Infusion method and flow aid
    1.
    发明授权
    Infusion method and flow aid 有权
    输液方法和流量辅助

    公开(公告)号:US09156208B2

    公开(公告)日:2015-10-13

    申请号:US13519935

    申请日:2010-12-29

    IPC分类号: B29C70/44 B29C70/54 B29C70/02

    摘要: Disclosed is an infusion method for the manufacture of a fiber-reinforced composite component with a flow promoter, wherein the flow velocity of the matrix material in a component to be infiltrated is modified by means of the flow promoter. Also disclosed is a flow promoter, which has an integral body section for the modification of the flow velocity.

    摘要翻译: 公开了一种用于制造具有流动促进剂的纤维增强复合材料组分的输注方法,其中通过流动促进剂改变要渗透的组分中的基质材料的流速。 还公开了一种流动促进器,其具有用于改变流速的整体主体部分。

    INFUSION METHOD AND FLOW AID
    2.
    发明申请
    INFUSION METHOD AND FLOW AID 有权
    输注方法和流量辅助

    公开(公告)号:US20130099426A1

    公开(公告)日:2013-04-25

    申请号:US13519935

    申请日:2010-12-29

    IPC分类号: B29C70/02

    摘要: Disclosed is an infusion method for the manufacture of a fibre-reinforced composite component with a flow promoter 18, wherein the flow velocity of the matrix material in a component 22 to be infiltrated is modified by means of the flow promoter 18; also disclosed is a flow promoter 18, which has an integral body section 20 for the modification of the flow velocity.

    摘要翻译: 公开了一种用于制造具有流动促进器18的纤维增强复合材料部件的输注方法,其中通过流动促进器18改变要渗透的部件22中的基质材料的流速; 还公开了一种流动促进器18,其具有用于改变流速的整体主体部分20。

    INFUSION METHOD AND A SYSTEM FOR AN INFUSION METHOD
    3.
    发明申请
    INFUSION METHOD AND A SYSTEM FOR AN INFUSION METHOD 审中-公开
    输注方法和一种用于输注方法的系统

    公开(公告)号:US20130069286A1

    公开(公告)日:2013-03-21

    申请号:US13519947

    申请日:2010-12-29

    IPC分类号: B29C70/36

    摘要: Disclosed is an infusion method for the manufacture of a fibre-reinforced composite component with semi-finished textile products in an open moulding tool, in which at least one local gas reception space is designed for the reception of volatile substances, such as resin gases and residual air contained in the matrix material and/or in the system, which gas reception space is blocked off from the matrix material by a local semi-permeable membrane; also disclosed is a system for the execution of such a method.

    摘要翻译: 公开了一种用于在开放模制工具中制造具有半成品纺织品的纤维增强复合部件的输注方法,其中至少一个局部气体接收空间被设计用于接收诸如树脂气体的挥发性物质, 包含在基体材料和/或系统中的残留空气,该气体接收空间被局部半透膜从基质材料中被阻挡; 还公开了一种用于执行这种方法的系统。

    Tool for the production of fiber composite components
    5.
    发明申请
    Tool for the production of fiber composite components 审中-公开
    用于生产纤维复合材料的工具

    公开(公告)号:US20080044506A1

    公开(公告)日:2008-02-21

    申请号:US11893028

    申请日:2007-08-14

    IPC分类号: B29C70/36

    CPC分类号: B29C70/443 B29C70/548

    摘要: The present invention provides a tool for the production of fiber composite components. The tool has a surface for depositing semifinished fiber products on the surface, the surface having a number of openings for feeding a matrix to the deposited semifinished fiber products. It is consequently possible to dispense entirely or partly with a conventional flow promoter and possible to achieve a high quality of fiber composite component.

    摘要翻译: 本发明提供了一种用于生产纤维复合材料组件的工具。 该工具具有用于在表面上沉积半成品纤维产品的表面,该表面具有用于将基质供给到沉积的半成品纤维产品的许多开口。 因此,可以完全或部分地用常规流动促进剂分配并且可能实现高质量的纤维复合材料组分。

    STRUCTURAL ELEMENT FOR AN AIRCRAFT OR SPACECRAFT AND METHOD FOR PRODUCING SUCH A STRUCTURAL ELEMENT
    6.
    发明申请
    STRUCTURAL ELEMENT FOR AN AIRCRAFT OR SPACECRAFT AND METHOD FOR PRODUCING SUCH A STRUCTURAL ELEMENT 有权
    用于制造这种结构元件的飞机或间隙的结构元件和方法

    公开(公告)号:US20120020801A1

    公开(公告)日:2012-01-26

    申请号:US13189743

    申请日:2011-07-25

    摘要: The present invention provides a structural element, in particular for an aircraft or spacecraft, comprising a core, the material density of which varies, at least in portions, in order to optimise the natural vibration behaviour of the structural element. The present invention further provides a method for producing a structural element, in particular for an aircraft or spacecraft, comprising the following steps: providing a structural element which has a core; determining the natural vibration behaviour of the structural element; and varying the material density of the core of the structural element, at least in portions, in such a way that the natural vibration behaviour of the structural element is optimised. The present invention provides still further an aircraft or spacecraft and a rotor blade, in particular for a wind turbine, comprising such a structural element.

    摘要翻译: 本发明提供了一种特别是飞机或航天器的结构元件,其包括至少部分地改变其材料密度的芯,以便优化结构元件的固有振动特性。 本发明还提供一种用于制造特别是飞行器或航天器的结构元件的方法,包括以下步骤:提供具有芯的结构元件; 确定结构元件的自然振动行为; 并且至少部分地改变结构元件的芯的材料密度,使得优化结构元件的固有振动特性。 本发明还提供一种飞机或航天器和特别是用于风力涡轮机的转子叶片,其包括这种结构元件。

    Reinforcing material for the local reinforcement of a component formed with a composite material, and method
    7.
    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

    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。

    Rod-shaped fibre composite, and method and device for the production thereof
    8.
    发明授权
    Rod-shaped fibre composite, and method and device for the production thereof 失效
    棒状纤维复合材料及其制造方法和装置

    公开(公告)号:US08104392B2

    公开(公告)日:2012-01-31

    申请号:US11921658

    申请日:2006-06-08

    IPC分类号: D04C1/00

    摘要: The invention relates to a rod-shaped fiber composite material (400) composed of a matrix (412) and a circular braid (402) embedded into the matrix. To increase the stability of the fiber composite material (400) and also to perform ducting functions for electricity and fluids, the wall of the circular braid is provided with wall chambers (408) which are separated by a phase boundary from the matrix (412) of the fiber composite material (400). These wall chambers (408) lead to inner and outer sections of the wall of the circular braid (402) being spaced apart, which is useful for the stability with regard to flexing and torsional loading in particular. Rod-shaped fiber composite materials (400) according to the invention can be used for creating stable structural components as well as for producing efficiently protected ducts. The invention further relates to an apparatus and a process which are useful for producing fiber composite material according to the invention.

    摘要翻译: 本发明涉及一种由矩阵(412)和嵌入矩阵中的圆形编织物(402)组成的棒状纤维复合材料(400)。 为了增加纤维复合材料(400)的稳定性并且还对电和流体进行管道功能,圆形编织物的壁上设置有由基体(412)相分离的壁室(408) 的纤维复合材料(400)。 这些壁室(408)通向圆形编织物(402)的壁的内部和外部部分被间隔开,这对于在特定的弯曲和扭转载荷方面的稳定性是有用的。 根据本发明的棒状纤维复合材料(400)可以用于产生稳定的结构部件以及用于生产有效保护的管道。 本发明还涉及一种可用于生产根据本发明的纤维复合材料的设备和方法。

    Reinforcing Material for the Local Reinforcement of a Component Formed With a Composite Material, and Method
    9.
    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

    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。

    Device And Method For Draping And Pre-Shaping Curved Profiled Structural Components Of Fiber Materials
    10.
    发明申请
    Device And Method For Draping And Pre-Shaping Curved Profiled Structural Components Of Fiber Materials 有权
    纤维材料的成型和预成型弯曲结构部件的装置和方法

    公开(公告)号:US20100252179A1

    公开(公告)日:2010-10-07

    申请号:US12575747

    申请日:2009-10-08

    IPC分类号: B65H81/00

    摘要: A device (10) for draping and pre-shaping curved profiled structural components of fiber materials comprises at least one shaping tool (20) having a curved shaping face (36) which has a profiled cross-section and which defines the outer contour of the profiled structural component, a plurality of unwinding devices (12a-12g) each for discharging a web-like fiber material (14a-14g), a device for performing a relative movement between the shaping tool (20) and the plurality of unwinding devices (12a-12g) for tangentially winding the web-like fiber materials (14a-14g) onto the curved shaping face (36) under tension, and a fixing device (22) for finally fixing the shape of all of the web-like fiber materials (14a-14g) wound on the curved shaping face (36).

    摘要翻译: 用于覆盖和预成型弯曲成型的纤维材料结构部件的装置(10)包括至少一个具有弯曲成形面(36)的成形工具(20),该成形工具具有成型横截面并限定了外形轮廓 成型结构部件,用于排出网状纤维材料(14a-14g)的多个展开装置(12a-12g),用于在成形工具(20)和多个退绕装置之间执行相对移动的装置 12a-12g),用于将卷状纤维材料(14a-14g)在张力下切向卷绕到弯曲成形面(36)上,以及用于最终固定所有网状纤维材料形状的定影装置(22) (14a-14g)缠绕在弯曲成形面(36)上。