Shroud honeycomb cutter
    21.
    发明授权

    公开(公告)号:US07273353B2

    公开(公告)日:2007-09-25

    申请号:US11503779

    申请日:2006-08-14

    IPC分类号: F01D11/12

    摘要: A turbine blade for use in a gas turbine engine is provided. The turbine blade includes an airfoil portion having a tip end, a shroud attached to the tip end, which shroud has an outer surface, and a knife edge attached to an outer surface of the shroud. The knife edge has a pair of cutter blades disposed substantially over an axis of the airfoil portion.