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    ELECTRIC POWER TRANSMISSION CABLE COMPRISING CONTINUOUSLY SYNTHESIZED TITANIUM ALUMINIDE INTERMETALLIC COMPOSITE WIRE
    4.
    发明申请
    ELECTRIC POWER TRANSMISSION CABLE COMPRISING CONTINUOUSLY SYNTHESIZED TITANIUM ALUMINIDE INTERMETALLIC COMPOSITE WIRE 审中-公开
    电力传输电缆，包含连续合成的钛酸铝中间复合线

    公开(公告)号：WO2012108980A1

    公开(公告)日：2012-08-16

    申请号：PCT/US2012/021617

    申请日：2012-01-17

    Applicant: HOLLOWAY, Scott, Richard

    Inventor： HOLLOWAY, Scott, Richard

    IPC: C22C14/00

    CPC classification number: C22C14/00 ,  B22D11/005 ,  H01B1/023

    Abstract: A method of manufacturing wire comprising aluminum oxide particles formed in situ in a fully dense matrix of titanium aluminide intermetallic material by means of the combustion synthesis of aluminum and titanium oxide followed by thermo-mechanical forming. The pre-combustion aluminum may be elemental, or an aluminum alloy containing one or more of the elements vanadium, niobium, molybdenum, or boron. The preferred embodiment of the present invention is an electric power transmission cable comprising a plurality of wires manufactured according to the present invention.

    Abstract translation: 一种制造线材的方法，其包括通过铝和氧化钛的燃烧合成然后进行热机械成型而在铝铝化物金属间化合物材料的完全致密基质中原位形成的氧化铝颗粒。 预燃铝可以是元素的，或含有钒，铌，钼或硼中的一种或多种元素的铝合金。 本发明的优选实施例是包括根据本发明制造的多根电线的电力传输电缆。

    SURGICAL INSTRUMENT
    5.
    发明申请
    SURGICAL INSTRUMENT 审中-公开
    手术器械

    公开(公告)号：WO2010112850A1

    公开(公告)日：2010-10-07

    申请号：PCT/GB2010/000633

    申请日：2010-03-31

    Applicant: MAIDSTONE & TUNBRIDGE WELLS NHS TRUST ,  SCOTT, Richard, Mark ,  HALL, Stephen, Addison

    Inventor： SCOTT, Richard, Mark ,  HALL, Stephen, Addison

    IPC: A61B10/02

    CPC classification number: A61B10/0266 ,  A61B10/0291 ,  A61B10/06 ,  A61B2010/0208 ,  A61B2017/2927 ,  A61B2017/32004

    Abstract: A surgical instrument (10) for removing a sample (50, 82) from a body of tissue (80) comprises a support structure (30) and a knife (32) arranged to cut into the body of tissue (80). The knife (32) has at least a first blade (36a), a second blade (36b) and a third blade (36c), and each blade has two cutting edges (42a, 44a; 42b, 44b; 42c, 44c) defining an apex. The knife (32) is movable between a first configuration in which the blades (36a, 36b, 36c) are substantially aligned along the longitudinal axis (X) of the support structure (30), and a second configuration in which the blades (36a, 36b, 36c) define the walls of a pyramidal enclosure for containing the sample (50, 82). In one embodiment, the instrument (10) further comprises a biasing member (52a, 52b, 52c) arranged to urge each blade (36a, 36b, 36c) towards the central axis (X) of the support structure (30). In another embodiment, the instrument (10) further comprises a plunger (72) disposed in, and being axially movable in a longitudinal direction along, the support structure (30). The plunger (72) is arranged to move the knife (32) between the first configuration and the second configuration.

    Abstract translation: 用于从组织体（80）去除样品（50,82）的外科器械（10）包括支撑结构（30）和布置成切入组织体（80）的刀（32）。 刀具（32）至少具有第一刀片（36a），第二刀片（36b）和第三刀片（36c），并且每个刀片具有两个切割边缘（42a，44a; 42b，44b; 42c，44c） 一个顶点 所述刀（32）可在其中所述刀片（36a，36b，36c）沿着所述支撑结构（30）的纵向轴线（X）基本上对准的第一构造和第二构造（第二构造，其中所述刀片 ，36b，36c）限定用于容纳样品（50,82）的金字塔形外壳的壁。 在一个实施例中，仪器（10）还包括偏置构件（52a，52b，52c），该偏压构件（52a，52b，52c）朝着支撑结构（30）的中心轴线（X）推动每个叶片（36a，36b，36c）。 在另一个实施例中，仪器（10）还包括柱塞（72），该柱塞（72）沿着支撑结构（30）沿着纵向方向设置并且可轴向移动。 柱塞72设置成在第一配置和第二配置之间移动刀具32。

    EXTRUSION RESISTANT GASKET FACE SEAL
    6.
    发明申请
    EXTRUSION RESISTANT GASKET FACE SEAL 审中-公开
    防挤压垫面

    公开(公告)号：WO2010019296A2

    公开(公告)日：2010-02-18

    申请号：PCT/US2009/043872

    申请日：2009-05-14

    Applicant: GENERAL ELECTRIC COMPANY ,  RAO, Justin, Sanjay ,  ZEARBAUGH, Scott, Richard

    Inventor： RAO, Justin, Sanjay ,  ZEARBAUGH, Scott, Richard

    IPC: F16J15/06 ,  F16L23/16 ,  F16J15/16 ,  F16L23/02

    CPC classification number: F16L23/18 ,  F16J15/104 ,  F16J15/127

    Abstract: A seal assembly for a fluid coupling includes: (a) a generally planar, substantially rigid seal retainer with opposed first and second faces, having an annular first groove formed in the first face; (b) a first resilient seal disposed in the first groove; and (c) an annular first backup ring positioned radially outboard of the first resilient seal and secured to the first resilient seal, wherein the first backup ring is substantially harder than the first resilient seal.

    Abstract translation: 用于流体联接的密封组件包括：（a）具有相对的第一和第二表面的大致平面的基本刚性的密封保持器，其具有形成在第一面中的环形第一凹槽; （b）设置在第一槽中的第一弹性密封件; 和（c）环形的第一支撑环，其定位在第一弹性密封件的径向外侧并且固定到第一弹性密封件，其中第一支撑环基本上比第一弹性密封件更硬。

    COOLED DUCT FOR GAS TURBINE ENGINE
    9.
    发明申请
    COOLED DUCT FOR GAS TURBINE ENGINE 审中-公开
    用于气体涡轮发动机的冷却塔

    公开(公告)号：WO2006059119A1

    公开(公告)日：2006-06-08

    申请号：PCT/GB2005/004617

    申请日：2005-12-01

    Applicant: UNITED TECHNOLOGIES CORPORATION ,  LECKEY, David, H. ,  COWAN, Curtis, C. ,  FARAH, Jorge, I. ,  KEHRET, Deborah, F. ,  KEYSA, Stanley ,  LAVIN, Jeffrey, R. ,  MURPHEY, Michael ,  PAUL, Stephen, A. ,  SCOTT, Richard

    Inventor： COWAN, Curtis, C. ,  FARAH, Jorge, I. ,  KEHRET, Deborah, F. ,  KEYSA, Stanley ,  LAVIN, Jeffrey, R. ,  MURPHEY, Michael ,  PAUL, Stephen, A. ,  SCOTT, Richard

    IPC: F02K1/82 ,  F02K1/00

    CPC classification number: F02K1/827 ,  F02K1/004 ,  F02K1/82 ,  F02K1/822 ,  Y02T50/675

    Abstract: A cooled exhaust duct (10) for use in gas turbine engines is provided. The cooled exhaust duct (10) includes an axial centerline (18), a circumference, an annulus (20), and a plurality of radially expandable bands (22). The annulus (20) is disposed between a first wall (24) and a second wall (26), and extends along the axial centerline (18). The first wall (24) is disposed radially inside of the second wall (26). Each of the plurality of radially expandable bands (22) extends circumferentially within the annulus (20). The bands (22) are axially spaced apart from one another. Each band (22) includes a first portion (32) attached to the first wall (24), a second portion (34) attached to the second wall (26) and an intermediate portion (36) connected to the first and second portions (32, 34). The bands (22) create circumferentially extending compartments that inhibit axial travel of the cooling air within the annulus (20).

    Abstract translation: 提供了一种用于燃气涡轮发动机的冷却排气管道（10）。 冷却的排气管道（10）包括轴向中心线（18），圆周，环形空间（20）和多个可径向扩张的带（22）。 环（20）设置在第一壁（24）和第二壁（26）之间，并且沿轴向中心线（18）延伸。 第一壁（24）径向设置在第二壁（26）的内部。 多个可径向扩张的带（22）中的每一个在环（20）内圆周地延伸。 带（22）彼此轴向间隔开。 每个带（22）包括附接到第一壁（24）的第一部分（32），附接到第二壁（26）的第二部分（34）和连接到第一和第二部分 32，34）。 带（22）形成周向延伸的隔室，其阻止环形空间（20）内的冷却空气的轴向移动。

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