Coolable rotor blade for an industrial gas turbine engine
    151.
    发明授权
    Coolable rotor blade for an industrial gas turbine engine 有权
    用于工业燃气涡轮发动机的可冷却转子叶片

    公开(公告)号:US06672836B2

    公开(公告)日:2004-01-06

    申请号:US10014952

    申请日:2001-12-11

    申请人: Brian D. Merry

    发明人: Brian D. Merry

    IPC分类号: F01D518

    摘要: A coolable rotor blade having an airfoil having two serpentine passages is disclosed. Various construction details are developed for providing cooling to the leading edge region and the trailing edge region of the airfoil. In one detailed embodiment, the airfoil trip strips in the passages having constant height and constant pitch over each leg in most legs of the passages except for the legs closest to the edge regions of the airfoil.

    摘要翻译: 公开了具有具有两个蛇形通道的翼型件的可冷却转子叶片。 开发了各种结构细节,用于向机翼的前缘区域和后缘区域提供冷却。 在一个详细的实施例中,通道中的翼型跳闸带在除了最接近翼型边缘区域的腿部之外的通道的大多数腿部的每个腿部上具有恒定的高度和恒定的间距。