Turbo compressor
    1.
    发明授权
    Turbo compressor 有权
    涡轮压缩机

    公开(公告)号:US07942628B2

    公开(公告)日:2011-05-17

    申请号:US11566337

    申请日:2006-12-04

    IPC分类号: F01D3/02

    摘要: A first compression stage and a second compression stage being arranged at positions adjacent to each other. The first centrifugal impeller and the second centrifugal impeller are arranged in such an orientation that back sides of the first centrifugal impeller and the second centrifugal impeller face to each other. A connection flow path is formed in the first housing and the second housing for introducing the compressed fluid from the first compression stage into the second compression stage. An upstream portion of the connection flow path is formed integrally with the first housing, and a downstream portion of the connection flow path is formed integrally with the second housing.

    摘要翻译: 第一压缩级和第二压缩级布置在彼此相邻的位置。 第一离心式叶轮和第二离心式叶轮配置成使得第一离心式叶轮和第二离心式叶轮的背面相互面对的方向。 连接流路形成在第一壳体和第二壳体中,用于将压缩流体从第一压缩级引入第二压缩级。 连接流路的上游部与第一壳体一体形成,连接流路的下游部与第二壳体一体形成。

    TURBO COMPRESSOR
    2.
    发明申请
    TURBO COMPRESSOR 有权
    涡轮压缩机

    公开(公告)号:US20070147984A1

    公开(公告)日:2007-06-28

    申请号:US11566337

    申请日:2006-12-04

    IPC分类号: F01D3/02

    摘要: A first compression stage and a second compression stage being arranged at positions adjacent to each other. The first centrifugal impeller and the second centrifugal impeller are arranged in such an orientation that back sides of the first centrifugal impeller and the second centrifugal impeller face to each other. A connection flow path is formed in the first housing and the second housing for introducing the compressed fluid from the first compression stage into the second compression stage. An upstream portion of the connection flow path is formed integrally with the first housing, and a downstream portion of the connection flow path is formed integrally with the second housing.

    摘要翻译: 第一压缩级和第二压缩级布置在彼此相邻的位置。 第一离心式叶轮和第二离心式叶轮配置成使得第一离心式叶轮和第二离心式叶轮的背面相互面对的方向。 连接流路形成在第一壳体和第二壳体中,用于将压缩流体从第一压缩级引入第二压缩级。 连接流路的上游部与第一壳体一体形成,连接流路的下游部与第二壳体一体形成。

    TURBO COMPRESSOR
    3.
    发明申请
    TURBO COMPRESSOR 有权
    涡轮压缩机

    公开(公告)号:US20070147985A1

    公开(公告)日:2007-06-28

    申请号:US11566428

    申请日:2006-12-04

    IPC分类号: F01D3/04

    摘要: A first centrifugal impeller and a second centrifugal impeller are arranged in such an orientation that back sides of the first centrifugal impeller and the second centrifugal impeller face to each other. Bearings are cylindrical roller bearings and a thrust bearing. The cylindrical roller bearings are arranged at two axially spaced supporting positions respectively, and support a radial load applied to the rotating shaft. The thrust bearing supports a thrust load applied to the rotating shaft.

    摘要翻译: 以第一离心式叶轮和第二离心式叶轮的背面彼此面对的方式配置第一离心式叶轮和第二离心式叶轮。 轴承是圆柱滚子轴承和推力轴承。 圆柱滚子轴承分别布置在两个轴向间隔的支撑位置,并且支撑施加到旋转轴的径向载荷。 推力轴承支承施加在旋转轴上的推力。

    Turbo compressor
    4.
    发明授权
    Turbo compressor 有权
    涡轮压缩机

    公开(公告)号:US07690887B2

    公开(公告)日:2010-04-06

    申请号:US11566428

    申请日:2006-12-04

    IPC分类号: F01D3/04

    摘要: A first centrifugal impeller and a second centrifugal impeller are arranged in such an orientation that back sides of the first centrifugal impeller and the second centrifugal impeller face to each other. Bearings are cylindrical roller bearings and a thrust bearing. The cylindrical roller bearings are arranged at two axially spaced supporting positions respectively, and support a radial load applied to the rotating shaft. The thrust bearing supports a thrust load applied to the rotating shaft.

    摘要翻译: 以第一离心式叶轮和第二离心式叶轮的背面彼此面对的方式配置第一离心式叶轮和第二离心式叶轮。 轴承是圆柱滚子轴承和推力轴承。 圆柱滚子轴承分别布置在两个轴向间隔的支撑位置,并且支撑施加到旋转轴的径向载荷。 推力轴承支承施加在旋转轴上的推力。

    Casing structure
    6.
    发明授权
    Casing structure 有权
    套管结构

    公开(公告)号:US08920118B2

    公开(公告)日:2014-12-30

    申请号:US13074298

    申请日:2011-03-29

    摘要: Provided is a casing structure including: an annular seal member which is disposed at a connection portion between first and second casings to keep air-tightness between an internal space formed by connecting the first and second casings to each other and an outside of the internal space; a first screw member which is threaded from the internal space, is disposed at the inside of the seal member in the radial direction, and fastens the first and second casings to each other; and a second screw member which is threaded from the outside, is disposed at the outside of the seal member in the radial direction, and fastens the first and second casings to each other.

    摘要翻译: 提供一种壳体结构,其包括:环形密封构件,其设置在第一和第二壳体之间的连接部分处,以通过将第一和第二壳体彼此连接形成的内部空间与内部空间的外部保持气密性 ; 从所述内部空间螺纹的第一螺纹构件沿径向设置在所述密封构件的内部,并且将所述第一和第二壳体彼此紧固; 并且从外部螺纹的第二螺纹构件沿径向设置在密封构件的外侧,并且将第一和第二壳体彼此紧固。

    Turbocompressor and turborefrigerator for simplified labor and reduced cost

    公开(公告)号:US09714662B2

    公开(公告)日:2017-07-25

    申请号:US13578838

    申请日:2011-02-17

    申请人: Kazuaki Kurihara

    发明人: Kazuaki Kurihara

    摘要: Provided is a turbocompressor (4) having a drive part (12) generating rotational power, an impeller (22a) to which the rotational power of the drive part (12) is transmitted to rotate, a plurality of gears (31, 32) transmitting the rotational power of the drive part (12) to the impeller (22a), and a drive part casing (13) in which the drive part (12) is installed. This turbocompressor (4) includes an impeller casing (22e) installed around the impeller (22a), and a gear casing (33) configured to be formed independently of the impeller casing (22e) and the drive part casing (13), to couple the impeller casing (22e) and the drive part casing (13), and to form an accommodation space (33a) in which the plurality of gears (31, 32) are accommodated. With this configuration, in manufacturing the turbocompressor, a working process can be simplified and working labor and cost can be reduced.

    TURBOCOMPRESSOR AND TURBOREFRIGERATOR
    8.
    发明申请
    TURBOCOMPRESSOR AND TURBOREFRIGERATOR 有权
    涡轮增压器和涡轮发电机

    公开(公告)号:US20130039746A1

    公开(公告)日:2013-02-14

    申请号:US13578838

    申请日:2011-02-17

    申请人: Kazuaki Kurihara

    发明人: Kazuaki Kurihara

    IPC分类号: F01D15/12

    摘要: Provided is a turbocompressor (4) having a drive part (12) generating rotational power, an impeller (22a) to which the rotational power of the drive part (12) is transmitted to rotate, a plurality of gears (31, 32) transmitting the rotational power of the drive part (12) to the impeller (22a), and a drive part casing (13) in which the drive part (12) is installed. This turbocompressor (4) includes an impeller casing (22e) installed around the impeller (22a), and a gear casing (33) configured to be formed independently of the impeller casing (22e) and the drive part casing (13), to couple the impeller casing (22e) and the drive part casing (13), and to form an accommodation space (33a) in which the plurality of gears (31, 32) are accommodated. With this configuration, in manufacturing the turbocompressor, a working process can be simplified and working labor and cost can be reduced.

    摘要翻译: 本发明提供一种具有产生旋转动力的驱动部(12)的涡轮压缩机(4),驱动部(12)的旋转动力传递到其上的旋转叶轮(22a),传递多个齿轮 驱动部件(12)到叶轮(22a)的旋转动力以及安装有驱动部件(12)的驱动部件壳体(13)。 该涡轮压缩机(4)包括安装在叶轮(22a)周围的叶轮壳体(22e)和与叶轮壳体(22e)和驱动部件壳体(13)独立形成的齿轮箱(33) 叶轮壳体(22e)和驱动部件壳体(13),并且形成容纳多个齿轮(31,32)的容置空间(33a)。 通过这样的结构,在制造涡轮压缩机的情况下,能够简化工作过程,能够降低劳动力和成本。

    GAS GENERATOR AND GAS GENERATION METHOD
    9.
    发明申请
    GAS GENERATOR AND GAS GENERATION METHOD 有权
    气体发生器和气体发生方法

    公开(公告)号:US20120058041A1

    公开(公告)日:2012-03-08

    申请号:US13292247

    申请日:2011-11-09

    IPC分类号: C01B31/18 C01B3/10 B01J15/00

    摘要: A gas generator includes a processing vessel defining a processing space and holding a support body therein, an evacuation system evacuating the processing space; a metal oxide film of a perovskite structure containing oxygen defects formed on the support body, a source gas supplying port supplying a source gas containing molecules of a source compound of carbon dioxide or water into the processing space, a gas outlet port for extracting a product gas containing molecules of a product compound in which oxygen atoms are removed from said source compound, and a heating part heating the support body.

    摘要翻译: 气体发生器包括限定处理空间并将支撑体保持在其中的处理容器,排空系统排空处理空间; 包含形成在支撑体上的氧缺陷的钙钛矿结构的金属氧化物膜,向处理空间供给含有二氧化碳或水源化合物的分子的源气体的源气体供给口,用于提取产物的气体出口 含有其中从所述源化合物中除去氧原子的产物化合物的分子的气体和加热所述载体的加热部分。