TURBINE DISCS AND METHODS OF FABRICATING THE SAME
    1.
    发明公开
    TURBINE DISCS AND METHODS OF FABRICATING THE SAME 审中-公开
    TURBINENSCHEIBEN UND VERFAHREN ZUR HERSTELLUNG DAVON

    公开(公告)号:EP3176367A1

    公开(公告)日:2017-06-07

    申请号:EP16200008

    申请日:2016-11-22

    申请人: GEN ELECTRIC

    IPC分类号: F01D5/08

    摘要: A turbine disc 202 having a radius and a circumference is provided. The turbine disc includes a central aperture 402 and a plurality of cooling channels 316, 414 circumferentially spaced about the central aperture such that the cooling channels are in flow communication with the central aperture. Each of the cooling channels has a radially inner end 424, a radially outer end 426, and a lengthwise axis 422 that is curved between the radially inner end and the radially outer end.

    摘要翻译: 提供具有半径和圆周的涡轮盘202。 涡轮盘包括中心孔402和围绕中心孔圆周地间隔开的多个冷却通道316,414,使得冷却通道与中心孔流动连通。 每个冷却通道具有径向内端424,径向外端426和在径向内端和径向外端之间弯曲的纵向轴线422。