Tie-rod nut including a nut flange with a plurality of mounting apertures
    21.
    发明授权
    Tie-rod nut including a nut flange with a plurality of mounting apertures 有权
    连杆螺母包括具有多个安装孔的螺母法兰

    公开(公告)号:US08992173B2

    公开(公告)日:2015-03-31

    申请号:US13289718

    申请日:2011-11-04

    摘要: A tie-rod nut includes a nut base that extends between a first nut end and a second nut end, and a nut flange that extends radially outwards from the nut base at the first nut end. The nut base includes a nut bore with a threaded bore region that extends axially from the second nut end towards the first nut end. The nut flange includes a plurality of mounting apertures that are arranged circumferentially around the nut base. The nut flange may be connected to a substrate by a fastener that extends through a first one of the plurality of mounting apertures.

    摘要翻译: 连杆螺母包括在第一螺母端和第二螺母端之间延伸的螺母基座,以及在第一螺母端处从螺母底座径向向外延伸的螺母凸缘。 螺母底座包括螺母孔,螺母孔具有从第二螺母端向第一螺母端轴向延伸的螺纹孔区域。 螺母凸缘包括围绕螺母底座周向布置的多个安装孔。 螺母法兰可以通过延伸穿过多个安装孔中的第一个的紧固件连接到基板。

    IMPINGEMENT COOLED NOZZLE LINER
    23.
    发明申请
    IMPINGEMENT COOLED NOZZLE LINER 有权
    IMPINGEMENT冷却喷嘴线

    公开(公告)号:US20130001319A1

    公开(公告)日:2013-01-03

    申请号:US13173903

    申请日:2011-06-30

    IPC分类号: B64D33/04

    摘要: A nozzle liner for a rotatable nozzle includes a seal land and a rotatable seal for moving with the nozzle. The seal has a first diffusion hole for distributing cooling air if the rotatable seal is in a first position and a second diffusion hole for distributing cooling air if the rotatable seal is in a first position and if in a second position.

    摘要翻译: 用于可旋转喷嘴的喷嘴衬套包括密封台面和用于与喷嘴一起移动的可旋转密封件。 如果可旋转密封件处于第一位置,密封件具有用于分配冷却空气的第一扩散孔和用于在可旋转密封件处于第一位置并且如果处于第二位置时分配冷却空气的第二扩散孔。

    Kinematic fixturing of optic components
    25.
    发明授权
    Kinematic fixturing of optic components 失效
    光学部件的运动夹具

    公开(公告)号:US5172277A

    公开(公告)日:1992-12-15

    申请号:US674829

    申请日:1991-03-20

    IPC分类号: G02B7/18

    CPC分类号: G02B7/1815

    摘要: An optical mirror is kinematically mounted at its sides on one fixed point and two movable points which points are supported by a frame spaced from the mirror. One of the movable points is a ball on a cantilevered arm which rests in a cone or groove in the mirror, the other movable point is a mechanical flexure prelaod mounting or a pneumatic preload mounting, which mountings serve to apply constant preload to such mirror. The mirror is made of ceramic material, of low thermal expansion or contraction and has water cooling passages therein. The frame is made of metal of higher thermal expansion or contraction. However such mirors, when reflecting a high intensity laser beam can thermally expand relative to the frame and must do so with minimal deformation from the desired optical contour thereof which result is accomplished by the resilient and constant preload mountings of the present invention. The preload mounting of the invention also serves to compensate for temperature differentials between the cooled ceramic mirror and its uncooled metal frame.

    摘要翻译: 一个光学镜在其侧面运动地安装在一个固定点和两个可移动点上,这些点由与镜子隔开的框架支撑。 可移动点之一是在反射镜中的锥体或凹槽中的悬臂上的球,另一个可移动点是机械挠曲预安装或气动预载安装,这些安装件用于对这种反射镜施加恒定的预载荷。 镜子由陶瓷材料制成,热膨胀或收缩低,并在其中具有水冷却通道。 框架由更高的热膨胀或收缩的金属制成。 然而,当反射高强度激光束的这种镜像可以相对于框架热膨胀,并且必须通过由本发明的弹性和恒定的预载安装件实现的期望的光学轮廓的最小变形来做到这一点。 本发明的预载安装还用于补偿冷却的陶瓷镜与其未被制造的金属框架之间的温差。

    Dual-intent locator pin and removable plug for gas turbines
    26.
    发明授权
    Dual-intent locator pin and removable plug for gas turbines 有权
    双目标定位销和燃气轮机的可拆卸插头

    公开(公告)号:US09494052B2

    公开(公告)日:2016-11-15

    申请号:US13431041

    申请日:2012-03-27

    IPC分类号: F01D25/24 F01D21/00

    摘要: A borescope plug configuration is disclosed. The borescope plug configuration comprises an inspection path defined through a bore in a first engine structure, a second engine structure, and an opening into the gas path of an engine. The borescope plug configuration further comprises a removable plug for sealing the inspection path. The removable plug is adapted to couple the first engine structure to the second engine structure.

    摘要翻译: 公开了管道镜插头配置。 管孔塞塞构造包括通过第一发动机结构中的孔,第二发动机结构和通向发动机的气体通道的开口限定的检查路径。 管孔塞插头配置还包括用于密封检查路径的可移除插头。 可拆卸插头适于将第一发动机结构联接到第二发动机结构。

    Cooling apparatus for a mid-turbine frame
    27.
    发明授权
    Cooling apparatus for a mid-turbine frame 有权
    用于中涡轮机架的冷却装置

    公开(公告)号:US08863531B2

    公开(公告)日:2014-10-21

    申请号:US13539827

    申请日:2012-07-02

    摘要: A cooling apparatus bifurcates and regulates cooling airflow provided to a mid-turbine frame. The cooling apparatus includes a flow metering tube and a metering plate. The flow metering tube includes a top portion and a tube portion, wherein the top portion includes a first central aperture that directs a first cooling airflow into the tube portion and a first plurality of apertures located circumferentially around the central aperture that directs a second cooling airflow to a portion outside the tube portion. The metering plate is located on the top portion of the flow metering tube, wherein the metering plate includes a second central aperture aligned with the central aperture of the flow metering tube and a second plurality of apertures located circumferentially around the central aperture, wherein a size of the second central aperture meters the first cooling airflow and a size and number of the second plurality of apertures meters the second cooling airflow.

    摘要翻译: 冷却装置使提供给中间涡轮机框架的冷却气流分叉并调节。 冷却装置包括流量计量管和计量盘。 流量计量管包括顶部部分和管部分,其中顶部包括将第一冷却气流引导到管部分中的第一中心孔和围绕中心孔周向定位的第一多个孔,其引导第二冷却气流 到管部分外部的部分。 计量板位于流量计量管的顶部,其中计量板包括与流量计量管的中心孔对准的第二中心孔和围绕中心孔周向定位的第二多个孔,其中尺寸 第二中心孔的第一冷却气流计量第二冷却气流,第二多个孔的尺寸和数量对第二冷却气流进行测量。

    Airfoil attachment arrangement
    28.
    发明授权
    Airfoil attachment arrangement 有权
    翼型附件装置

    公开(公告)号:US08668448B2

    公开(公告)日:2014-03-11

    申请号:US12915575

    申请日:2010-10-29

    IPC分类号: F01D5/32

    CPC分类号: F01D9/042

    摘要: An example airfoil retention arrangement includes a retention assembly having a first retention segment and a second retention segment. Each of the retention segments is separately moveable to an installed position relative to an airfoil assembly and a support structure. The retention segments each have a portion position between a lip of the airfoil assembly and a collar of the support structure when the retention segments are in the installed position. The retention assembly is configured to limit radial movement of an airfoil relative to the support structure when in the installed position.

    摘要翻译: 示例性翼型保持装置包括具有第一保持段和第二保留段的保持组件。 每个保持段分别可移动到相对于翼型组件和支撑结构的安装位置。 当保持段处于安装位置时,保持段各自具有在翼型组件的唇缘和支撑结构的套环之间的部分位置。 保持组件构造成在处于安装位置时限制翼型件相对于支撑结构的径向移动。

    TIE-ROD NUT INCLUDING A NUT FLANGE WITH A PLURALITY OF MOUNTING APERTURES
    29.
    发明申请
    TIE-ROD NUT INCLUDING A NUT FLANGE WITH A PLURALITY OF MOUNTING APERTURES 有权
    TIE-ROD NUT包括具有多重安装孔的NUT法兰

    公开(公告)号:US20130115079A1

    公开(公告)日:2013-05-09

    申请号:US13289718

    申请日:2011-11-04

    IPC分类号: F04D29/52 F16B37/00

    摘要: A tie-rod nut includes a nut base that extends between a first nut end and a second nut end, and a nut flange that extends radially outwards from the nut base at the first nut end. The nut base includes a nut bore with a threaded bore region that extends axially from the second nut end towards the first nut end. The nut flange includes a plurality of mounting apertures that are arranged circumferentially around the nut base. The nut flange may be connected to a substrate by a fastener that extends through a first one of the plurality of mounting apertures.

    摘要翻译: 连杆螺母包括在第一螺母端和第二螺母端之间延伸的螺母基座,以及在第一螺母端处从螺母底座径向向外延伸的螺母凸缘。 螺母底座包括螺母孔,螺母孔具有从第二螺母端向第一螺母端轴向延伸的螺纹孔区域。 螺母凸缘包括围绕螺母底座周向布置的多个安装孔。 螺母法兰可以通过延伸穿过多个安装孔中的第一个的紧固件连接到基板。

    Cooled duct for gas turbine engine
    30.
    发明授权
    Cooled duct for gas turbine engine 有权
    燃气轮机发动机冷却管道

    公开(公告)号:US07631481B2

    公开(公告)日:2009-12-15

    申请号:US11000829

    申请日:2004-12-01

    IPC分类号: F02C7/08

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

    摘要翻译: 提供了一种用于燃气涡轮发动机的冷却排气管。 冷却的排气管道包括轴向中心线,圆周,环形空间和多个可径向扩张的带。 环形空间设置在第一壁和第二壁之间,并且沿轴向中心线延伸。 第一壁径向设置在第二壁的内侧。 多个可径向扩张的带中的每一个在圆环内周向延伸。 带彼此轴向间隔开。 每个带包括附接到第一壁的第一部分,附接到第二壁的第二部分和连接到第一和第二部分的中间部分。 带形成周向延伸的隔室,其阻止环形空间内的冷却空气的轴向移动。