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1. 发明公开

EP3381665A1 COMPOSITE STRUCTURAL COMPONENT WITH CAPTIVE MECHANICAL JOINT 有权
公开(公告)号：EP3381665A1
公开(公告)日：2018-10-03
申请号：EP17164438.8
申请日：2017-03-31
申请人： Crompton Technology Group Limited
发明人： BEALE, Tom
IPC分类号： B29C65/56 , B29C65/64 , F16C7/02 , B29C70/86 , B29K105/08 , B29K705/00 , B29K307/04 , B29K309/08 , B29L31/06 , B29D99/00
CPC分类号： F16B7/0406 , B29C65/562 , B29C65/64 , B29C66/1122 , B29C66/301 , B29C66/534 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C70/86 , B29D99/0046 , B29L2031/06 , E04C3/28 , F16C3/026 , F16C7/026 , B29K2309/08 , B29K2307/04
摘要： A composite structural component 1 comprises an elongate member 2 made of a polymer matrix composite material. The elongate member 2 comprises a main portion 2A extending along an axis A and an end portion 2B with an inner surface 2C extending from the main portion 2B to an open end of the member 2. The composite structural component 1 also comprises an end fitting 6 forming a mechanical joint 4 with the end portion 2B, the end fitting 6 comprising an internal portion 8 positioned captive within the elongate member 2 in contact with the inner surface 2C of the end portion 2B; an external portion 10 positioned in contact with an outer surface 2D of the end portion 2B; and an adjustable fastener 12, 14 extending axially between the internal and external portions 8, 10 to clamp the end portion 2B between the internal and external portions 8, 10. The inner surface 2C of the end portion 2B in contact with the internal portion 8 extends towards the axis A at an increasing angle to the axis A.

2. 发明授权

EP2722533B1 Procédé de collage de deux pièces soumises à des efforts de traction, pièces collées obtenues 有权
标题翻译：粘合两块经受拉伸应力的方法，获得粘合块
公开(公告)号：EP2722533B1
公开(公告)日：2018-05-02
申请号：EP13306423.8
申请日：2013-10-17
申请人： Epsilon Composite
发明人： Carrere, Noël , Ciccone, Anatole
IPC分类号： F16B11/00
CPC分类号： B32B1/08 , B29C65/48 , B29C65/542 , B29C66/12441 , B29C66/1246 , B29C66/534 , B29C66/721 , B29C66/742 , B29L2031/06 , F16B11/006 , F16B11/008 , F16C7/026 , Y10T403/47

3. 发明授权

EP2433024B1 PROCEDE DE FABRICATION D'UNE BIELLE EN MATERIAU COMPOSITE 有权转让
标题翻译：在复合材料中制造杆的方法
公开(公告)号：EP2433024B1
公开(公告)日：2018-05-02
申请号：EP10723014.6
申请日：2010-05-18
申请人： Safran Landing Systems
发明人： MASSON, Richard , DUNLEAVY, Patrick
IPC分类号： F16C7/00 , B29C70/24 , B29C70/86
CPC分类号： F16C7/026 , B29C70/24 , B29C70/48 , B29L2031/06

4. 发明公开

EP3213928A1 METHOD FOR MANUFACTURING DECORATIVE-ARTISTIC ARTICLES 审中-公开
标题翻译：制造装饰艺术物品的方法
公开(公告)号：EP3213928A1
公开(公告)日：2017-09-06
申请号：EP16818325.9
申请日：2016-08-05
申请人： Litnitskii, Iurii Ivanovich
发明人： Litnitskii, Iurii Ivanovich
IPC分类号： B44C5/00 , B29C45/14 , B29C45/26
CPC分类号： B44C5/00 , B29C39/10 , B29C39/42 , B29C44/146 , B29C51/04 , B29C51/105 , B29C51/266 , B29C51/30 , B29C51/36 , B29C2791/001 , B29C2791/006 , B29K2075/00 , B29K2621/00 , B29K2623/06 , B29K2623/12 , B29K2625/06 , B29K2627/06 , B29K2705/00 , B29K2711/14 , B29L2031/06 , B29L2031/44 , B29L2031/722 , B29L2031/766
摘要： A method for manufacturing decorative-artistic articles from a fluid self-hardening material, in which a casting mould consisting of two dies is pre-manufactured, a lining material is placed into at least one of the dies, the space between the lining material and the working surface of the die is evacuated, the die is closed, after which the fluid self-hardening material is cast, wherein, before the lining material is placed into at least one of the dies, said material is pre-shaped by a punch in a thermal vacuum press, and the cavity between the dies is evacuated before the self-hardening material is cast. The technical results of the article include the production of an article from a fluid self-hardening material which is covered with a lining material, without creases and without loss of the material pattern, with good decorative properties and with an aesthetic external appearance, of any profile, without the formation of internal voids and casting defects, and not requiring additional processing of the surface; and a reduction in labour costs and costs of production.
摘要翻译：一种由流体自硬材料制造装饰艺术品的方法，其中预先制造由两个模具构成的铸模，将衬材放入至少一个模具中，衬材和将模具的工作表面抽空，关闭模具，然后浇铸流体自硬材料，其中，在将衬里材料放入至少一个模具之前，通过冲头将所述材料预成形在热真空压机中，并且在自硬化材料被铸造之前，模具之间的空腔被抽空。该文章的技术结果包括由流体自硬材料生产的物品覆盖有衬里材料，没有折痕且没有材料图案的损失，具有良好的装饰性能和具有美学外观的任何没有形成内部空隙和铸造缺陷，并且不需要额外处理表面; 并减少劳动力成本和生产成本。

5. 发明授权

EP2324258B1 COMPOSITE TIE ROD AND METHOD FOR MAKING THE SAME 有权
标题翻译： VERBUNDZUGSTANGE及其制造方法
公开(公告)号：EP2324258B1
公开(公告)日：2016-11-23
申请号：EP09790782.8
申请日：2009-07-23
申请人： The Boeing Company
发明人： SCHALLA, James, P. , LIN, Dennis, C. , BOBZIEN, Phillip, J.
IPC分类号： F16C7/02 , B29C70/22 , B64C1/06 , E04C3/29 , B64D11/00
CPC分类号： F16C7/026 , B29C70/222 , B29L2031/06 , B64C1/066 , B64D11/00 , E04C3/291 , F16C2326/43 , Y02T50/43 , Y02T50/46 , Y10T428/24008
摘要： A composite tie rod comprises an open lattice body formed of interlaced filaments held in a solid matrix. A pair of fittings rigidly connect rod ends with the ends of the body. The rod ends form attachment points on the tie rod.

6. 发明公开

EP3040191A1 Method for manufacturing fillers of composite material 有权
标题翻译： Verfahren zur Herstellung vonEckfüllungenaus Verbundwerkstoff
公开(公告)号：EP3040191A1
公开(公告)日：2016-07-06
申请号：EP14382583.4
申请日：2014-12-30
申请人： Airbus Operations, S.L.
发明人： Cruzado Parla, Gabriel , López Fernández, Pablo , Echevarría Hernández, Aitor , Martinez Cerezo, Alberto , Mulas de Lamo, Alberto , Mora Medias, María
IPC分类号： B29D99/00 , B29C70/34 , B29C70/54 , B29C70/46
CPC分类号： B29C70/382 , B29C70/345 , B29C70/386 , B29C70/545 , B29D99/0003 , B29L2031/06
摘要： The invention refers to a method for manufacturing rod-shaped components of composite material, for example rowings or fillers, wherein a laminate (5) is layered by automatically laying up a plurality of plies of composite material, which is then cut in an automated machine (7) to obtain a plurality of rods (8) having substantially the same cross-sectional shape. The obtained rods (8) are then simultaneously conformed by applying heat and pressure to obtain rods with the desired cross-sectional shape. With the method of the invention, a large number of these type of components is produced with improved quality and in a very simple manner, using the machinery and equipment already commonly existing in a factory of aeronautic components.
摘要翻译：本发明涉及一种用于制造复合材料的棒状部件的方法，例如排列或填料，其中层压体（5）通过自动铺设多个复合材料层而层叠，然后将其从自动化机器（7），以获得具有基本上相同横截面形状的多个杆（8）。然后通过施加热和压力同时使得到的棒（8）适应，以获得具有所需横截面形状的棒。利用本发明的方法，使用已经通常存在于航空部件的工厂中的机械和设备，以很简单的方式制造了大量这些类型的部件。

7. 发明授权

EP2525964B1 PROCEDE DE FABRICATION DE PIECES COMPOSITES COMPORTANT DES FIBRES TRESSEES 有权转让
标题翻译：用于生产复合材料部件带编织纤维
公开(公告)号：EP2525964B1
公开(公告)日：2015-03-11
申请号：EP11700618.9
申请日：2011-01-19
申请人： Messier-Bugatti-Dowty
发明人： MASSON, Richard , GOURET, Mathieu , BOUDIER, Romain
IPC分类号： B29C70/32 , B29C70/54 , B29C70/88 , F16C7/00
CPC分类号： B29C70/32 , B29C70/545 , B29C70/887 , B29L2031/06 , F16C7/02 , F16C7/026 , Y10T156/1052

8. 发明公开

EP2753837A1 COMPOSITE LINK FITTING 审中-公开
标题翻译：复合连接配件
公开(公告)号：EP2753837A1
公开(公告)日：2014-07-16
申请号：EP12829985.6
申请日：2012-06-22
申请人： Blair HSM Composites LLC
发明人： PADDEN, Vincent
IPC分类号： F16C7/00
CPC分类号： B32B37/12 , B29C70/86 , B29L2031/06 , B32B37/142 , F16C7/026 , F16C2208/04 , F16C2208/82 , F16C2208/86 , F16C2220/28 , Y02T50/43 , Y10T29/49288 , Y10T29/49622 , Y10T29/49787 , Y10T29/49826 , Y10T29/49915 , Y10T29/49924 , Y10T29/49947 , Y10T74/2142 , Y10T74/2162 , Y10T156/1052 , Y10T156/1075 , Y10T156/1724
摘要： A link fitting having bearing supports, an inner core and an outer band surrounding it all. Each bearing support includes a first stepped portion, a separate second stepped portion and a recess disposed between the first and second stepped portions. The inner core includes a central elongate layer, a first outer layer and a second outer layer. The first and second outer layers are disposed on opposed first and second sides of the central layer. The first outer layer engages the first side of the central layer and a portion of the first stepped portion on each of the two bearing supports. The second outer layer engaging the second side of the central layer and a portion of the second stepped portion on each of the two bearing supports. Opposed first and second ends of the central layer disposed within the recesses of each of the two bearing supports.

9. 发明公开

EP2722531A1 Hybrid joint manufacturing 审中-公开
标题翻译： Hybridverbindungsherstellung
公开(公告)号：EP2722531A1
公开(公告)日：2014-04-23
申请号：EP12275159.7
申请日：2012-10-22
申请人： BAE Systems PLC
发明人： The designation of the inventor has not yet been filed
IPC分类号： F16B5/04
CPC分类号： B29C66/742 , B21J15/00 , B21J15/147 , B21K25/00 , B29C65/606 , B29C65/607 , B29C65/64 , B29C66/1122 , B29C66/21 , B29C66/30321 , B29C66/43 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/72143 , B29C66/8322 , B29C70/48 , B29C70/545 , B29C70/86 , B29C2793/0045 , B29L2031/06 , B29L2031/3076 , F16B5/045 , B29K2309/08 , B29K2307/04
摘要： A method for forming a joint between a fibre reinforced composite component and a metallic component and a joint are provided. The metallic component and the composite component each define a joint surface for mating with the joint surface of the other to join the two components together and the composite component defines a free surface opposed to the joint surface thereof. The joint surface of the metallic component defines an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface. The method includes the steps of pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate through the fibre reinforcing material, and modifying the effective cross sectional shape of the pin heads whereby to increase the constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component.
摘要翻译：提供了一种在纤维增强复合部件与金属部件和接头之间形成接头的方法。金属部件和复合部件各自限定用于与另一个的接头表面配合的接合表面，以将两个部件连接在一起，并且复合部件限定与其接头表面相对的自由表面。金属部件的接合表面限定了从其延伸的销的阵列，每个销在远离接合表面的一端限定销头。该方法包括以下步骤：将两个部件的接合表面压在一起，从而使销的阵列穿过纤维增强材料，并且改变销头的有效横截面形状，从而增加对复合材料的约束防止复合部件从金属部件的接合面剥离。

10. 发明公开

EP2184766A3 Directional extruded bead control 有权
标题翻译：定向挤压球控制
公开(公告)号：EP2184766A3
公开(公告)日：2012-01-25
申请号：EP09173586.0
申请日：2009-10-21
申请人： SolarWorld Innovations GmbH
发明人： Fork, David K. , Solberg, Scott E.
IPC分类号： H01L21/67 , B29C47/12 , B81C99/00
CPC分类号： H01L21/6715 , B29C47/0002 , B29C47/0016 , B29C47/026 , B29C47/062 , B29C47/084 , B29C47/128 , B29L2031/06 , B81B2207/07 , B81C99/0015
摘要： The present invention refers to a micro-extrusion system including a printhead assembly and a material feed system for extruding one or more materials out of extrusion nozzles defined in the printhead assembly. The extruded materials form parallel beads on an upper surface of a target substrate. According to the invention, the printhead assembly comprises a first plate structure, a second plate structure and a layered nozzle structure sandwiched between the first and second plate structures. The layered nozzle structure includes a top nozzle plate including a first front edge and defining a first inlet port and a nozzle outlet plate including a second front edge and defining an elongated nozzle channel extending in a predetermined first flow direction from a closed end to an opening defined through said second front edge, wherein the top nozzle plate is mounted on the nozzle outlet plate to form an extrusion nozzle, where a portion of the top nozzle plate forms an upper wall of the extrusion nozzle, opposing edges of the elongated channel form side walls of the extrusion nozzle, and the opening formed in the second front edge defines an outlet orifice of the extrusion nozzle, wherein the first inlet port is aligned with the closed end of the elongated channel, whereby extrusion material forced through the first inlet port flows in the first flow direction along the extrusion nozzle and out of said outlet orifice to form said bead, and wherein said layered nozzle structure comprises means for biasing the bead toward the target substrate.

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