BEARING DEVICE AND ROTARY MACHINE
    82.
    发明申请

    公开(公告)号:US20180073562A1

    公开(公告)日:2018-03-15

    申请号:US15561629

    申请日:2015-03-31

    发明人: Yuichi SASAKI

    IPC分类号: F16C33/08 F16C41/00 F16C33/10

    摘要: The present invention relates to a bearing device (61) provided with: a plurality of bearing pads (72) arranged between the outer peripheral surface of a turbine rotor (30) and the inner peripheral surface of a bearing housing (71) so as to be separated from each other in the circumferential direction of the rotor (30), the bearing housing (71) externally surrounding the rotor (30), the bearing pads (72) being supported on the inner peripheral surface of the bearing housing (71) and rotatably supporting the rotor (30); and a thermometer (75) provided to at least one of the plurality of bearing pads (72). The thermometer-equipped bearing pad (73) provided with the thermometer (75) has: a pad body (90) disposed facing the outer peripheral surface of the rotor (30); and a pair of pad shoulders (91) having different shapes and protruding from the pad body (90) to both sides of the bearing housing (71) in the direction of the center axis (O1) thereof. The bearing housing (71) has a pair of housing shoulders (78) having a shape corresponding to that of the pair of pad shoulders (91).

    GAS TURBINE STARTING DEVICE AND GAS TURBINE SYSTEM

    公开(公告)号:US20180038283A1

    公开(公告)日:2018-02-08

    申请号:US15551999

    申请日:2015-02-23

    摘要: Provided is a gas turbine starting device which has a sun gear, a planetary carrier, an internal gear, and a planetary gear, the sun gear, the planetary carrier and the internal gear serving as rotating bodies rotating about an axis; and a variable speed power source which has a rotor connected to one of the rotating bodies in the planetary gear mechanism. A rotating shaft of the gas turbine is connected to one of the rotating bodies other than the rotating body to which the variable speed power source is connected, and the rotating shaft of the compressor is connected to the remaining one of the rotating bodies other than the rotating bodies to which the rotor of the variable speed power source and the rotating shaft of the gas turbine are connected.

    CENTRIFUGAL COMPRESSOR AND GEARED CENTRIFUGAL COMPRESSOR

    公开(公告)号:US20180030992A1

    公开(公告)日:2018-02-01

    申请号:US15549636

    申请日:2015-08-10

    摘要: A centrifugal compressor includes a rotation shaft that extends along an axis; an impeller that includes a disk fixed to the rotation shaft and protruding outward in a radial direction, a plurality of blades provided in a surface facing one side in an axial direction of the disk to be separated from each other in a circumferential direction, and a cover covering the blades from the one side in the axial direction; and a casing that includes a facing inner peripheral surface facing an outer peripheral surface of the cover in the impeller and covers the impeller from an outside. The facing inner peripheral surface includes a cylindrical inner peripheral surface that extends along the axis and an enlarged inner peripheral surface that is connected to another side of the cylindrical inner peripheral surface in the axial direction and extends outward in the radial direction toward the other side.

    CENTRIFUGAL COMPRESSOR
    87.
    发明申请

    公开(公告)号:US20180023589A1

    公开(公告)日:2018-01-25

    申请号:US15547392

    申请日:2015-09-16

    IPC分类号: F04D29/44 F04D29/28 F04D29/42

    摘要: A centrifugal compressor includes an impeller that rotates about an axis; an inlet guide vane including a plurality of vanes disposed on an upstream side of the impeller and provided at intervals in a circumferential direction of the axis, the inlet guide vane being directed inward in the radial direction between adjacent vanes, and forming a guide flow path having an exit angle in the radial direction and guiding the fluid; and a suction flow path that introduces the fluid from a part in a circumferential direction into the inlet guide vane. The exit angle of the vane of the first region on the one side when viewed from the suction flow path in the inlet guide vane is displaced to the suction flow path side as compared to the exit angle of the vane of a second region on the opposite side of the one side.

    CENTRIFUGAL COMPRESSOR CASING AND CENTRIFUGAL COMPRESSOR

    公开(公告)号:US20180017073A1

    公开(公告)日:2018-01-18

    申请号:US15546221

    申请日:2015-01-27

    发明人: Hideki Yamada

    IPC分类号: F04D29/44 F04D17/12

    摘要: A centrifugal compressor casing, comprising a bundle which rotatably supports a rotating shaft, and an impeller fixed to the rotating shaft and that rotates with the rotating shaft about an axis of the rotating shaft, and in which an annular suction flow channel centered on the axis introduces fluid into the flow channel of the impeller, and an annular discharge flow channel centered on the axis that discharges the fluid from the flow channel of the impeller, are formed; a casing main body which covers the bundle from the outer circumferential side; and a volute piece which is provided on an inner surface of the casing main body in the discharge flow channel.