METHODS AND SYSTEM FOR FLUIDIC SEALING IN GAS TURBINE ENGINES
    1.
    发明申请
    METHODS AND SYSTEM FOR FLUIDIC SEALING IN GAS TURBINE ENGINES 审中-公开
    气体涡轮发动机流体密封方法与系统

    公开(公告)号:US20160123169A1

    公开(公告)日:2016-05-05

    申请号:US14532884

    申请日:2014-11-04

    CPC classification number: F01D25/12 F01D11/04 F05D2240/127 Y02T50/675

    Abstract: A sealing system for a rotatable element defining an axis of rotation includes a rotor blade including a shank and an angel wing extending axially from the shank. The sealing system also includes a stator vane positioned axially adjacent the rotor blade. The stator vane includes a platform extending in an axial direction over the angel wing such that a clearance gap is defined therebetween. The sealing system also includes a sealing mechanism including a portion of the platform and a portion of the angel wing. The sealing mechanism includes a plurality of circumferentially-spaced grooves defined in the stator platform.

    Abstract translation: 用于限定旋转轴线的可旋转元件的密封系统包括转子叶片,其包括柄和从柄部轴向延伸的天使翼。 该密封系统还包括定位于叶片轴向相邻的定子叶片。 定子叶片包括在轴向方向上延伸穿过天使翼的平台,从而在它们之间限定间隙。 密封系统还包括密封机构,其包括平台的一部分和天使翼的一部分。 密封机构包括限定在定子平台中的多个周向间隔开的凹槽。

    METHODS AND SYSTEM FOR FLUIDIC SEALING IN GAS TURBINE ENGINES
    2.
    发明申请
    METHODS AND SYSTEM FOR FLUIDIC SEALING IN GAS TURBINE ENGINES 有权
    气体涡轮发动机流体密封方法与系统

    公开(公告)号:US20160123168A1

    公开(公告)日:2016-05-05

    申请号:US14532870

    申请日:2014-11-04

    CPC classification number: F01D11/001 F05D2250/294

    Abstract: A sealing system for a rotatable element defining an axis of rotation includes a rotor blade including a shank and an angel wing extending axially from the shank. The sealing system also includes a stator vane positioned axially adjacent the rotor blade. The stator vane includes a platform extending in an axial direction over the angel wing such that a clearance gap is defined therebetween. The sealing system also includes a sealing mechanism including a portion of the platform and a portion of the angel wing. The sealing mechanism includes at least one obliquely oriented surface such that the clearance gap defines a converging nozzle.

    Abstract translation: 用于限定旋转轴线的可旋转元件的密封系统包括转子叶片,其包括柄和从柄部轴向延伸的天使翼。 该密封系统还包括定位于叶片轴向相邻的定子叶片。 定子叶片包括在轴向方向上延伸穿过天使翼的平台,从而在它们之间限定间隙。 密封系统还包括密封机构,其包括平台的一部分和天使翼的一部分。 密封机构包括至少一个倾斜取向的表面,使得间隙间隙限定会聚喷嘴。

    Methods and system for fluidic sealing in gas turbine engines

    公开(公告)号:US09771817B2

    公开(公告)日:2017-09-26

    申请号:US14532870

    申请日:2014-11-04

    CPC classification number: F01D11/001 F05D2250/294

    Abstract: A sealing system for a rotatable element defining an axis of rotation includes a rotor blade including a shank and an angel wing extending axially from the shank. The sealing system also includes a stator vane positioned axially adjacent the rotor blade. The stator vane includes a platform extending in an axial direction over the angel wing such that a clearance gap is defined therebetween. The sealing system also includes a sealing mechanism including a portion of the platform and a portion of the angel wing. The sealing mechanism includes at least one obliquely oriented surface such that the clearance gap defines a converging nozzle.

Patent Agency Ranking