Rod-shaped fibre composite, and method and device for the production thereof
    11.
    发明申请
    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:US20090229452A1

    公开(公告)日:2009-09-17

    申请号:US11921658

    申请日:2006-06-08

    IPC分类号: D04C1/06 D04C3/00 D04C3/40

    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。

    Structural element for an aircraft or spacecraft and method for producing such a structural element
    13.
    发明授权
    Structural element for an aircraft or spacecraft and method for producing such a structural element 有权
    用于飞行器或航天器的结构元件和用于生产这种结构元件的方法

    公开(公告)号:US08882469B2

    公开(公告)日:2014-11-11

    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 optimize the natural vibration behavior 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 behavior 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 behavior of the structural element is optimized. 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。

    Device and method for draping and pre-shaping curved profiled structural components of fiber materials
    16.
    发明授权
    Device and method for draping and pre-shaping curved profiled structural components of fiber materials 有权
    纤维材料弯曲成型结构件的悬垂和预成型装置及方法

    公开(公告)号:US07972457B2

    公开(公告)日:2011-07-05

    申请号:US12575747

    申请日:2009-10-08

    IPC分类号: B29C70/32

    摘要: A device for draping and pre-shaping curved profiled structural components of fiber materials includes at least one shaping tool having a curved shaping face which has a profiled cross-section and which defines the outer contour of the profiled structural component. The device also includes a plurality of unwinding devices each for discharging a web-like fiber material, a device for performing a relative movement between the shaping tool and the plurality of unwinding devices for tangentially winding the web-like fiber materials onto the curved shaping face under tension, and a fixing device for finally fixing the shape of all of the web-like fiber materials wound on the curved shaping face. A method of draping and pre-shaping curved profiled structural components of fiber materials is also disclosed.

    摘要翻译: 一种用于覆盖和预成型的纤维材料弯曲成型结构部件的装置包括至少一个具有弯曲成形面的成型工具,该成型工具具有成型横截面并且限定成型结构部件的外部轮廓。 该装置还包括多个退绕装置,每个退绕装置用于排出网状纤维材料,用于在成形工具和多个退绕装置之间进行相对运动的装置,用于将卷状纤维材料切向卷绕到弯曲成形面 以及用于最终固定卷绕在弯曲成形面上的所有卷状纤维材料的形状的固定装置。 还公开了一种用于纤维材料的弯曲成型结构部件的覆盖和预成形的方法。

    APPARATUS AND METHOD FOR DRAPING KNITTED FIBER FABRICS FOR CURVED PROFILED STRUCTURAL PARTS OF FIBER COMPOSITE MATERIAL
    19.
    发明申请
    APPARATUS AND METHOD FOR DRAPING KNITTED FIBER FABRICS FOR CURVED PROFILED STRUCTURAL PARTS OF FIBER COMPOSITE MATERIAL 审中-公开
    针对纤维复合材料弯曲型材结构部件的针织纤维织物的缠绕装置和方法

    公开(公告)号:US20120090768A1

    公开(公告)日:2012-04-19

    申请号:US13264207

    申请日:2010-04-14

    IPC分类号: B32B37/18 B29C65/78

    摘要: An apparatus for draping knitted fiber fabrics for curved profiled structural parts of fiber composite material includes a mold having a mold surface that corresponds to a portion of the desired profile geometry and curvature of the profiled structural part, a clamping device for tensioning a layer of a knitted fiber fabric along a tensioning line in a prestressed state, and a movement device for producing a relative movement between the mold and the clamped-in fabric layer such that the mold surface moves close to the fabric layer in a direction perpendicular to the tensioning line and, in the further course of the relative movement, pushes through the tensioning line such that the fabric layer completely covers the mold surface. The clamping device is equipped to load the fabric layer during the entire draping operation with a tensile force acting along the tensioning line.

    摘要翻译: 一种用于覆盖纤维复合材料的弯曲成型结构部件的针织纤维织物的装置,包括具有对应于所需轮廓几何形状的一部分和成型结构部件的曲率的模具表面的模具,用于张紧一层 编织纤维织物沿着预张紧状态的张紧线,以及运动装置,用于在模具和夹紧的织物层之间产生相对运动,使得模具表面在垂直于张紧线的方向上靠近织物层移动 并且在相对运动的进一步过程中,推动张紧线,使得织物层完全覆盖模具表面。 夹紧装置装备在整个悬垂操作期间以沿着张紧线作用的张力来装载织物层。