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    • 7. 发明授权
    • Reinforcing material for the local reinforcement of a component formed with a composite material, and method
    • 用于复合材料形成的部件的局部增强的加强材料及方法
    • US08802224B2
    • 2014-08-12
    • US12223936
    • 2007-02-01
    • Axel Herrmann
    • Axel Herrmann
    • B32B15/08B32B7/02B05D5/10B32B27/00B32B27/08B32B27/32B32B17/10C09J7/02
    • B32B27/00B29C70/088B29C70/44B29K2705/00B29K2705/12B29K2705/14B29K2707/04B29K2863/00B29K2867/06B29K2995/0072B29L2031/3085B32B15/08B32B17/10761B32B27/08B32B27/32C09J7/22C09J7/38Y02T50/43Y10T428/24967Y10T428/28Y10T428/2852Y10T428/287Y10T428/2896
    • 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.
    • 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。
    • 9. 发明申请
    • Reinforcing Material for the Local Reinforcement of a Component Formed With a Composite Material, and Method
    • 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
    • US20100316857A1
    • 2010-12-16
    • US12223936
    • 2007-02-01
    • Axel Herrmann
    • Axel Herrmann
    • B32B15/08B32B7/02B05D5/10
    • B32B27/00B29C70/088B29C70/44B29K2705/00B29K2705/12B29K2705/14B29K2707/04B29K2863/00B29K2867/06B29K2995/0072B29L2031/3085B32B15/08B32B17/10761B32B27/08B32B27/32C09J7/22C09J7/38Y02T50/43Y10T428/24967Y10T428/28Y10T428/2852Y10T428/287Y10T428/2896
    • 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.
    • 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。