Turbine blade
    2.
    发明授权

    公开(公告)号:US11867085B2

    公开(公告)日:2024-01-09

    申请号:US17778974

    申请日:2021-03-23

    IPC分类号: F01D5/18

    CPC分类号: F01D5/187 F05D2220/32

    摘要: A turbine blade is provided with an airfoil portion having a leading edge, a trailing edge, and a pressure surface and a suction surface which extend between the leading edge and the trailing edge, the airfoil portion internally forming a cooling passage. The cooling passage includes: a first cooling passage located closer to the pressure surface than the suction surface; and a second cooling passage located closer to the suction surface than the pressure surface. The first cooling passage and the second cooling passage are separated by a partition member disposed in the airfoil portion. At least one communication space connecting the first cooling passage and the second cooling passage is formed in the partition member.