Turbo compressor
    1.
    发明授权

    公开(公告)号:US11480194B2

    公开(公告)日:2022-10-25

    申请号:US17055289

    申请日:2019-04-24

    Abstract: A turbo compressor comprises a rotary shaft including a rotor; a first impeller coupled to one side of the rotary shaft, a thrust bearing runner coupled between the first impeller and the rotary shaft, an impeller sleeve compressed and coupled between the first impeller and the thrust bearing runner, a second impeller coupled to the other side of the rotary shaft, and a tie rod passing through the first impeller and a thrust bearing and fastened to the rotary shaft.

    Thrust bearing for turbo compressor

    公开(公告)号:US11193529B2

    公开(公告)日:2021-12-07

    申请号:US16812806

    申请日:2020-03-09

    Abstract: Disclosed herein is a thrust bearing for a turbo compressor, the thrust bearing has a structure that is modified in response to a portion where a deformation amount of a thrust runner is relatively large on the basis of magnitude of a force applied at the time of rotation of a shaft of a turbo compressor, to maintain a thickness of an oil film constantly and to increase a load supporting force of the thrust bearing, thereby ensuring improved durability of the thrust bearing.

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