利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

7 条记录 (耗时 0.015 秒)

    Conductive Coupling Assembly
    5.
    发明申请
    Conductive Coupling Assembly 有权
    导电耦合组件

    公开(公告)号：US20130327888A1

    公开(公告)日：2013-12-12

    申请号：US13747732

    申请日：2013-01-23

    申请人： THE BOEING COMPANY

    发明人： Kevin O'Brien Gaw ,  Nathan Michael Kelley ,  John Thomas Axtell ,  James Patrick Irwin ,  David William Minteer ,  Diego A. Velasco

    IPC分类号： B64D45/02 ,  F17D1/00 ,  F16L25/02

    CPC分类号： B64D45/02 ,  B60R16/06 ,  B63B43/00 ,  F16L9/14 ,  F16L21/065 ,  F16L25/01 ,  F16L25/025 ,  F16L25/026 ,  F17D1/00 ,  F17D5/08 ,  H05F1/00 ,  Y10T137/8593

    摘要： A method and apparatus for conducting an electrical current between a first transport member and a second transport member. In one illustrative embodiment, a coupling assembly comprises a first fitting associated with a first end of a first transport member, a second fitting associated with a second end of a second transport member, and a seal. The seal is configured for placement around the first fitting and the second fitting when the first end of the first transport member is positioned relative to the second end of the second transport member. The seal is further configured to seal an interface between the first transport member and the second transport member. The seal is comprised of a material configured such that the seal has a level of conductivity within a selected range and such that a conductive pathway is formed between the first transport member and the second transport member.

    摘要翻译： 一种用于在第一输送构件和第二输送构件之间进行电流的方法和装置。 在一个说明性实施例中，联接组件包括与第一输送构件的第一端相关联的第一配件，与第二输送构件的第二端相关联的第二配件和密封件。 当第一输送构件的第一端相对于第二输送构件的第二端定位时，密封件构造成围绕第一配件和第二配件放置。 密封件进一步构造成密封第一输送构件和第二输送构件之间的界面。 密封件由构造成使得密封件具有在所选范围内的导电率水平并且使得在第一输送构件和第二输送构件之间形成导电通路的材料构成。

    Conductive coupling assembly
    6.
    发明授权
    Conductive coupling assembly 有权
    导电联轴器组件

    公开(公告)号：US09169029B2

    公开(公告)日：2015-10-27

    申请号：US13747732

    申请日：2013-01-23

    申请人： The Boeing Company

    发明人： Kevin O'Brien Gaw ,  Nathan Michael Kelley ,  John Thomas Axtell ,  James Patrick Irwin ,  David William Minteer ,  Diego A. Velasco

    IPC分类号： F16L25/01 ,  B64D45/02 ,  F16L25/02 ,  F17D1/00 ,  F16L9/14 ,  H05F1/00 ,  F16L21/06

    CPC分类号： B64D45/02 ,  B60R16/06 ,  B63B43/00 ,  F16L9/14 ,  F16L21/065 ,  F16L25/01 ,  F16L25/025 ,  F16L25/026 ,  F17D1/00 ,  F17D5/08 ,  H05F1/00 ,  Y10T137/8593

    摘要： A method and apparatus for conducting an electrical current between a first transport member and a second transport member. In one illustrative embodiment, a coupling assembly comprises a first fitting associated with a first end of a first transport member, a second fitting associated with a second end of a second transport member, and a seal. The seal is configured for placement around the first fitting and the second fitting when the first end of the first transport member is positioned relative to the second end of the second transport member. The seal is further configured to seal an interface between the first transport member and the second transport member. The seal is comprised of a material configured such that the seal has a level of conductivity within a selected range and such that a conductive pathway is formed between the first transport member and the second transport member.

    摘要翻译： 一种用于在第一输送构件和第二输送构件之间进行电流的方法和装置。 在一个说明性实施例中，联接组件包括与第一输送构件的第一端相关联的第一配件，与第二输送构件的第二端相关联的第二配件和密封件。 当第一输送构件的第一端相对于第二输送构件的第二端定位时，密封件构造成围绕第一配件和第二配件放置。 密封件进一步构造成密封第一输送构件和第二输送构件之间的界面。 密封件由构造成使得密封件具有在所选范围内的导电率水平并且使得在第一输送构件和第二输送构件之间形成导电通路的材料构成。

    Fluid Transport System for Preventing Electrical Discharge
    7.
    发明申请
    Fluid Transport System for Preventing Electrical Discharge 有权
    用于防止放电的流体输送系统

    公开(公告)号：US20130329333A1

    公开(公告)日：2013-12-12

    申请号：US13747780

    申请日：2013-01-23

    申请人： THE BOEING COMPANY

    发明人： David William Minteer ,  James Patrick Irwin ,  Benjamin A. Johnson ,  John Thomas Axtell

    IPC分类号： H05F1/00

    CPC分类号： B64D45/02 ,  B60R16/06 ,  B63B43/00 ,  F16L9/14 ,  F16L21/065 ,  F16L25/01 ,  F16L25/025 ,  F16L25/026 ,  F17D1/00 ,  F17D5/08 ,  H05F1/00 ,  Y10T137/8593

    摘要： A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. The aerospace vehicle is operated. The fluid transport system in the aerospace vehicle is comprised of materials selected such that the fluid transport system has an electrical configuration. The intensity of the electrical discharge that occurs within the fluid transport system during operation of the aerospace vehicle is reduced to within selected tolerances by the electrical configuration of the fluid transport system.

    摘要翻译： 一种用于降低在航空航天车辆的流体输送系统内发生的放电强度的方法和装置。 航空航天车辆运行。 航空航天车辆中的流体输送系统由选择的材料组成，使得流体输送系统具有电气结构。 通过流体输送系统的电气配置，在航空航天车辆的运行期间在流体输送系统内发生的放电强度降低到选定的公差内。