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1. 发明公开

CN101384420A 使用复合材料形成的部件的局部增强用增强材料及方法无效
公开(公告)号：CN101384420A
公开(公告)日：2009-03-11
申请号：CN200780005819.5
申请日：2007-02-01
申请人：空中客车德国有限公司
发明人：阿克塞尔·S·赫尔曼
IPC分类号： B29C70/88
CPC分类号： B32B27/00 , B29C70/088 , B29C70/44 , B29K2705/00 , B29K2705/12 , B29K2705/14 , B29K2707/04 , B29K2863/00 , B29K2867/06 , B29K2995/0072 , B29L2031/3085 , B32B15/08 , B32B17/10761 , B32B27/08 , B32B27/32 , C09J7/22 , C09J7/38 , Y02T50/43 , Y10T428/24967 , Y10T428/28 , Y10T428/2852 , Y10T428/287 , Y10T428/2896
摘要：本发明涉及一种用于特别在力引入区域和/或连接区域(7)中局部增强使用复合材料形成的部件(6)的增强材料1。根据本发明，所述增强材料(1)由金属片状结构形成，所述金属片状结构具有粗糙度增大以改善粘附的表面(4)，以及被涂敷到所述表面(4)上以提供密封，并且改善与所述复合材料的粘合的涂层(5)。

2. 发明授权

US08802224B2 Reinforcing material for the local reinforcement of a component formed with a composite material, and method 有权
标题翻译：用于复合材料形成的部件的局部增强的加强材料及方法
公开(公告)号：US08802224B2
公开(公告)日：2014-08-12
申请号：US12223936
申请日：2007-02-01
申请人： Axel Herrmann
发明人： Axel Herrmann
IPC分类号： B32B15/08 , B32B7/02 , B05D5/10 , B32B27/00 , B32B27/08 , B32B27/32 , B32B17/10 , C09J7/02
CPC分类号： B32B27/00 , B29C70/088 , B29C70/44 , B29K2705/00 , B29K2705/12 , B29K2705/14 , B29K2707/04 , B29K2863/00 , B29K2867/06 , B29K2995/0072 , B29L2031/3085 , B32B15/08 , B32B17/10761 , B32B27/08 , B32B27/32 , C09J7/22 , C09J7/38 , Y02T50/43 , Y10T428/24967 , Y10T428/28 , Y10T428/2852 , Y10T428/287 , Y10T428/2896
摘要： Disclosed is a reinforcing material for the local reinforcement of a component formed with a composite material, in particular in areas of force introduction and/or connecting areas. The reinforcing material is formed by a metallic sheet-like formation, the metallic sheet-like formation having a surface with increased roughness to improve adhesion and a coating applied to the surface to provide a seal and improve the bond with the composite material. As a result of the presence of a coating on the metallic sheet-like formation, once it has been rolled up on supply rolls, said sheet-like formation can be drawn off from the supply rolls and at the same time processed in an automated manner by means of known computer-controlled laying devices with CRP prepreg materials in web form by laying layer by layer to produce components, in particular of large format, for aircraft. The reinforcing material thereby ensures a high embedding strength in the case of introduced boreholes or the like, in particular in areas of force introduction and/or connecting areas. Also disclosed is a method for producing a reinforcing material. In addition, the invention relates to a method for producing components, in particular components of large format for aircraft, with the composite material and with the reinforcing material.
摘要翻译：公开了一种用于局部增强由复合材料形成的部件的增强材料，特别是在力引入和/或连接区域的区域。增强材料通过金属片状结构形成，金属片状结构具有粗糙度增加的表面以提高粘附性，并且涂覆在表面上以提供密封并改善与复合材料的粘结。由于在金属片状结构上存在涂层，一旦已经在供给辊上卷起，所述片状结构可以从供给辊中抽出，同时以自动方式进行处理通过已知的计算机控制的铺设装置，其中通过逐层铺设具有卷筒纸形式的CRP预浸料材料，以生产用于飞行器的特别是大格式的部件。因此，在引入的钻孔等的情况下，特别是在力引入区域和/或连接区域中，增强材料确保了高嵌入强度。还公开了一种用于生产增强材料的方法。此外，本发明涉及用于生产组件的方法，特别是用于航空器的大格式的组件，其具有复合材料和增强材料。

3. 发明申请

US20100316857A1 Reinforcing Material for the Local Reinforcement of a Component Formed With a Composite Material, and Method 有权
标题翻译：用复合材料形成的部件的局部增强材料的增强材料及方法
公开(公告)号：US20100316857A1
公开(公告)日：2010-12-16
申请号：US12223936
申请日：2007-02-01
申请人： Axel Herrmann
发明人： Axel Herrmann
IPC分类号： B32B15/08 , B32B7/02 , B05D5/10
CPC分类号： B32B27/00 , B29C70/088 , B29C70/44 , B29K2705/00 , B29K2705/12 , B29K2705/14 , B29K2707/04 , B29K2863/00 , B29K2867/06 , B29K2995/0072 , B29L2031/3085 , B32B15/08 , B32B17/10761 , B32B27/08 , B32B27/32 , C09J7/22 , C09J7/38 , Y02T50/43 , Y10T428/24967 , Y10T428/28 , Y10T428/2852 , Y10T428/287 , Y10T428/2896
摘要： Disclosed is a reinforcing material for the local reinforcement of a component formed with a composite material, in particular in areas of force introduction and/or connecting areas. The reinforcing material is formed by a metallic sheet-like formation, the metallic sheet-like formation having a surface with increased roughness to improve adhesion and a coating applied to the surface to provide a seal and improve the bond with the composite material. As a result of the presence of a coating on the metallic sheet-like formation, once it has been rolled up on supply rolls, said sheet-like formation can be drawn off from the supply rolls and at the same time processed in an automated manner by means of known computer-controlled laying devices with CRP prepreg materials in web form by laying layer by layer to produce components, in particular of large format, for aircraft. The reinforcing material thereby ensures a high embedding strength in the case of introduced boreholes or the like, in particular in areas of force introduction and/or connecting areas. Also disclosed is a method for producing a reinforcing material. In addition, the invention relates to a method for producing components, in particular components of large format for aircraft, with the composite material and with the reinforcing material.
摘要翻译：公开了一种用于局部增强由复合材料形成的部件的增强材料，特别是在力引入和/或连接区域的区域。增强材料通过金属片状结构形成，金属片状结构具有粗糙度增加的表面以提高粘附性，并且涂覆在表面上以提供密封并改善与复合材料的粘结。由于在金属片状结构上存在涂层，一旦已经在供给辊上卷起，所述片状结构可以从供给辊中抽出并且同时以自动方式进行处理通过已知的计算机控制的铺设装置，其中通过逐层铺设具有卷筒纸形式的CRP预浸料材料，以生产用于飞行器的特别是大格式的部件。因此，在引入的钻孔等的情况下，特别是在力引入区域和/或连接区域中，增强材料确保了高嵌入强度。还公开了一种用于生产增强材料的方法。此外，本发明涉及用于生产组件的方法，特别是用于航空器的大格式的组件，其具有复合材料和增强材料。

4. 发明授权

EP0341797B1 Mould and process for the fabrication thereof 失效转让
标题翻译：其制造的模具和工艺
公开(公告)号：EP0341797B1
公开(公告)日：1992-09-30
申请号：EP89201174.3
申请日：1989-05-09
申请人： DSM N.V.
发明人： Van Dalen, Hendrik
IPC分类号： B29C33/38 , B29C33/56
CPC分类号： B29C33/38 , B29C33/56 , B29C37/0082 , B29K2709/06 , B29K2863/00 , B29K2867/06 , B29K2909/06

5. 发明授权

EP1984166B1 REINFORCING MATERIAL FOR THE LOCAL REINFORCEMENT OF A COMPONENT FORMED WITH A COMPOSITE MATERIAL, AND METHOD 有权
标题翻译：加强材料的局部加固与复合成型构件和方法
公开(公告)号：EP1984166B1
公开(公告)日：2010-05-12
申请号：EP07704282.8
申请日：2007-02-01
申请人： Airbus Deutschland GmbH
发明人： HERRMANN, Axel, S.
IPC分类号： B29C70/88
CPC分类号： B32B27/00 , B29C70/088 , B29C70/44 , B29K2705/00 , B29K2705/12 , B29K2705/14 , B29K2707/04 , B29K2863/00 , B29K2867/06 , B29K2995/0072 , B29L2031/3085 , B32B15/08 , B32B17/10761 , B32B27/08 , B32B27/32 , C09J7/22 , C09J7/38 , Y02T50/43 , Y10T428/24967 , Y10T428/28 , Y10T428/2852 , Y10T428/287 , Y10T428/2896
摘要： Disclosed is a reinforcing material for the local reinforcement of a component formed with a composite material, in particular in areas of force introduction and/or connecting areas. The reinforcing material is formed by a metallic sheet-like formation, the metallic sheet-like formation having a surface with increased roughness to improve adhesion and a coating applied to the surface to provide a seal and improve the bond with the composite material. As a result of the presence of a coating on the metallic sheet-like formation, once it has been rolled up on supply rolls, said sheet-like formation can be drawn off from the supply rolls and at the same time processed in an automated manner by means of known computer-controlled laying devices with CRP prepreg materials in web form by laying layer by layer to produce components, in particular of large format, for aircraft. The reinforcing material thereby ensures a high embedding strength in the case of introduced boreholes or the like, in particular in areas of force introduction and/or connecting areas. Also disclosed is a method for producing a reinforcing material. In addition, the invention relates to a method for producing components, in particular components of large format for aircraft, with the composite material and with the reinforcing material.

6. 发明公开

EP1984166A1 REINFORCING MATERIAL FOR THE LOCAL REINFORCEMENT OF A COMPONENT FORMED WITH A COMPOSITE MATERIAL, AND METHOD 有权
标题翻译：加强材料的局部加固与复合成型构件和方法
公开(公告)号：EP1984166A1
公开(公告)日：2008-10-29
申请号：EP07704282.8
申请日：2007-02-01
申请人： Airbus Deutschland GmbH
发明人： HERRMANN, Axel, S.
IPC分类号： B29C70/88
CPC分类号： B32B27/00 , B29C70/088 , B29C70/44 , B29K2705/00 , B29K2705/12 , B29K2705/14 , B29K2707/04 , B29K2863/00 , B29K2867/06 , B29K2995/0072 , B29L2031/3085 , B32B15/08 , B32B17/10761 , B32B27/08 , B32B27/32 , C09J7/22 , C09J7/38 , Y02T50/43 , Y10T428/24967 , Y10T428/28 , Y10T428/2852 , Y10T428/287 , Y10T428/2896
摘要： Disclosed is a reinforcing material for the local reinforcement of a component formed with a composite material, in particular in areas of force introduction and/or connecting areas. The reinforcing material is formed by a metallic sheet-like formation, the metallic sheet-like formation having a surface with increased roughness to improve adhesion and a coating applied to the surface to provide a seal and improve the bond with the composite material. As a result of the presence of a coating on the metallic sheet-like formation, once it has been rolled up on supply rolls, said sheet-like formation can be drawn off from the supply rolls and at the same time processed in an automated manner by means of known computer-controlled laying devices with CRP prepreg materials in web form by laying layer by layer to produce components, in particular of large format, for aircraft. The reinforcing material thereby ensures a high embedding strength in the case of introduced boreholes or the like, in particular in areas of force introduction and/or connecting areas. Also disclosed is a method for producing a reinforcing material. In addition, the invention relates to a method for producing components, in particular components of large format for aircraft, with the composite material and with the reinforcing material.

7. 发明申请

WO2007093503A1 REINFORCING MATERIAL FOR THE LOCAL REINFORCEMENT OF A COMPONENT FORMED WITH A COMPOSITE MATERIAL, AND METHOD 审中-公开
标题翻译：用复合材料形成的组分的本地增强材料的增强材料和方法
公开(公告)号：WO2007093503A1
公开(公告)日：2007-08-23
申请号：PCT/EP2007/050960
申请日：2007-02-01
申请人： AIRBUS DEUTSCHLAND GMBH , HERRMANN, Axel, S.
发明人： HERRMANN, Axel, S.
IPC分类号： B29C70/88
CPC分类号： B32B27/00 , B29C70/088 , B29C70/44 , B29K2705/00 , B29K2705/12 , B29K2705/14 , B29K2707/04 , B29K2863/00 , B29K2867/06 , B29K2995/0072 , B29L2031/3085 , B32B15/08 , B32B17/10761 , B32B27/08 , B32B27/32 , C09J7/22 , C09J7/38 , Y02T50/43 , Y10T428/24967 , Y10T428/28 , Y10T428/2852 , Y10T428/287 , Y10T428/2896
摘要： The invention relates to a reinforcing material 1 for the local reinforcement of a component (6) formed with a composite material, in particular in areas of force introduction and/or connecting areas (7). According to the invention, the reinforcing material (1) is formed by a metallic sheet-like formation, the metallic sheet- like formation having a surface (4) with increased roughness to improve adhesion and a coating (5) applied to the surface (4) to provide a seal and improve the bond with the composite material.
摘要翻译：本发明涉及一种用于局部增强由复合材料形成的部件（6）的增强材料，特别是在力引入和/或连接区域（7）的区域中。根据本发明，增强材料（1）通过金属片状结构形成，金属片状结构具有表面（4），其表面粗糙度增加以提高粘附性，并且涂覆（5）施加到表面 4）提供密封并改善与复合材料的粘结。

8. 发明公开

EP0341797A1 Mould and process for the fabrication thereof 失效转让
标题翻译： Giessform und Verfahren zu deren Herstellung。
公开(公告)号：EP0341797A1
公开(公告)日：1989-11-15
申请号：EP89201174.3
申请日：1989-05-09
申请人： DSM N.V.
发明人： Van Dalen, Hendrik
IPC分类号： B29C33/38 , B29C33/56
CPC分类号： B29C33/38 , B29C33/56 , B29C37/0082 , B29K2709/06 , B29K2863/00 , B29K2867/06 , B29K2909/06
摘要： The invention relates to a mould for the preparation of shaped products, which mould possesses a body fabricated substantially from a cement-comprising composition (7). The mould face of the mould is proved with a coating comprising at least a layer of thermosetting plastic (4) bordering on the mould body. On the interface a bonding agent is present which consists of a single layer of closely adjacent metal particles (5), which metal particles are partially embedded in the layer of thermosetting plastic (4) and are at least bonded to it by chemical bonds. The metal particle surfaces (8) that are not in contact with the plastic are entirely surrounded by cement, yielding at least a mechanical anchoring in the mould body.
摘要翻译：本发明涉及一种用于制备成型产品的模具，该模具具有基本上由含水泥的组合物（7）制成的主体。模具的模具表面被证明具有至少一层邻近模具体的热固性塑料层（4）的涂层。在界面上，存在由单层紧密相邻的金属颗粒（5）组成的粘合剂，该金属颗粒部分地嵌入热固性塑料层（4）中，并且至少通过化学键与其键合。与塑料不接触的金属颗粒表面（8）完全被水泥包围，至少在模具体中产生机械锚定。

9. 发明申请

US20120295019A1 COMPLETE TOOLING PACKAGES FOR MOLD BUILDING STRUCTURES 审中-公开
标题翻译：模具建筑结构的完整工具包
公开(公告)号：US20120295019A1
公开(公告)日：2012-11-22
申请号：US13444616
申请日：2012-04-11
申请人： Randall Lake , Robert Mark Adams , Brian Michael Kruchten , John Pfaff , Louis Paul Schaefer , Helena Twardowska
发明人： Randall Lake , Robert Mark Adams , Brian Michael Kruchten , John Pfaff , Louis Paul Schaefer , Helena Twardowska
IPC分类号： B28B7/36 , B28B1/52
CPC分类号： B29C33/3807 , B29C33/301 , B29D30/30 , B29K2867/06 , B29K2875/00 , B32B27/08 , B32B27/18 , B32B27/36
摘要： Tooling packages for mold building structures, mold structures, and methods of making mold structures are described.
摘要翻译：描述了模具建筑结构的模具包，模具结构以及制造模具结构的方法。

10. 发明申请

US20120135147A1 HIGH BUILD LOW TEMPERATURE EXOTHERM EXTRUDABLE MATERIAL 审中-公开
标题翻译：高温低温EXOTHERM挤出材料
公开(公告)号：US20120135147A1
公开(公告)日：2012-05-31
申请号：US13302590
申请日：2011-11-22
申请人： Helena Twardowska , Cameron Giffen , Louis Paul Schaefer , Randall Lake
发明人： Helena Twardowska , Cameron Giffen , Louis Paul Schaefer , Randall Lake
IPC分类号： B05D7/00 , B05D3/12 , B05D3/00 , C08L75/14 , C08L33/04
CPC分类号： C08G18/68 , B29C70/025 , B29C70/66 , B29K2867/06 , B29K2875/00
摘要： A high build tooling compound suited for plug building by extrusion process with conventional FRP dispensing equipment is described. The material is based on urethane hybrid and unsaturated polyester resin mixture with additives to provide low shrinkage and low exotherm. The formulation allows building a desired part thicknesses from 0.5 to 3 inches in one application. Methods of making a plug are also described.
摘要翻译：描述了适用于通过挤出工艺与传统FRP分配设备进行塞子建造的高成型加工组合物。该材料基于具有添加剂的聚氨酯混合和不饱和聚酯树脂混合物，以提供低收缩率和低放热性。该配方允许在一个应用中构建0.5至3英寸的所需部分厚度。还描述了制作插头的方法。

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