BLADED ROTOR FOR A GAS TURBINE ENGINE
    1.
    发明申请
    BLADED ROTOR FOR A GAS TURBINE ENGINE 审中-公开
    用于气体涡轮发动机的叶片转子

    公开(公告)号:US20160333708A1

    公开(公告)日:2016-11-17

    申请号:US15138650

    申请日:2016-04-26

    CPC classification number: F01D5/3015 F05D2250/71

    Abstract: A bladed rotor includes rotor disc having a peripheral region, and a plurality of rotor blades attached to and extending radially outwardly from peripheral region. Each rotor blade has a root portion which is located in a correspondingly shaped axially-extending slot provided in the peripheral region of rotor disc, and the root portion of each blade is axially retained in its respective slot by a plate located axially adjacent the root portion and rotor disc, and which extends circumferentially across respective slot. Retention plate is held in position by seal member having a first surface which engages radially-inwardly directed surface of rotor disc, and second surface which is located radially-outwardly of first surface and engages the retention plate. Seal member has a curved profile in radial cross-section so as to define a concavity located radially between first and second engaging surfaces and which is directed axially towards the rotor disc.

    Abstract translation: 叶片转子包括具有周边区域的转子盘和附接到外围区域并从周边区域径向向外延伸的多个转子叶片。 每个转子叶片具有根部,其位于设置在转子盘的周边区域中的相应形状的轴向延伸槽中,并且每个叶片的根部通过位于轴向邻近根部的板轴向保持在其相应的狭槽中 和转子盘,并且其周向延伸穿过相应的槽。 保持板通过具有接合转子盘的径向向内的表面的第一表面的密封构件和位于第一表面的径向向外并且与保持板接合的第二表面保持就位。 密封构件具有径向横截面的弯曲轮廓,以便限定径向地位于第一和第二接合表面之间并且朝向转子盘轴向定向的凹面。

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