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    TURBINE ENGINE HEAT RECUPERATOR PLATE AND PLATE STACK
    1.
    发明申请
    TURBINE ENGINE HEAT RECUPERATOR PLATE AND PLATE STACK 有权
    涡轮发动机加热板和板堆

    公开(公告)号：US20130199152A1

    公开(公告)日：2013-08-08

    申请号：US13365711

    申请日：2012-02-03

    申请人： David Harold MENHEERE ,  Andreas ELEFTHERIOU ,  Daniel T. ALECU ,  Quantai LIU

    发明人： David Harold MENHEERE ,  Andreas ELEFTHERIOU ,  Daniel T. ALECU ,  Quantai LIU

    IPC分类号： F02C7/10 ,  F28D7/00

    CPC分类号： F02C7/10 ,  F05D2260/37 ,  F28D9/0068 ,  F28D9/0087 ,  F28D21/0003 ,  F28D2021/0026 ,  F28F3/046 ,  F28F2225/04 ,  Y02T50/672

    摘要： A heat recuperator includes a plurality of channel walls composed substantially of thermally-conductive material and supported in spaced-apart relation, defining fluid channels and interstices therebetween. The fluid channels receive at least one primary fluid flow and the interstices receive at least one secondary fluid flow so as to effect heat exchange between the two flows. In use, the plurality of channel walls are deformable by pressure differential between the primary and secondary fluid flows. When at least some of the channel walls are in a deformed state, the plurality of channel walls are stabilized through press fit engagement of mutually opposed contact regions formed in adjacent pairs of the channel walls.

    摘要翻译： 热回收器包括多个通道壁，其基本上由导热材料组成并以间隔的关系支撑，限定了流体通道和间隙。 流体通道接收至少一个主要流体流，并且间隙接收至少一个次要流体流，以便实现两个流动之间的热交换。 在使用中，多个通道壁可通过主要和次要流体流之间的压力差而变形。 当至少一些通道壁处于变形状态时，多个通道壁通过在相邻的通道壁对中形成的相互相对的接触区域的压配合接合来稳定。

    SPRING-TENSIONED STATOR RESTRAINING STRAP
    2.
    发明申请
    SPRING-TENSIONED STATOR RESTRAINING STRAP 有权
    弹簧定位器限制带

    公开(公告)号：US20130058771A1

    公开(公告)日：2013-03-07

    申请号：US13223701

    申请日：2011-09-01

    申请人： David Harold MENHEERE ,  Richard IVAKITCH ,  Andreas ELEFTHERIOU

    发明人： David Harold MENHEERE ,  Richard IVAKITCH ,  Andreas ELEFTHERIOU

    IPC分类号： F01D1/02 ,  F01D5/30

    CPC分类号： F01D5/225 ,  F05D2260/30

    摘要： A vane assembly of a gas turbine engine includes a plurality of circumferentially spaced vanes extending radially between an outer case and an inner case. A spring-tensioned stator restraining strap is provided around the outer case and surrounding outer ends of the respective vanes. The outer ends of the vanes are received in corresponding openings defined in the outer case and project radially outwardly from the outer case. The spring-tensioned strap compresses the respective vanes radially and inwardly in position.

    摘要翻译： 燃气涡轮发动机的叶片组件包括在外壳和内壳之间径向延伸的多个周向隔开的叶片。 弹簧张紧的定子限制带设置在外壳周围并且围绕相应叶片的外端。 叶片的外端容纳在限定在外壳中的相应开口中，并从外壳径向向外突出。 弹簧张紧的带子将各个叶片径向和内向压缩在适当位置。

    CONNECTOR ASSEMBLY FOR VARIABLE INLET GUIDE VANES AND METHOD
    4.
    发明申请
    CONNECTOR ASSEMBLY FOR VARIABLE INLET GUIDE VANES AND METHOD 有权
    连接器组件可变入口导向件和方法

    公开(公告)号：US20130251518A1

    公开(公告)日：2013-09-26

    申请号：US13429839

    申请日：2012-03-26

    申请人： Andreas ELEFTHERIOU ,  David Harold Menheere ,  Andrew Marshall

    发明人： Andreas ELEFTHERIOU ,  David Harold Menheere ,  Andrew Marshall

    IPC分类号： F01D25/00 ,  B23P11/00 ,  F01D9/02

    CPC分类号： F01D17/162 ,  F04D9/042 ,  F04D29/563 ,  Y10T29/49245

    摘要： A connector assembly for variable inlet guide vanes in a compressor case of a gas turbine engine comprises an annular case insert having a plurality of circumferentially distributed open-ended receptacles. The annular case insert is sized so as to be received inside a compressor case, with the plurality of circumferentially distributed open-ended receptacles being in register with holes in the compressor case. Bushings have an outer diameter sized to be received in a respective one of the receptacles of the annular case insert, and an inner diameter adapted to receive a connector portion of a vane. Sets of the bushing and the connector portion of a vane in one of the receptacles forming a rotational joint. A method for installing vanes in a compressor case is also provided.

    摘要翻译： 用于燃气涡轮发动机的压缩机壳体中的可变入口导向叶片的连接器组件包括具有多个周向分布的开放式容器的环形壳体插入件。 环形壳体插入件的尺寸被设计成容纳在压缩机壳体内部，多个周向分布的开放式容器与压缩机壳体中的孔对准。 衬套的外径尺寸被设计成容纳在环形盒插入件的插座的相应一个中，并且适于容纳叶片的连接器部分的内径。 在一个容器中形成旋转接头的套管和叶片的连接器部分。 还提供了一种用于在压缩机壳体中安装叶片的方法。

    FABRICATED INTERMEDIATE CASE WITH ENGINE MOUNTS
    5.
    发明申请
    FABRICATED INTERMEDIATE CASE WITH ENGINE MOUNTS 有权
    制造中间件与发动机安装

    公开(公告)号：US20130058778A1

    公开(公告)日：2013-03-07

    申请号：US13224379

    申请日：2011-09-02

    申请人： Andreas ELEFTHERIOU ,  David MENHEERE ,  Quantai LIU

    发明人： Andreas ELEFTHERIOU ,  David MENHEERE ,  Quantai LIU

    IPC分类号： F02C7/20

    CPC分类号： F02C7/20 ,  F05D2230/232

    摘要： A fabricated engine case has a plurality of circumferentially spaced struts radially extending between an outer case and an inner case. A mount apparatus is affixed to the outer case of the engine case. The mount apparatus is a mount base radially spaced apart from a circumferential skin of the outer case and a load bearing member extending radially inwardly to connect the mount base to an outer end of one of the struts.

    摘要翻译： 制造的发动机壳体具有在外壳和内壳之间径向延伸的多个周向间隔的支柱。 发动机壳体的外壳附着有安装装置。 安装装置是与外壳的圆周表皮径向间隔开的安装基座和径向向内延伸的承载构件，以将安装基座连接到一个支柱的外端。