利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

979 条记录 (耗时 0.026 秒)

    WIRE HARNESS
    82.
    发明公开
    WIRE HARNESS 有权
    线束

    公开(公告)号：EP2665143A1

    公开(公告)日：2013-11-20

    申请号：EP11855414.6

    申请日：2011-12-20

    申请人： Yazaki Corporation

    发明人： GOTOU, Hiroki ,  KAWAGUCHI, Kenichirou ,  TSUNODA, Mitsunori

    IPC分类号： H02G3/04 ,  F16B19/00 ,  H01B7/00

    CPC分类号： H01B7/0045 ,  B60R16/0215 ,  F16B5/0642 ,  F16B11/006 ,  F16B21/086 ,  H02G3/0487 ,  H02G3/305

    摘要： A wire harness is provided which can be attached to an attached body in a simple and inexpensive way, and a wire harness is provided so that the pitch precision with which clamps are attached to the wire harness can be improved and the man hours taken to assemble the wire harness can be reduced.
    A wire harness (13) is packaged by one-sided adhesive sheet (17) which hold clamps (33) in a plurality of sheet holes (31) which are opened at a predetermined pitch in accordance with positions where an attached body (43) is attached. It is desired that a surface material (15) at the side opposite to the adhesive surface of the one-sided adhesive sheet (17) has waterproofness. The positions of the sheet holes (31) which are bored through the one-sided adhesive sheet (17) and through which the clamps (33) are inserted may be offset from the positions X where the wire harness (13) is wired. The clamps (33) have shafts (39) which are inserted through the sheet holes (31) and which may be smaller in diameter than the sheet holes (31) to make it possible to adjust the pitch.

    摘要翻译： 提供了一种线束，其能够以简单和廉价的方式附接到附接体上，并且线束被设置为使得可以提高夹具附接到线束的间距精度并且组装所需的工时 线束可以减少。 线束（13）通过将夹具（33）保持在多个片孔（31）中的单面粘合片（17）包装，多个片孔（31）根据安装体（43）的位置以预定间距打开， 被附上。 期望在单面粘合片（17）的粘合面的相反侧的表面材料（15）具有防水性。 穿过单面粘合片（17）钻出并且夹具（33）插入的片孔（31）的位置可以从线束（13）布线的位置X偏移。 夹具（33）具有插入穿过片孔（31）的轴（39）并且其直径可以小于片孔（31）的直径以便能够调节节距。

    FASTENING ARRANGEMENT AND FASTENING FITTING FOR FASTENING A COMPONENT TO A STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT
    83.
    发明公开
    FASTENING ARRANGEMENT AND FASTENING FITTING FOR FASTENING A COMPONENT TO A STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT 有权
    安装装置和固定部件，用于固定组件的一个组成部分飞机或航天器的结构

    公开(公告)号：EP2651758A2

    公开(公告)日：2013-10-23

    申请号：EP11799277.6

    申请日：2011-12-13

    申请人： Airbus Operations GmbH

    发明人： KLAUKIEN, Frank-Michael

    IPC分类号： B64C1/40

    CPC分类号： F16B17/002 ,  A47G1/17 ,  B64C1/406 ,  B64G1/66 ,  F16B11/006 ,  F21V21/0808 ,  Y02T50/46 ,  Y10T403/472

    摘要： A fastening arrangement for fastening a component, in particular a cabin component, to a structural component of an aircraft or spacecraft, including a structural component which has a connection surface; a fastening fitting which has a geometry matched to the geometrical shape of the structural component, has a connection portion associated with the connection surface of the structural component and is produced from a thermoplastic injection-moulding material; and an elastomeric adhesive joint for stable fastening of the connection portion of the fastening fitting to the associated connection surface of the structural component. A corresponding fastening fitting and an aircraft or spacecraft comprising a fastening arrangement of this type and/or a fastening fitting of this type are also described.

    摘要翻译： 用于将部件紧固，尤其是机舱部件，飞机或航天器，其中包括具有连接表面的结构部件的结构部件的紧固装置; 紧固配件其中有匹配于结构部件的几何形状的几何形状，具有与所述结构部件的连接表面相关联的连接部分和由热塑性注射成型的材料制成; 并且在用于紧固装配到结构部件的相关联的连接表面的连接部的稳定的固定弹性粘合剂接头。 相应的紧固配件和飞机或航天器包括这种类型和/或这种类型的紧固接头的紧固装置被如此描述。

    Fay surface sealant application
    89.
    发明公开
    Fay surface sealant application 有权
    Passflächen-Abdichtungsanwendung

    公开(公告)号：EP2518340A1

    公开(公告)日：2012-10-31

    申请号：EP12157277.0

    申请日：2012-02-28

    申请人： Sikorsky Aircraft Corporation

    发明人： Denavit, Paul H. ,  Hovan, William E. ,  Rogg, Christian A. ,  Bremmer, Jonathan ,  Sauer, Jeffrey G. ,  McNeill, Chandira

    IPC分类号： F16B43/00 ,  F16B11/00 ,  C09J5/00 ,  B64F5/00

    CPC分类号： F16B11/006 ,  C09J5/04 ,  Y10T156/10 ,  Y10T428/249923 ,  Y10T428/26 ,  Y10T428/31504

    摘要： A method of sealing between two components includes applying and curing a layer of fay surface sealant to a first component. A layer of liquid shim is applied to one or more of the first component and a second component. The first component is assembled to the second component with the layer of fay surface sealant and the layer of liquid shim therebetween. An assembly of two components includes a first component and a layer of fay surface sealant applied and cured to a first facing surface of the first component. A second component includes a second facing surface, such that the second facing surface and the layer of fay surface sealant define a gap therebetween. A layer of liquid shim is located between the second component and the layer of fay surface sealant thereby substantially filling the gap.

    摘要翻译： 在两个部件之间的密封方法包括将一层费用表面密封剂施加和固化到第一部件上。 一层液体垫片施加到第一部件和第二部件中的一个或多个。 将第一部件组装到第二部件上，并且其间具有散热表面密封剂层和液体垫片。 两个组件的组件包括施加并固化到第一部件的第一面对表面的第一部件和一个散热表面密封剂层。 第二组件包括第二面对表面，使得第二面对表面和费用表面密封剂层在其之间形成间隙。 一层液体垫片位于第二部件和费用表面密封剂层之间，从而基本上填充间隙。