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    Reinforcing material for the local reinforcement of a component formed with a composite material, and method
    1.
    发明授权
    Reinforcing material for the local reinforcement of a component formed with a composite material, and method 有权
    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。

    Reinforcing Material for the Local Reinforcement of a Component Formed With a Composite Material, and Method
    2.
    发明申请
    Reinforcing Material for the Local Reinforcement of a Component Formed With a Composite Material, and Method 有权
    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。

    Core member for fabrication of shaped plastic
    5.
    发明授权
    Core member for fabrication of shaped plastic 失效
    成型塑料制造的核心成员

    公开(公告)号：US4939020A

    公开(公告)日：1990-07-03

    申请号：US210965

    申请日：1988-06-24

    申请人： Katsuhiko Takashima ,  Katsuhiro Moriwaki

    发明人： Katsuhiko Takashima ,  Katsuhiro Moriwaki

    IPC分类号： B29C70/00 ,  B29C33/40 ,  B29C33/76 ,  B29C44/22 ,  B29C70/66 ,  B29K105/08 ,  C08G75/00 ,  C08J9/32 ,  D04H1/645

    CPC分类号： B29C44/22 ,  B29C33/40 ,  B29C70/66 ,  C08G75/00 ,  C08J9/32 ,  B29C33/76 ,  B29K2105/0854 ,  B29K2105/165 ,  B29K2867/06 ,  Y10T428/249985 ,  Y10T442/652

    摘要： The invention core member is prepared by treatment of non-woven fabric with a coating composition which comprises an emulsion-form curable vinyl polymer, heat-expandable microspheres, and a thiocyanate compound, and this core member is advantageously utilized with use of liquid-form unsaturated polyester-based molding composition which contains a cobalt-containing compound as cure accelerator, wherein color development becomes available when said unsaturated polyester-based liquid composition infiltrates into voids of the core member, due to encounter of the thiocyanate compound with the cobalt-containing compound, thereby infiltration of said liquid composition is monitored by use of the color development.

    摘要翻译： 通过用包含乳液形式的可固化乙烯基聚合物，热膨胀性微球和硫氰酸酯化合物的涂料组合物处理无纺织物来制备本发明芯构件，并且该芯构件有利地利用液体形式 含有含钴化合物作为固化促进剂的不饱和聚酯类模塑组合物，其中当所述不饱和聚酯基液体组合物渗透到芯构件的空隙中时，由于与含钴的 化合物，从而通过使用显色来监测所述液体组合物的渗透。