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    ROTOR BLADE WITH PLATFORM SUPPORT AND DAMPER POSITIONING MEANS
    3.
    发明申请
    ROTOR BLADE WITH PLATFORM SUPPORT AND DAMPER POSITIONING MEANS 审中-公开
    具有平台支持和阻尼器定位手段的转子叶片

    公开(公告)号：WO1994012774A1

    公开(公告)日：1994-06-09

    申请号：PCT/US1993011127

    申请日：1993-11-12

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： UNITED TECHNOLOGIES CORPORATION ,  CHLUS, Wieslaw, A. ,  HOUSTON, David, P.

    IPC: F01D05/26

    CPC classification number: F01D5/22 ,  Y10S416/50

    Abstract: A rotor blade (44) having axially spaced gussets (72, 78) disposed between a root portion (66) and a platform (64) is disclosed. Various construction details are developed which provide a gusset providing both platform support and damper positioning means. In one particular embodiment, a rotor blade assembly (38) includes a plurality of circumferentially spaced rotor blades (44) having dampers (88) disposed between adjacent blades (44), wherein each blade (44) includes an axially spaced pair of gussets (78, 82) extending laterally from the rotor blade (44). The gussets (78, 82) extend from a root portion (66) of the rotor blade (44) to a platform (64) and provide radial support of the platform (64) during rotation of the rotor assembly (38). The gussets (78, 82) include a curved lateral edge which, during rotation of the rotor assembly (38), urges the damper (88) away from the root portion (66) of the blade (44).

    Abstract translation: 公开了一种设置在根部（66）和平台（64）之间的具有轴向间隔的角撑板（72,78）的转子叶片（44）。 开发了各种构造细节，其提供提供平台支撑和阻尼器定位装置的角撑板。 在一个特定实施例中，转子叶片组件（38）包括多个周向间隔开的转子叶片（44），其具有设置在相邻叶片（44）之间的阻尼器（88），其中每个叶片（44）包括轴向间隔开的一对角撑板 78）从转子叶片（44）横向延伸。 在转子组件（38）旋转期间，角撑板（78,82）从转子叶片（44）的根部（66）延伸到平台（64）并且提供平台（64）的径向支撑。 角撑板（78,82）包括弯曲的侧边缘，其在转子组件（38）的旋转期间促使阻尼器（88）远离叶片（44）的根部（66）。

    ROTOR BLADE WITH PLATFORM SUPPORT AND DAMPER POSITIONING MEANS
    5.
    发明公开
    ROTOR BLADE WITH PLATFORM SUPPORT AND DAMPER POSITIONING MEANS 失效
    一种用于涡轮动叶片及用于定位的装置的阻尼元件

    公开(公告)号：EP0774049A1

    公开(公告)日：1997-05-21

    申请号：EP94901542.0

    申请日：1993-11-12

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： CHLUS, Wieslaw, A. ,  HOUSTON, David, P.

    IPC: F01D5

    CPC classification number: F01D5/22 ,  Y10S416/50

    Abstract: A rotor blade (44) having axially spaced gussets (72, 78) disposed between a root portion (66) and a platform (64) is disclosed. Various construction details are developed which provide a gusset providing both platform support and damper positioning means. In one particular embodiment, a rotor blade assembly (38) includes a plurality of circumferentially spaced rotor blades (44) having dampers (88) disposed between adjacent blades (44), wherein each blade (44) includes an axially spaced pair of gussets (78, 82) extending laterally from the rotor blade (44). The gussets (78, 82) extend from a root portion (66) of the rotor blade (44) to a platform (64) and provide radial support of the platform (64) during rotation of the rotor assembly (38). The gussets (78, 82) include a curved lateral edge which, during rotation of the rotor assembly (38), urges the damper (88) away from the root portion (66) of the blade (44).

    AIRFOIL INCLUDING LOOSE DAMPER
    7.
    发明公开
    AIRFOIL INCLUDING LOOSE DAMPER 有权
    包含松散阻尼器的机翼

    公开(公告)号：EP2841705A1

    公开(公告)日：2015-03-04

    申请号：EP13782220.1

    申请日：2013-04-20

    Applicant: United Technologies Corporation

    Inventor： FISK, Benjamin, T. ,  PROPHETER-HINCKLEY, Tracy, A. ,  HOUSTON, David, P. ,  TRACY, Anita, L.

    IPC: F01D5/12 ,  F01D5/18 ,  F02C7/00 ,  F02K3/00

    Abstract: An airfoil includes an airfoil body that has a leading edge and a trailing edge and a first sidewall and a second sidewall that is spaced apart from the first sidewall. The first sidewall and the second sidewall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. A damper member is enclosed in the cavity and is loose within the cavity.

    Abstract translation: 翼型包括具有前缘和后缘以及第一侧壁和与第一侧壁间隔开的第二侧壁的翼型体。 第一侧壁和第二侧壁连接前缘和后缘并且至少部分地限定翼型体中的空腔。 阻尼器构件被封闭在空腔中并且在空腔内松动。

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