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    • 3. 发明申请
    • TURBINE ROTOR BLADE
    • 涡轮转子叶片
    • US20110217175A1
    • 2011-09-08
    • US12673494
    • 2009-01-08
    • Naoto TochitaniShohei DannoShoki Yamashita
    • Naoto TochitaniShohei DannoShoki Yamashita
    • F01D5/22B21K25/00
    • F01D5/3007F01D5/225Y10T29/49321
    • It is possible to easily and rapidly slot a blade root of a final (last) turbine rotor blade into a blade groove on a turbine disc even when the plan-view shape of a shroud of the turbine rotor blade is complex. A turbine rotor blade that is provided with a blade root that is slotted into a blade groove formed on a circumferential portion of the turbine disc to hold the whole blade, a blade portion that is exposed to high-temperature gas, a platform that supports this blade portion, a shank that connects the blade root and the platform, and a shroud that extends along the circumferential direction from the end of the blade portion has a cut-out portion cut out to a predetermined depth, either at the leading-edge or the trailing-edge of the blade root, along the lengthwise direction thereof from the end of the blade root to an intermediate part of the shank.
    • 即使当涡轮转子叶片的护罩的平面视图形状复杂时,也可以将最终(最后)涡轮转子叶片的叶片根部容易且快速地插入到涡轮盘上的叶片槽中。 一种涡轮转子叶片,其具有叶片根部,该叶片根部形成在涡轮盘的周向部分上形成的叶片槽中以保持整个叶片,暴露于高温气体的叶片部分,支撑该叶片根部的平台 叶片部分,连接叶片根部和平台的柄部以及从叶片部分的端部沿圆周方向延伸的护罩具有切除到预定深度的切口部分,或者在前缘或 叶片根部的后缘沿着其从叶根的端部到柄的中间部分的长度方向。