Turbomachine Having an Axially Displaceable Rotor
    2.
    发明申请
    Turbomachine Having an Axially Displaceable Rotor 有权
    具有轴向位移转子的涡轮机

    公开(公告)号:US20080232949A1

    公开(公告)日:2008-09-25

    申请号:US10586795

    申请日:2005-01-19

    IPC分类号: F01D11/22

    摘要: The invention relates to a compressor, which is axially flowed through, for a gas turbine having an axially displaceable rotor. An annular flow channel, which narrows in an axial direction, is formed between a rotationally fixed outer delimiting surface and an inner delimiting surface on the rotor. A stationary ring comprised of guide profiles and at least one ring comprised of moving profiles attached to the rotor are placed inside said annular flow channel. The end of each moving or guide blade is located opposite an axial section of one of both delimiting surfaces while forming a radial gap. The aim of the invention is to provide a non-positive-displacement machine having an axially displaceable rotor whose velocity losses are at least not increased during an axial displacement of the rotor. To this end, the invention provides that the size of the radial gap between the end of each moving or guide blade and the opposite axial section of the delimiting surface is constant at least over the path of displacement of the rotor, and the radial gap extends parallel to the rotation axis of the rotor.

    摘要翻译: 本发明涉及一种用于具有可轴向移动的转子的燃气轮机的轴向流过的压缩机。 在旋转固定的外部限定表面和转子上的内部限定表面之间形成有在轴向方向上变窄的环形流动通道。 包括导向轮廓的固定环和由连接到转子的移动轮廓组成的至少一个环被放置在所述环形流动通道内。 每个移动或引导刀片的端部与形成径向间隙的两个限定表面之一的轴向部分相对。 本发明的目的是提供一种具有轴向移位的转子的非正排量机械,其在转子的轴向位移期间速度损失至少不增加。 为此,本发明规定,每个移动或引导叶片的端部与限定表面的相对的轴向部分之间的径向间隙的尺寸至少在转子的位移路径上是恒定的,并且径向间隙延伸 平行于转子的旋转轴线。