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    FLEXIBLE PIPE HAVING PRESSURE ARMOUR LAYER AND COMPONENTS THEREOF
    62.
    发明申请
    FLEXIBLE PIPE HAVING PRESSURE ARMOUR LAYER AND COMPONENTS THEREOF 有权
    具有压力铠装层及其组件的柔性管道

    公开(公告)号：US20110247695A1

    公开(公告)日：2011-10-13

    申请号：US13128845

    申请日：2009-10-30

    申请人： Geoffrey Stephen Graham

    发明人： Geoffrey Stephen Graham

    IPC分类号： F15D1/00 ,  B32B37/00 ,  C09J7/02 ,  F16L11/00 ,  B32B3/30

    CPC分类号： F16L11/082 ,  E21B17/01 ,  F16L11/16 ,  Y10T137/0318 ,  Y10T428/12389 ,  Y10T428/24479 ,  Y10T428/24521 ,  Y10T428/24612

    摘要： An elongate metallic or polymeric or composite tape is disclosed along with a method of manufacturing such tape. The tape is of a type suitable for forming at least one helically wound layer of interlocked windings in a flexible pipe body for transporting production fluids. The tape is configured for interlocking of adjacent windings in the layer of tape by nesting a hooked region of a winding in a valley region of an adjacent winding. The tape comprises first and second elongate tape elements arranged in contacting relation.

    摘要翻译： 公开了一种细长的金属或聚合物或复合带以及制造这种带的方法。 该带是适合于在柔性管体中形成用于输送生产流体的互锁绕组的至少一个螺旋缠绕层的类型。 带被配置为通过在相邻绕组的谷区域中嵌套绕组的钩形区域来将带的相邻绕组互锁。 带包括以接触关系布置的第一和第二细长带元件。

    STRUCTURAL ELEMENT FOR REINFORCING A FUSELAGE OF AN AIRCRAFT
    64.
    发明申请
    STRUCTURAL ELEMENT FOR REINFORCING A FUSELAGE OF AN AIRCRAFT 有权
    用于加固飞机的结构的结构元件

    公开(公告)号：US20110236711A1

    公开(公告)日：2011-09-29

    申请号：US13081943

    申请日：2011-04-07

    申请人： Nikolaus Ohrloff ,  Thomas Beumler ,  Derk Daverschot ,  Matthijs Plokker

    发明人： Nikolaus Ohrloff ,  Thomas Beumler ,  Derk Daverschot ,  Matthijs Plokker

    IPC分类号： B32B15/08 ,  B32B7/12 ,  B32B7/08 ,  B32B5/02 ,  B32B3/00

    CPC分类号： B64C1/065 ,  B64C1/12 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10T428/12347 ,  Y10T428/12389 ,  Y10T428/12486 ,  Y10T428/12569 ,  Y10T428/24 ,  Y10T428/24612 ,  Y10T428/31678

    摘要： A structural element for reinforcing a fuselage cell of an aircraft is provided. The structural element comprises a reinforcement profile which is made in one piece from a metallic material. The profile is provided with a strap at least in regions. As a result of the strap which is made of a fibre-reinforced layer material or fibre metal laminate and is adhesively bonded, at least in regions, to a flange of the reinforcement profile the structural element has high damage tolerance and advantageous fatigue properties. The fibre metal laminate or layer material is made of a plurality of metal layers and fibre-reinforced plastics material layers which are stacked in alternating fashion and adhesively bonded to one another over the entire surface. The reinforcement profile and the strap are joined by means of a joining layer. Said joining layer is preferably constructed from two prepreg layers and a non-fibre-reinforced adhesive layer.

    摘要翻译： 提供了一种用于加强飞机的机身单元的结构元件。 结构元件包括由金属材料制成一体的加强型材。 该轮廓至少在区域中设置有带。 作为由纤维增强层材料或纤维金属层压材料制成的带材的结果，至少在区域中粘合地结合到增强轮廓的凸缘上，该结构元件具有高损伤容限和有利的疲劳性能。 纤维金属层压体或层材料由多个金属层和纤维增强塑料材料层制成，这些层以交替的方式堆叠并且在整个表面上彼此粘合。 加强轮廓和带通过接合层连接。 所述接合层优选由两个预浸料层和非纤维增强的粘合剂层构成。

    Tubular product and manufacturing method and manufacturing device thereof
    66.
    发明授权
    Tubular product and manufacturing method and manufacturing device thereof 有权
    管状产品及其制造方法及其制造装置

    公开(公告)号：US08020422B2

    公开(公告)日：2011-09-20

    申请号：US12044414

    申请日：2008-03-07

    申请人： Yukitaka Kunimoto ,  Toshiya Saito

    发明人： Yukitaka Kunimoto ,  Toshiya Saito

    IPC分类号： B21D17/04 ,  B21D31/00 ,  B21D51/02

    CPC分类号： B21H7/187 ,  Y10T428/12382 ,  Y10T428/12389

    摘要： A tubular product comprises a side section having outer surfaces disposed along a parallelogram and a bottom section formed on one end of the side section. The outer surfaces of the side section are pressure formed by a roller. The tubular product preferably is manufactured from a tubular material by a process comprising the use of a device having a roller that is configured to engage with a side section of the tubular material. The device also comprises a mandrel configured to position the tubular material so that the roller can apply pressure against at least a portion of the outer surfaces of the side section and can extend the side section of the tubular material to form the product.

    摘要翻译： 管状产品包括具有沿平行四边形设置的外表面的侧部分和形成在侧部的一端上的底部部分。 侧部的外表面是由辊形成的压力。 管状产品优选地通过包括使用具有被配置成与管状材料的侧部部分接合的辊的装置的方法由管状材料制成。 该装置还包括心轴，所述心轴构造成定位管状材料，使得辊可以对侧部的至少一部分外表面施加压力，并且可以延伸管状材料的侧部以形成产品。

    Slide Surface and Surface Processing Method of the Same
    69.
    发明申请
    Slide Surface and Surface Processing Method of the Same 有权
    滑动表面和表面处理方法

    公开(公告)号：US20110189439A1

    公开(公告)日：2011-08-04

    申请号：US13008639

    申请日：2011-01-18

    申请人： Akinobu Sato ,  Akiko Suzuki ,  Takeshi Kawano

    发明人： Akinobu Sato ,  Akiko Suzuki ,  Takeshi Kawano

    IPC分类号： B32B3/30 ,  C23F4/00

    CPC分类号： H01J37/3056 ,  B21D37/18 ,  B32B3/30 ,  C23F4/00 ,  H01J37/317 ,  Y10T428/12389 ,  Y10T428/24355 ,  Y10T428/24446 ,  Y10T428/24479

    摘要： A slide part has a surface structure in which there are at least two periodic structures among a first periodic structure with a period of 10 nm to 100 nm inclusive and a depth of 5 nm to 50 nm inclusive, a second periodic structure with a period of 100 nm to 1000 nm inclusive and a depth of 20 nm to 500 nm inclusive, and a third periodic structure with a period of 1000 nm to 10000 nm inclusive and a depth of 100 nm to 3000 nm inclusive, in which one of the at least two periodic structures is formed on the other periodic structure.

    摘要翻译： 滑动部件具有表面结构，其中在具有10nm至100nm的周期和包括端点在内的5nm至50nm的深度的第一周期性结构中存在至少两个周期性结构，第二周期性结构具有周期为 100nm至1000nm，包括深度为20nm至500nm的第三周期结构，以及包括端值在内的1000nm至10000nm的周期和深度为100nm至3000nm的第三周期结构，其中至少 在另一个周期性结构上形成两个周期性结构。

    COMPOSITE CAST TOOL
    70.
    发明申请
    COMPOSITE CAST TOOL 有权
    复合铸造工具

    公开(公告)号：US20110052933A1

    公开(公告)日：2011-03-03

    申请号：US12920886

    申请日：2009-03-05

    申请人： Christer Svensson ,  Tomas Nilsson

    发明人： Christer Svensson ,  Tomas Nilsson

    IPC分类号： B32B15/01 ,  B32B3/30

    CPC分类号： B22D19/16 ,  B22D19/06 ,  Y10T428/12389 ,  Y10T428/12958

    摘要： A composite cast tool is cast in one continuous piece, partly of steel and partly of grey iron, so that an interconnection zone is formed between the steel and the grey iron. The steel portion forms the working component of the tool, for example a cutting edge, and the grey iron portion forms the body component of the tool. The steel portion and the grey iron portion have projections or walls extending towards one another. The interconnection zone is located in the region of union between these walls and is planar.

    摘要翻译： 复合铸造工具铸造在一个连续的部件中，部分由钢制成，部分是灰铸铁，从而在钢和灰铸铁之间形成互连区。 钢部分形成工具的工作部件，例如切削刃，灰铸铁部分形成工具的主体部件。 钢部分和灰铸铁部分具有朝向彼此延伸的突出部或壁部。 互连区域位于这些壁之间的并联区域中并且是平面的。