Harness for performing aerobic exercises on a therapeutic ball
    5.
    发明授权
    Harness for performing aerobic exercises on a therapeutic ball 失效
    用于在治疗球上进行有氧运动的线束

    公开(公告)号:US06475125B1

    公开(公告)日:2002-11-05

    申请号:US09819528

    申请日:2001-03-28

    申请人: Steven D. Roberts

    发明人: Steven D. Roberts

    IPC分类号: A63B2102

    摘要: A harness for an ABS therapeutic ball allows a user to perform aerobic exercises while seated on the ABS therapeutic ball. The harness includes a stabilizer portion having circumferential straps extending therefrom. A handle is positioned between the circumferential straps proximate a joining area thereof. An adjustment strap having a self fastening system also extends from the stabilizer portion of the harness and interacts with the joining area of the circumferential straps to provide a single, overall size adjustment of the harness to accommodate various sizes of ABS therapeutic balls. Once installed onto an ABS therapeutic ball, the user may perform various aerobic exercises while seated on the ABS therapeutic ball and firmly grasping the handle of the harness. The harness thus provides a secure, no-slip, and stable platform for aerobically exercising on the ABS therapeutic ball.

    摘要翻译: 用于ABS治疗球的线束允许用户在坐在ABS治疗球上时进行有氧运动。 线束包括具有从其延伸的周向带的稳定器部分。 手柄位于靠近其接合区域的圆周带之间。 具有自固定系统的调节带也从线束的稳定器部分延伸并与周向带的接合区域相互作用,以提供线束的单个整体尺寸调节以适应各种尺寸的ABS治疗球。 一旦安装到ABS治疗球上,用户可以在坐在ABS治疗球上并且牢固地抓住线束的把手时执行各种有氧运动。 因此,该线束提供了用于在ABS治疗球上进行有氧运动的安全,防滑和稳定的平台。

    Flexible seal for gas turbine engine system
    6.
    发明授权
    Flexible seal for gas turbine engine system 有权
    燃气轮机发动机系统的柔性密封

    公开(公告)号:US09228533B2

    公开(公告)日:2016-01-05

    申请号:US11947814

    申请日:2007-11-30

    IPC分类号: F02C7/28 F02K1/80 F01D11/00

    摘要: A gas turbine engine system includes an airframe support, a gas turbine engine mounted to the airframe support, a nozzle exhaust mounted to the airframe support, and a flexible annular seal having a first end that is attached to the gas turbine engine and a second end that is attached to an exhaust nozzle. The flexible annular seal may include a flexible annular wall that permits relative deflection between the gas turbine engine and the exhaust nozzle to facilitate the reduction of undesirable load transfer.

    摘要翻译: 燃气涡轮发动机系统包括机体支撑件,安装到机身支撑件的燃气涡轮发动机,安装到机体支撑件上的喷嘴排气口以及具有连接到燃气涡轮发动机的第一端的柔性环形密封件,以及附接到燃气涡轮发动机的第一端 其附接到排气喷嘴。 柔性环形密封件可以包括允许燃气涡轮发动机和排气喷嘴之间的相对偏转的柔性环形壁,以便于减少不期望的负载传递。

    FLEXIBLE SEAL SYSTEM FOR A GAS TURBINE ENGINE
    7.
    发明申请
    FLEXIBLE SEAL SYSTEM FOR A GAS TURBINE ENGINE 有权
    用于气体涡轮发动机的柔性密封系统

    公开(公告)号:US20130121813A1

    公开(公告)日:2013-05-16

    申请号:US13297458

    申请日:2011-11-16

    IPC分类号: F03B3/00 F16J15/02

    摘要: A flexible seal system for a gas turbine engine includes an annular mounting bracket, an annular support bracket, an annular flexible seal and a plurality of mounting spacers. The flexible seal extends axially between a first mounting segment and a second mounting segment. The first mounting segment is connected axially between the mounting bracket and the support bracket, and includes a plurality of mounting apertures that extend axially through the first mounting segment. Each of the mounting spacers is arranged within a respective one of the mounting apertures, and extends axially between the mounting bracket and the support bracket.

    摘要翻译: 用于燃气涡轮发动机的柔性密封系统包括环形安装支架,环形支撑支架,环形柔性密封件和多个安装间隔件。 柔性密封件在第一安装段和第二安装段之间轴向延伸。 第一安装段轴向地连接在安装支架和支撑托架之间,并且包括多个安装孔,其轴向延伸穿过第一安装段。 每个安装间隔件布置在相应的一个安装孔内,并且在安装支架和支撑托架之间轴向延伸。

    FLEXIBLE SEAL FOR GAS TURBINE ENGINE SYSTEM
    8.
    发明申请
    FLEXIBLE SEAL FOR GAS TURBINE ENGINE SYSTEM 有权
    气动涡轮发动机系统的柔性密封

    公开(公告)号:US20090140497A1

    公开(公告)日:2009-06-04

    申请号:US11947814

    申请日:2007-11-30

    IPC分类号: F02C7/28

    摘要: A gas turbine engine system includes an airframe support, a gas turbine engine mounted to the airframe support, a nozzle exhaust mounted to the airframe support, and a flexible annular seal having a first end that is attached to the gas turbine engine and a second end that is attached to an exhaust nozzle. The flexible annular seal may include a flexible annular wall that permits relative deflection between the gas turbine engine and the exhaust nozzle to facilitate the reduction of undesirable load transfer.

    摘要翻译: 燃气涡轮发动机系统包括机体支撑件,安装到机身支撑件的燃气涡轮发动机,安装到机体支撑件上的喷嘴排气口以及具有连接到燃气涡轮发动机的第一端的柔性环形密封件,以及附接到燃气涡轮发动机的第一端 其附接到排气喷嘴。 柔性环形密封件可以包括允许燃气涡轮发动机和排气喷嘴之间的相对偏转的柔性环形壁,以便于减少不期望的负载传递。

    Flexible seal system for a gas turbine engine
    10.
    发明授权
    Flexible seal system for a gas turbine engine 有权
    用于燃气轮机的柔性密封系统

    公开(公告)号:US09284889B2

    公开(公告)日:2016-03-15

    申请号:US13297458

    申请日:2011-11-16

    IPC分类号: F02C7/28 F02K1/80

    摘要: A flexible seal system for a gas turbine engine includes an annular mounting bracket, an annular support bracket, an annular flexible seal and a plurality of mounting spacers. The flexible seal extends axially between a first mounting segment and a second mounting segment. The first mounting segment is connected axially between the mounting bracket and the support bracket, and includes a plurality of mounting apertures that extend axially through the first mounting segment. Each of the mounting spacers is arranged within a respective one of the mounting apertures, and extends axially between the mounting bracket and the support bracket.

    摘要翻译: 用于燃气涡轮发动机的柔性密封系统包括环形安装支架,环形支撑支架,环形柔性密封件和多个安装间隔件。 柔性密封件在第一安装段和第二安装段之间轴向延伸。 第一安装段轴向地连接在安装支架和支撑托架之间,并且包括多个安装孔,其轴向延伸穿过第一安装段。 每个安装间隔件布置在相应的一个安装孔内,并且在安装支架和支撑托架之间轴向延伸。