Ring segment of gas turbine
    1.
    发明授权
    Ring segment of gas turbine 有权
    燃气轮机的环段

    公开(公告)号:US07033138B2

    公开(公告)日:2006-04-25

    申请号:US10235825

    申请日:2002-09-06

    IPC分类号: F01D25/08

    摘要: An object of the present invention is to provide a ring segment of a gas turbine in which the temperature is maintained low, damage due to high temperature oxidation is prevented, and high temperature deformation is prevented. In order to achieve the object, the present invention provides a ring segment of a gas turbine which comprises a blade ring, a main shaft and moving blades comprising a plurality of individual units which define an annular form by being arranged around the peripheral direction of the main shaft, and disposed so that its inner peripheral surface is maintained at a constant distance from the tips of the moving blades, wherein grooves which extend along the axial direction of the main shaft of the turbine are formed upon of the individual units so as mutually to confront one another; a seal plate which is inserted into each mutually confronting pair of the grooves so as to connect together the adjacent pair of individual units; and contact surfaces which are formed at positions more radially inward than the seal plates, which extend in the axial direction and the peripheral direction and which mutually contact one another.

    摘要翻译: 本发明的目的是提供一种燃气轮机的环段,其中温度保持较低,防止了由于高温氧化引起的损坏,并且防止了高温变形。 为了实现该目的,本发明提供了一种燃气轮机的环形段,其包括叶片环,主轴和包括多个独立单元的活动叶片,所述多个单独的单元通过围绕 主轴,并且配置成使其内周面与动叶片的前端保持恒定的距离,其中沿涡轮主轴的轴向延伸的槽形成在各个单元上,以便相互 相互对抗 密封板,其插入每个相互面对的一对槽中,以将相邻的一对单独的单元连接在一起; 以及形成在比轴向和周向延伸并彼此相互接触的密封板更径向向内的位置处的接触表面。