TURBOMACHINERY AND METHOD FOR DESIGNING TURBOMACHINERY

    公开(公告)号:US20230250753A1

    公开(公告)日:2023-08-10

    申请号:US18164073

    申请日:2023-02-03

    Inventor: Shu Taguchi

    Abstract: A turbomachinery includes a casing, a rotor shaft rotatably attached to the casing, a first blade row fixed to either one of the rotor shaft or the casing, and a second blade row fixed to either one of the rotor shaft or the casing and arranged adjacent to the upstream side or downstream side of the first blade row, wherein the turbomachinery sets the number of first blades and the number of second blades in a manner that the interblade phase angle difference of the second blade row is ±180°.

    Centrifugal compressor
    12.
    发明授权

    公开(公告)号:US10760588B2

    公开(公告)日:2020-09-01

    申请号:US16355979

    申请日:2019-03-18

    Inventor: Shu Taguchi

    Abstract: In a centrifugal compressor including an impeller (70) having rotor blades (74), a shroud (72) surrounding the impeller, and a diffuser (76) having stator vanes (78), the shroud (72) includes a plurality of openings (80) opening toward the impeller (70) in a part thereof adjacent to an impeller outlet portion (42B), and a communication passage (82) communicating the openings (80) with one another, the openings including first openings (80A) that are arranged at a same interval as the stator vanes, and second openings (80B) arranged intermediately between the adjacent first openings.

    VARIABLE STATOR VANE STRUCTURE OF AXIAL COMPRESSOR

    公开(公告)号:US20200063755A1

    公开(公告)日:2020-02-27

    申请号:US16355990

    申请日:2019-03-18

    Inventor: Shu Taguchi

    Abstract: In an axial compressor including a row of rotor blades (70) provided on a rotational shaft (20) around a central axial line of the rotational shaft at a prescribed pitch, and a row of stator vanes (40) provided on a casing around the central axial line at a prescribed pitch so as to adjoin the row of rotor blades on an upstream or downstream side thereof, the rotor blades each extend along a radial line (R) emanating from the central axial line, and the stator vanes each extend along a slanted line (I) that is slanted with respect to a corresponding radial line in a circumferential direction.

    CENTRIFUGAL COMPRESSOR
    14.
    发明申请

    公开(公告)号:US20200040908A1

    公开(公告)日:2020-02-06

    申请号:US16355979

    申请日:2019-03-18

    Inventor: Shu Taguchi

    Abstract: In a centrifugal compressor including an impeller (70) having rotor blades (74), a shroud (72) surrounding the impeller, and a diffuser (76) having stator vanes (78), the shroud (72) includes a plurality of openings (80) opening toward the impeller (70) in a part thereof adjacent to an impeller outlet portion (42B), and a communication passage (82) communicating the openings (80) with one another, the openings including first openings (80A) that are arranged at a same interval as the stator vanes, and second openings (80B) arranged intermediately between the adjacent first openings.

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