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    VIBRATION DAMPING SHROUD FOR A TURBOMACHINE VANE
    2.
    发明申请
    VIBRATION DAMPING SHROUD FOR A TURBOMACHINE VANE 审中-公开
    振动阻尼器用于涡轮增压器

    公开(公告)号：WO1996004468A1

    公开(公告)日：1996-02-15

    申请号：PCT/US1995009277

    申请日：1995-07-20

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： UNITED TECHNOLOGIES CORPORATION ,  VARSIK, David, A.

    IPC: F01D09/04

    CPC classification number: F01D9/042 ,  F01D25/04 ,  Y02T50/671 ,  Y02T50/673

    Abstract: A gas turbine engine (10) has a row of fan stator vanes (18) extending radially across a flow path (20) and joined to inner and outer cases (22 and 24). A vibration damping shroud (78) includes a radially extending chamber (84) for receiving one end of each stator vane in a primary vibration damping material (86). At least one pin receiving cavity (88), independent of the chamber, contains a secondary vibration damping material (92) which slidably engages a corresponding support pin (72) extending from the adjacent case (22) to anchor the vane to the case. The independence of the chamber and the cavity enables the use of different primary and secondary materials capable of satisfying conflicting performance requirements.

    Abstract translation: 燃气涡轮发动机（10）具有一排风扇定子叶片（18），径向延伸穿过流动路径（20）并且连接到内壳体和外壳体（22和24）。 减震罩（78）包括用于接收主振动阻尼材料（86）中的每个定子叶片的一端的径向延伸室（84）。 至少一个销接收腔（88），独立于腔室，包含二次减振材料（92），其可滑动地接合从相邻壳体（22）延伸的对应的支撑销（72），以将叶片锚固到壳体上。 室和腔的独立性使得能够使用能够满足相互矛盾的性能要求的不同的一次和二次材料。

    VIBRATION DAMPING SHROUD FOR A TURBOMACHINE VANE
    4.
    发明授权
    VIBRATION DAMPING SHROUD FOR A TURBOMACHINE VANE 失效
    防震甲板带TURBOMASCHINEN铲

    公开(公告)号：EP0839260B1

    公开(公告)日：1999-04-14

    申请号：EP95928110.6

    申请日：1995-07-20

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： VARSIK, David, A.

    IPC: F01D9/04 ,  F01D25/04

    CPC classification number: F01D9/042 ,  F01D25/04 ,  Y02T50/671 ,  Y02T50/673

    Abstract: A gas turbine engine (10) has a row of fan stator vanes (18) extending radially across a flow path (20) and joined to inner and outer cases (22 and 24). A vibration damping shroud (78) includes a radially extending chamber (84) for receiving one end of each stator vane in a primary vibration damping material (86). At least one pin receiving cavity (88), independent of the chamber, contains a secondary vibration damping material (92) which slidably engages a corresponding support pin (72) extending from the adjacent case (22) to anchor the vane to the case. The independence of the chamber and the cavity enables the use of different primary and secondary materials capable of satisfying conflicting performance requirements.

    VIBRATION DAMPING SHROUD FOR A TURBOMACHINE VANE
    5.
    发明公开
    VIBRATION DAMPING SHROUD FOR A TURBOMACHINE VANE 失效
    防震甲板带TURBOMASCHINEN铲

    公开(公告)号：EP0839260A1

    公开(公告)日：1998-05-06

    申请号：EP95928110.0

    申请日：1995-07-20

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： VARSIK, David, A.

    IPC: F01D9 ,  F01D25 ,  F04D29

    CPC classification number: F01D9/042 ,  F01D25/04 ,  Y02T50/671 ,  Y02T50/673

    Abstract: A gas turbine engine (10) has a row of fan stator vanes (18) extending radially across a flow path (20) and joined to inner and outer cases (22 and 24). A vibration damping shroud (78) includes a radially extending chamber (84) for receiving one end of each stator vane in a primary vibration damping material (86). At least one pin receiving cavity (88), independent of the chamber, contains a secondary vibration damping material (92) which slidably engages a corresponding support pin (72) extending from the adjacent case (22) to anchor the vane to the case. The independence of the chamber and the cavity enables the use of different primary and secondary materials capable of satisfying conflicting performance requirements.

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