Stabilising the honeycomb core for sandwich components
    1.
    发明授权
    Stabilising the honeycomb core for sandwich components 有权
    稳定三明治组件的蜂巢芯

    公开(公告)号:US09475266B2

    公开(公告)日:2016-10-25

    申请号:US14232638

    申请日:2012-07-10

    IPC分类号: B32B37/04 B32B3/12

    CPC分类号: B32B37/04 B32B3/12

    摘要: A method for stabilizing a honeycomb core for a sandwich-type structural component includes configuring the honeycomb core. A hardenable adhesive layer is applied to at least one exterior surface of the honeycomb core. A semi-permeable membrane is positioned on the at least one exterior surface. The membrane is gas-permeable and liquid-impermeable. Air in the honeycomb core is drawn off through the semi-permeable membrane. The adhesive layer is hardened.

    摘要翻译: 用于稳定夹层结构部件的蜂窝芯的方法包括构造蜂窝芯。 将可硬化的粘合剂层施加到蜂窝芯的至少一个外表面上。 半透膜位于至少一个外表面上。 膜是透气且不透液体的。 蜂窝芯中的空气通过半透膜被抽出。 粘合剂层硬化。

    Flying device with improved movement on the ground
    3.
    发明授权
    Flying device with improved movement on the ground 有权
    飞行装置具有改进的地面运动

    公开(公告)号:US07959104B2

    公开(公告)日:2011-06-14

    申请号:US11722739

    申请日:2005-12-22

    申请人: Julian Kuntz

    发明人: Julian Kuntz

    IPC分类号: B64C37/00

    摘要: The invention relates to a flying device which can efficiently move in the air by aerodynamic forces and by direct force transmission on the ground, without the need for independent drive and thrust generation systems for the two modes of movement. The rotors (1) of the flying device are provided on the outside thereof with an annular rotating covering (4), connected directly to the rotor blade tips, which, when the flying device is on the ground and the rotor rotational axes (2) are correspondingly pitched about an axis (3), come into contact with the ground. The covering (4) hence permits a movement of the flying device on the ground by rolling, which is based on a direct force transfer to the ground. A further rotor pitching axis (5) permits the flying device to be controlled in the air and on the ground by means of the same actuator system. The above flying principle permits, for example, remote controlled reconnaissance drones for close or remote espionage, to independently enter inaccessible regions, or in the context of police or military application in buildings presenting danger for personnel, to gain access to upper floors.

    摘要翻译: 本发明涉及一种飞行装置,其可以通过空气动力力和通过在地面上的直接力传递而有效地在空气中移动,而不需要用于两种运动模式的独立的驱动和推力发生系统。 飞行装置的转子(1)在其外侧设置有环形旋转覆盖物(4),其直接连接到转子叶片尖端,当飞行装置在地面上时,转子旋转轴线(2) 相应地围绕轴线(3)倾斜,与地面接触。 因此,覆盖物(4)允许通过滚动将飞行装置在地面上的移动,其基于对地面的直接力传递。 另一个转子俯仰轴线(5)允许飞行装置通过相同的致动器系统被控制在空气中并在地面上。 上述飞行原则允许例如用于近距离或间接间谍的遥控侦察无人机,独立地进入无法进入的区域,或者在对人员造成危险的建筑物中的警察或军事应用情况下,进入较高楼层。

    STABILISING THE HONEYCOMB CORE FOR SANDWICH COMPONENTS
    4.
    发明申请
    STABILISING THE HONEYCOMB CORE FOR SANDWICH COMPONENTS 有权
    稳定三元组件的蜂窝电话核心

    公开(公告)号:US20140224408A1

    公开(公告)日:2014-08-14

    申请号:US14232638

    申请日:2012-07-10

    IPC分类号: B32B37/04

    CPC分类号: B32B37/04 B32B3/12

    摘要: A method for stabilising a honeycomb core for a sandwich-type structural component includes configuring the honeycomb core. A hardenable adhesive layer is applied to at least one exterior surface of the honeycomb core. A semi-permeable membrane is positioned on the at least one exterior surface. The membrane is gas-permeable and liquid-impermeable. Air in the honeycomb core is drawn off through the semi-permeable membrane. The adhesive layer is hardened.

    摘要翻译: 用于稳定夹层结构部件的蜂窝芯的方法包括构造蜂窝芯。 将可硬化的粘合剂层施加到蜂窝芯的至少一个外表面上。 半透膜位于至少一个外表面上。 膜是透气且不透液体的。 蜂窝芯中的空气通过半透膜被抽出。 粘合剂层硬化。

    Method for measuring and/or testing waviness of a planar textile
    6.
    发明授权
    Method for measuring and/or testing waviness of a planar textile 失效
    用于测量和/或测试平面纺织品波纹的方法

    公开(公告)号:US08573035B2

    公开(公告)日:2013-11-05

    申请号:US13120556

    申请日:2009-09-30

    IPC分类号: G01B5/28

    CPC分类号: G01B5/285 G01B13/22

    摘要: The invention relates to a method for measuring and/or testing a geometric design parameter, particularly waviness, of a planar textile (10), comprising the steps: disposing the planar textile (10) in an intermediate space (26) between a support (20) and a flexible film (22), applying a differential pressure (Δp) between the intermediate space (26) and the environment, so that the film (22) adapts to the planar textile (10), and capturing a surface profile (32) of the film (22).

    摘要翻译: 本发明涉及一种用于测量和/或测试平面织物(10)的几何设计参数,特别是波纹的方法,包括以下步骤:将平面织物(10)设置在支撑件(10)之间的中间空间(26) 20)和柔性膜(22),在中间空间(26)和环境之间施加差压(Deltap),使得膜(22)适应于平面织物(10),并且捕获表面轮廓 32)。

    Partially Fixated Semi-Finished Textile
    7.
    发明申请
    Partially Fixated Semi-Finished Textile 审中-公开
    部分固定的半成品纺织品

    公开(公告)号:US20120107596A1

    公开(公告)日:2012-05-03

    申请号:US13283830

    申请日:2011-10-28

    申请人: Julian KUNTZ

    发明人: Julian KUNTZ

    IPC分类号: B32B5/04 B32B38/00 B32B37/12

    摘要: A semi-finished textile for producing a fiber composite component part has a textile structure and a fixation structure so as to provide a semi-finished textile that can be easily handled and that is suitable for use in complex component part shapes. The textile structure includes a first multitude of reinforcement-fiber bundles of high-performance fibers. Displacement sections are formed between adjacent reinforcement-fiber bundles and adjacent reinforcement-fiber bundles can be displaced against each other. The fixation structure fixates the reinforcement-fiber bundles, depending on the textile structure, with a fixation pattern in such a way that the reinforcement-fiber bundles are fixated at least partially and the displacement sections remain at least partially free.

    摘要翻译: 用于生产纤维复合材料部件的半成品纺织品具有织物结构和固定结构,以便提供可以容易地处理并且适用于复杂部件形状的半成品织物。 纺织结构包括第一多种高性能纤维的增强纤维束。 在相邻的增强纤维束之间形成位移部分,并且相邻的增强纤维束可相对于彼此移位。 固定结构根据纺织结构固定增强纤维束,其具有固定图案,使得增强纤维束至少部分地固定,并且位移部分保持至少部分自由。

    Partially fixated semi-finished textile

    公开(公告)号:US10221511B2

    公开(公告)日:2019-03-05

    申请号:US13283830

    申请日:2011-10-28

    申请人: Julian Kuntz

    发明人: Julian Kuntz

    摘要: A semi-finished textile for producing a fiber composite component part has a textile structure and a fixation structure so as to provide a semi-finished textile that can be easily handled and that is suitable for use in complex component part shapes. The textile structure includes a first multitude of reinforcement-fiber bundles of high-performance fibers. Displacement sections are formed between adjacent reinforcement-fiber bundles and adjacent reinforcement-fiber bundles can be displaced against each other. The fixation structure fixates the reinforcement-fiber bundles, depending on the textile structure, with a fixation pattern in such a way that the reinforcement-fiber bundles are fixated at least partially and the displacement sections remain at least partially free.