65/00 ,  B29C70/00 ,  B29C70/08 ,  B29C70/84 ,  B32B27/12

CPC分类号： B29C65/564 ,  B29C65/483 ,  B29C65/4835 ,  B29C65/488 ,  B29C65/4885 ,  B29C65/5057 ,  B29C65/5092 ,  B29C65/72 ,  B29C65/8276 ,  B29C66/02245 ,  B29C66/0246 ,  B29C66/1122 ,  B29C66/43 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/73921 ,  B29C66/73941 ,  B29C66/83421 ,  B29C70/84 ,  B64C1/00 ,  C08K3/04 ,  C08K3/041 ,  C08K7/06 ,  C08K2201/001 ,  C09J5/02 ,  C09J5/06 ,  C09J7/10 ,  C09J9/02 ,  C09J11/04 ,  C09J2205/102 ,  C09J2205/31 ,  Y02T50/43 ,  Y10T156/17 ,  Y10T428/249923 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2277/10 ,  B29K2067/00 ,  B29K2063/00 ,  B29K2305/00 ,  B29K2277/00 ,  B29K2309/02 ,  B29K2307/02 ,  B29K2309/14 ,  B29K2311/00 ,  B29K2061/04 ,  B29K2067/06 ,  B29K2075/02 ,  B29K2079/00 ,  B29K2083/00

摘要： Method for connecting two intermediate products (11a, 11b) for forming a fiber composite product, wherein the two intermediate products (11a, 11b) respectively consist of composite fiber material with a layer of matrix material and reinforcing fibers extending therein by means of connecting areas that adjoin one another in an overlapping region of the interconnected intermediate products (11a, 11b), with the method featuring the following steps:
■ applying an adhesive layer (1) that features an adhesive film (2) with a plurality of connecting particles (9) onto the connecting areas (18a, 18b) of the intermediate products (11 a, 11 b) in such a way that at least a portion of the plurality of connecting particles (9) sectionally comes in contact with reinforcing fibers of the first connecting area or the second connecting area,
■ arranging the second intermediate product (11b) on the first intermediate product (11a) or vice versa in such a way that the connecting areas (18a, 18b) at least partially overlap one another,
■ connecting the two intermediate products,

wherein the invention also pertains to a structural component (19) that consists of at least a first (11a) and a second (11b) fiber-reinforced intermediate product produced in accordance with such a method,
such a fiber composite product, a method for producing an adhesive layer (1) for connecting the intermediate products anda production device for carrying out such a method.

摘要翻译： 用于连接两个中间产物的方法（11A，11B），用于形成纤维复合产品，worin两个中间产物（11A，11B）分别与基体材料的层由复合纤维材料构成，并且增强纤维借助于在其中延伸的连接区域的 即彼此邻接在互连的中间产品的重叠区域（11A，11B）中，用配有以下步骤的方法： - 粘合剂层上施加（1）那样，设有一个粘合膜（2）与连接颗粒的多个（ 9）到连接区域（18A，18B）（在寻求一种方式的中间产物（11 A，11 b）的至少做连接的颗粒的多个部分9）部分地抵接与所述第一的增强纤维 连接区域或第二连接区域， - 布置所述第二中间产物（11B）上的第一中间产物（11A），或反之亦然的方式做了检查连接区域（18A，18B）一 吨至少部分地彼此重叠， - 连接两个中间产物，worin因此，本发明涉及在雅舞蹈生成的结构分量（19），至少一个第一（11A）的确实besteht和第二（11b）的纤维增强的中间产物 与搜索方法，寻找一个纤维复合产品，在用于连接所述中间产品用于执行寻求方法安达生产设备粘合剂层（1）的制造方法。

公开(公告)号：EP1995032A4

公开(公告)日：2012-11-14

申请号：EP07708296

申请日：2007-02-09

申请人： MITSUBISHI HEAVY IND LTD

发明人： OGURI KAZUYUKI

IPC分类号： B29C37/00 ,  B05D3/12 ,  B05D7/02 ,  B24C1/06

CPC分类号： B29C59/022 ,  B05D3/12 ,  B24C1/06 ,  B24C11/00 ,  B29C65/48 ,  B29C65/4815 ,  B29C65/484 ,  B29C65/8207 ,  B29C65/8253 ,  B29C66/02245 ,  B29C66/026 ,  B29C66/41 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/72143 ,  B29C66/73161 ,  B29C66/7392 ,  B29C66/73921 ,  B29C66/7394 ,  B29C66/73941 ,  B29C2059/027 ,  B29K2027/06 ,  B29K2055/02 ,  B29K2063/00 ,  B29K2067/00 ,  B29K2069/00 ,  B29K2077/00 ,  B29K2101/10 ,  B29K2101/12 ,  B29K2105/06 ,  B29K2277/00 ,  B29K2277/10 ,  B29K2307/00 ,  B29K2307/02 ,  B29K2309/02 ,  B29K2309/04 ,  B29K2309/08 ,  B29C65/00 ,  B29K2307/04 ,  B29K2067/06 ,  B29K2033/12

公开(公告)号：EP2243701A2

公开(公告)日：2010-10-27

申请号：EP10159744.1

申请日：2010-04-13

申请人： Mitsubishi Heavy Industries, Ltd.

发明人： Tanaka, Atsumi ,  Maruyama, Hironori ,  Kanemasu, Masayuki

IPC分类号： B64C1/06

CPC分类号： B64C1/062 ,  B29C65/483 ,  B29C65/5057 ,  B29C66/721 ,  B29C70/086 ,  B29C70/865 ,  B29C70/88 ,  B29K2063/00 ,  B29K2067/00 ,  B29K2067/06 ,  B29K2069/00 ,  B29K2075/00 ,  B29K2077/00 ,  B29K2077/10 ,  B29K2079/08 ,  B29K2101/10 ,  B29K2101/12 ,  B29K2105/06 ,  B29K2277/10 ,  B29K2305/00 ,  B29K2307/00 ,  B29K2307/02 ,  B29K2309/04 ,  B29K2309/08 ,  B29K2707/04 ,  B29K2995/0089 ,  B29L2031/3076 ,  B29L2031/608 ,  Y02T50/43 ,  Y10T156/10

摘要： An object is to provide an impact-absorbing structure superior in impact-absorbing capacity. An impact-absorbing structure includes a pair of flat, plate-like face plates (19) arranged to oppose each other with a predetermined distance therebetween; a core member (17) arranged between the face plates and fixed to the face plates; and a composite-material tube arranged between the face plates (7), at the core member side, the impact-absorbing member extending in one direction and fracturing progressively due to an impact compression force acting in the one direction. The composite-material tube is fixed to the face plates at one portion constituting a bonded region and is allowed to move relative to the face plates at a remaining portion constituting a non-bonded region.

摘要翻译： 目的在于提供一种冲击吸收能力优异的冲击吸收结构。 冲击吸收结构包括一对扁平的板状面板（19），它们以彼此相对的间隔彼此相隔预定距离; 芯片构件，其布置在所述面板之间并固定到所述面板; 以及复合材料管，其布置在所述面板（7）之间，在所述芯部件侧，所述冲击吸收部件沿一个方向延伸并且由于沿所述一个方向作用的冲击压缩力而逐渐断裂。 复合材料管在构成接合区域的一部分处固定到面板，并且在构成非接合区域的剩余部分处允许复合材料管相对于面板移动。

公开(公告)号：EP1910061A1

公开(公告)日：2008-04-16

申请号：EP06777554.4

申请日：2006-07-03

申请人： European Aeronautic Defence and Space Company - EADS France

发明人： SOCCARD, Eric

IPC分类号： B29C65/08

CPC分类号： B29C66/836 ,  B29C65/08 ,  B29C65/16 ,  B29C65/1635 ,  B29C65/364 ,  B29C65/3676 ,  B29C65/7841 ,  B29C65/7894 ,  B29C66/112 ,  B29C66/131 ,  B29C66/232 ,  B29C66/244 ,  B29C66/30221 ,  B29C66/30223 ,  B29C66/41 ,  B29C66/4722 ,  B29C66/474 ,  B29C66/5346 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/723 ,  B29C66/73772 ,  B29C66/73774 ,  B29C66/73921 ,  B29C66/81422 ,  B29C66/81469 ,  B29C66/8242 ,  B29C66/8362 ,  B29C66/8432 ,  B29C66/91411 ,  B29C66/9161 ,  B29C66/919 ,  B29C66/91931 ,  B29C66/9241 ,  B29C66/9261 ,  B29C66/934 ,  B29C66/9513 ,  B29C66/9516 ,  B29C66/96 ,  B29C66/962 ,  B29K2071/00 ,  B29K2079/085 ,  B29K2081/04 ,  B29K2101/12 ,  B29K2105/06 ,  B29K2307/00 ,  B29K2307/02 ,  B29K2309/08 ,  B29K2995/0027 ,  B29K2995/0039 ,  B29K2995/004 ,  B29L2009/00 ,  B29L2031/003 ,  B29L2031/3082 ,  Y10T428/24 ,  B29K2307/04

摘要： The invention concerns a method for assembling at least two thermoplastic rigid parts (1, 2) which consists in superimposing the two parts (1, 2) so that they have at least one interface zone (4), at least one of the two parts bearing one or more projecting energy directing elements (5) located in the interface zone (4), exciting at least one ultrasonic source (10) contacted with one of the two parts, said ultrasonic source (10) applying a compressive force (F) to the two parts (1, 2) in a region (4.1) of the interface zone located opposite the ultrasonic source (10), moving the ultrasonic source (10) continuously at the interface zone (4) so as to form a continuous weld joint (6) by melting the thermoplastic material of the region (4.1) located opposite the ultrasonic sound (10). The invention is in particular useful for assembling laminated parts.

公开(公告)号：EP0048055A3

公开(公告)日：1984-07-25

申请号：EP81200988

申请日：1981-09-07

申请人： Koninklijke Nijverdal-Ten Cate N.V.

发明人： Pott, Richard

IPC分类号： B29D03/02

CPC分类号： B63B35/7906 ,  B29C65/5028 ,  B29C65/5042 ,  B29C66/1142 ,  B29C66/43 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C70/08 ,  B29C70/22 ,  B29C70/865 ,  B29D24/001 ,  B29K2063/00 ,  B29K2067/06 ,  B29K2079/085 ,  B29K2277/00 ,  B29K2307/00 ,  B29K2307/02 ,  B29L2031/307 ,  B63B5/24 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2277/10 ,  B29K2067/00 ,  B29K2079/08 ,  B29K2061/04

摘要： The invention relates to a laminate reinforcement for fibre-reinforced sunthetic resins and has for its object to provide a laminate reinforcement of highly resistant and high elasticity modulus fibres for extremely heavy-duty, yet light-weight and indent-resistent floating bodies and provides to that purpose such a reinforcement in which the laminate reinforcement is obtained by means of at least two parallel tissue tapes forming by their tissue seams a paunch gap, which is covered with a similar, but narrower covering tape, doubling of the reinforcing fibres in the area of the paunch gap in parallel relationship producing a Stringer effect, in which the warp and weft yarns of the tissue tape are made from reinforcing fibres having a higher elasticity modulus and a higher specific tensile strength than glass fibres, said fibres consisting of carbon, aramid, boron fibres or the like, the warp yarns of carbon and aramid being in intimate contact with one another and the weft yarns of aramid or carbon being spaced apart in parallel relationship by a larger distance than the warp yarns.

公开(公告)号：EP1801428B1

公开(公告)日：2017-05-31

申请号：EP06381046.9

申请日：2006-10-31

申请人： Airbus Operations S.L.

发明人： Escobar Benavides, Francisco de Paula ,  Claret Virós, Daniel ,  Ávila Domínguez, Rafael

IPC分类号： F16B5/00 ,  B29C65/56 ,  B64C1/00 ,  B29K101/10 ,  B29K101/12 ,  B29K307/04 ,  B29K309/08 ,  B29K307/02 ,  B29K705/00 ,  B29L31/30

CPC分类号： B32B15/14 ,  B29C65/562 ,  B29C65/601 ,  B29C66/1122 ,  B29C66/43 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/7392 ,  B29C66/73921 ,  B29C66/7394 ,  B29C66/73941 ,  B29K2307/00 ,  B29L2031/3076 ,  B29L2031/3082 ,  B29L2031/737 ,  B32B7/08 ,  B32B15/043 ,  B32B15/08 ,  B32B2260/021 ,  B32B2262/106 ,  B32B2305/08 ,  B32B2311/18 ,  F16B5/02 ,  Y10T428/19 ,  Y10T428/24008 ,  Y10T428/24017 ,  Y10T428/24752 ,  B29K2305/00 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2277/10 ,  B29K2307/02 ,  B29K2305/02 ,  B29K2305/12

公开(公告)号：EP2799728A4

公开(公告)日：2015-12-23

申请号：EP12861083

申请日：2012-12-17

申请人： MITSUBISHI HEAVY IND LTD

发明人： NONAKA YOSHINORI ,  KASHIWAGI MASAHIRO ,  ABE TOSHIO

IPC分类号： F16B5/02 ,  B29C65/56 ,  B29C65/64

CPC分类号： F16B5/12 ,  B29C65/48 ,  B29C65/562 ,  B29C65/72 ,  B29C66/1122 ,  B29C66/474 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/7394 ,  B29C66/73941 ,  F16B5/02 ,  Y10T403/472 ,  Y10T403/75 ,  B29K2309/08 ,  B29K2307/02 ,  B29K2307/04 ,  B29K2277/10 ,  B29K2069/00 ,  B29K2063/00

摘要： A joint structure for a composite member having a light-weight and low-cost structure, easy to manufacture, and resistible against a large shear load, is provided. A joint structure (1) for a composite member made from a composite material, comprising a plate for increasing thickness (40a, 40b) adhered to at least one side of the composite member (10); wherein the composite member (10) and a counterpart member (20) are fastened together by inserting and fixing a fastener member (30) into a through-hole (24, 26) formed through the composite member (10), the plate for increasing thickness (40a, 40b), and the counterpart member (20) to be joined to the composite member.

公开(公告)号：EP1801428A3

公开(公告)日：2014-11-05

申请号：EP06381046.9

申请日：2006-10-31

申请人： Airbus Operations S.L.

发明人： Escobar Benavides, Francisco de Paula ,  Claret Virós, Daniel ,  Ávila Domínguez, Rafael

IPC分类号： F16B5/00 ,  B29C65/56 ,  B64C1/00 ,  B29K101/10 ,  B29K101/12 ,  B29K307/04 ,  B29K309/08 ,  B29K307/02 ,  B29K705/00 ,  B29L31/30

CPC分类号： B32B15/14 ,  B29C65/562 ,  B29C65/601 ,  B29C66/1122 ,  B29C66/43 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/7392 ,  B29C66/73921 ,  B29C66/7394 ,  B29C66/73941 ,  B29K2307/00 ,  B29L2031/3076 ,  B29L2031/3082 ,  B29L2031/737 ,  B32B7/08 ,  B32B15/043 ,  B32B15/08 ,  B32B2260/021 ,  B32B2262/106 ,  B32B2305/08 ,  B32B2311/18 ,  F16B5/02 ,  Y10T428/19 ,  Y10T428/24008 ,  Y10T428/24017 ,  Y10T428/24752 ,  B29K2305/00 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2277/10 ,  B29K2307/02 ,  B29K2305/02 ,  B29K2305/12

摘要： A mechanically fastened permanent or detachable joint between two or more parts (21, 23, 25, 41), at least one of them made of a composite material, preferably carbon fibres impregnated with thermoset resin, with continuous plies from the full-composite area along the joint area (15) and including a metal reinforcement, preferably made of titanium, in the joint area (15), the joint area (15) thickness being increased in the thickness of said reinforcement plus the eventual additional composite plies laid only on the reinforced area. The metal reinforcement may consist of one or more metal foils or sheets (31) interleaved between the composite plies or one or more metal plates (33) embedded between two of the composite plies.

公开(公告)号：EP2025954A1

公开(公告)日：2009-02-18

申请号：EP08162257.3

申请日：2008-08-12

申请人： The Boeing Company

发明人： Keener, Steven G.

IPC分类号： F16B33/00 ,  B29C65/00 ,  B29C65/56

CPC分类号： F16B33/006 ,  B29C65/562 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72143 ,  B29C66/7392 ,  B29C66/73921 ,  B29C66/7394 ,  B29C66/73941 ,  B29C70/545 ,  B29K2023/06 ,  B29K2027/12 ,  B29K2027/18 ,  B29K2031/00 ,  B29K2063/00 ,  B29K2067/00 ,  B29K2067/006 ,  B29K2071/00 ,  B29K2075/00 ,  B29K2077/10 ,  B29K2079/085 ,  B29K2081/04 ,  B29K2081/06 ,  B29K2101/10 ,  B29K2101/12 ,  B29K2105/0079 ,  B29K2277/10 ,  B29K2307/00 ,  B29K2307/02 ,  B29K2309/02 ,  B29K2309/08 ,  B29K2707/04 ,  B29K2709/02 ,  B29K2709/08 ,  B29L2031/3076 ,  B29L2031/727 ,  B64F5/10 ,  F16B39/02 ,  Y10T29/49622 ,  Y10T29/49885 ,  Y10T29/49906 ,  Y10T29/49952 ,  Y10T29/49964 ,  Y10T29/4997 ,  Y10T29/53 ,  Y10T29/53709 ,  B29K2307/04

摘要： A method for attaching parts. A composite male fastening component (810) is placed through at least a first part (804) and a second part (802). The composite male fastener component (810) preferably has a threaded portion. A composite female fastener component (812) is positioned adjacent to and surrounding the threaded portion of the male fastener component (810). A portion of the composite female fastener component (812) is caused to flow around and form into the threaded portion of the composite male fastener component (810). The portion of the composite female fastener component (812) that flowed around and formed into the threaded portion of the composite male fastener component (810) is re-solidified and re-consolidated such that the composite female fastener component (812) is securely attached to the composite male fastener component (810) thereby joining the mating parts.

摘要翻译： 一种用于安装部的方法。 一种复合阳紧固元件（810）通过至少一个第一部分（804）和第二部分（802）放置。 所述复合插入式紧固件部件（810）优选地具有螺纹部。 一种复合式紧固件部件（812）定位成邻近于并围绕所述阳紧固件部件（810）的螺纹部分。 该复合式紧固件部件（812）的一部分被使得周围流动，并形成到复合插入式紧固件部件（810）的螺纹部分。 该复合式紧固件部件（812）的所述部分并围绕流动并形成所述复合插入式紧固件部件（810）的螺纹部分是再固化和重新合并检查并复合式紧固件部件（812）被牢固地附 到复合插入式紧固件部件（810），从而接合所述配合部件。