Inlet connecting piece for an axial-flow compressor
    1.
    发明授权
    Inlet connecting piece for an axial-flow compressor 有权
    用于轴流压缩机的进口连接件

    公开(公告)号:US09004856B2

    公开(公告)日:2015-04-14

    申请号:US12866077

    申请日:2008-11-03

    摘要: An inlet connection piece for an axial compressor, particularly for a turbocompressor, includes an inlet housing (1) in which is arranged a bearing housing (2) with a bearing (3), particularly a radial and/or axial bearing, for a rotor. The bearing housing (2) is connected to the inlet housing (1) by an inlet strut (4) which is connected to the inlet housing in a front cross section. The center of the bearing (3) is arranged axially in the flow direction of a fluid to be compressed behind the area center of the front cross section by at least 0.1-times, particularly at least 0.15-times, particularly at least 0.2-times, particularly at least 0.25-times, the chord length of the front cross section. In addition or alternatively, a fluid passage (5, 6) is formed in the inlet strut (4), and at least portions of this fluid passage (5, 6) form an acute angle with a normal plane relative to the longitudinal axis of the inlet connection piece.

    摘要翻译: 用于轴向压缩机的入口连接件,特别是用于涡轮压缩机的入口连接件包括入口壳体(1),其中布置有用于转子的轴承(3),特别是径向和/或轴向轴承的轴承壳体(2) 。 轴承壳体(2)通过入口支柱(4)连接到入口壳体(1),入口支柱(4)以前横截面连接到入口壳体。 轴承(3)的中心轴向地被布置在待压缩流体的流动方向后面的前横截面的区域中心的至少0.1倍,特别是至少0.15倍,特别是至少0.2倍 ,特别是至少0.25倍的前横截面的弦长。 另外或替代地,在入口支柱(4)中形成流体通道(5,6),并且该流体通道(5,6)的至少一部分与正常平面相对于纵向轴线的纵向轴线形成锐角 入口连接件。

    Inlet Connecting Piece for an Axial-Flow Compressor
    2.
    发明申请
    Inlet Connecting Piece for an Axial-Flow Compressor 有权
    用于轴流压缩机的进口连接件

    公开(公告)号:US20100329861A1

    公开(公告)日:2010-12-30

    申请号:US12866077

    申请日:2008-11-03

    摘要: An inlet connection piece for an axial compressor, particularly for a turbocompressor, includes an inlet housing (1) in which is arranged a bearing housing (2) with a bearing (3), particularly a radial and/or axial bearing, for a rotor. The bearing housing (2) is connected to the inlet housing (1) by an inlet strut (4) which is connected to the inlet housing in a front cross section. The center of the bearing (3) is arranged axially in the flow direction of a fluid to be compressed behind the area center of the front cross section by at least 0.1-times, particularly at least 0.15-times, particularly at least 0.2-times, particularly at least 0.25-times, the chord length of the front cross section. In addition or alternatively, a fluid passage (5, 6) is formed in the inlet strut (4), and at least portions of this fluid passage (5, 6) form an acute angle with a normal plane relative to the longitudinal axis of the inlet connection piece.

    摘要翻译: 用于轴向压缩机的入口连接件,特别是用于涡轮压缩机的入口连接件包括入口壳体(1),其中布置有具有用于转子的轴承(3),特别是径向和/或轴向轴承的轴承壳体(2) 。 轴承壳体(2)通过入口支柱(4)连接到入口壳体(1),入口支柱(4)以前横截面连接到入口壳体。 轴承(3)的中心轴向地被布置在待压缩流体的流动方向后面的前横截面的区域中心的至少0.1倍,特别是至少0.15倍,特别是至少0.2倍 ,特别是至少0.25倍的前横截面的弦长。 另外或替代地,在入口支柱(4)中形成流体通道(5,6),并且该流体通道(5,6)的至少一部分与正常平面相对于纵向轴线的纵向轴线形成锐角 入口连接件。

    COMPRESSOR ARRANGEMENT
    4.
    发明申请
    COMPRESSOR ARRANGEMENT 有权
    压缩机安排

    公开(公告)号:US20150139788A1

    公开(公告)日:2015-05-21

    申请号:US14495501

    申请日:2014-09-24

    IPC分类号: F04D17/02

    摘要: A compressor arrangement has a common shaft, an axial compressor having at least a single-stage, and a radial compressor having at least single-stage. Assemblies of the, or each, axial compressor stage on the rotor side and assemblies of the, or each, radial compressor stage on the rotor side are attached to a common shaft (4). A ratio between a maximum diameter of the shaft (4) in the region of the axial compressor (2) and a minimum radial impeller seat diameter of the shaft (4) in the region of the radial compressor (3) is between 1.5 and 3.0.

    摘要翻译: 压缩机装置具有公共轴,具有至少单级的轴向压缩机和至少具有单级的径向压缩机。 转子侧的或每个轴向压缩机级的组件或转子侧上的每个或径向压缩机级的组件都附接到公共轴(4)。 轴向压缩机(2)区域中的轴(4)的最大直径与径向压缩机(3)区域中的轴(4)的最小径向叶轮座直径之间的比率在1.5和3.0之间 。

    Cover disk for a closed impeller
    5.
    发明授权
    Cover disk for a closed impeller 有权
    盖盘用于封闭的叶轮

    公开(公告)号:US08469669B2

    公开(公告)日:2013-06-25

    申请号:US12919553

    申请日:2009-03-10

    申请人: Henning Ressing

    发明人: Henning Ressing

    IPC分类号: F01D5/22

    CPC分类号: F04D29/2216 F04D29/284

    摘要: A cover disk (1) for a closed rotor of a radial flow machine or diagonal flow machine for defining a flow channel has a wall thickness which has a local maximum along the profile mean line of the meridional cross section of the cover disk between a first front side (2) and a second front side (3) of the cover disk. An outer surface (1.2) of the cover disk remote of the flow channel has in the area of this local maximum a convex curvature with a radius (R2.2) whose ratio (R2.2/D2) to an outer diameter (D2) of the rotor is within a range of 0.05 to 0.5 (0.05≦R2.2/D2≦0.5).

    摘要翻译: 用于限定流动通道的径向流动机器或对角流动机器的闭合转子的盖盘(1)具有壁厚,该壁厚沿着盖盘的子午线横截面的轮廓平均线在第一 盖板的前侧(2)和第二前侧(3)。 远离流道的盖盘的外表面(1.2)在该局部最大的区域中具有半径(R2.2)(R2.2 / D2)与外径(D2)的半径的凸曲面, 的转子在0.05至0.5的范围内(0.05 @ R2.2 / D2 @ 0.5)。

    COVER DISK FOR A CLOSED IMPELLER
    6.
    发明申请
    COVER DISK FOR A CLOSED IMPELLER 有权
    封闭的密封盘

    公开(公告)号:US20110008160A1

    公开(公告)日:2011-01-13

    申请号:US12919553

    申请日:2009-03-10

    申请人: Henning Ressing

    发明人: Henning Ressing

    IPC分类号: F04D29/44

    CPC分类号: F04D29/2216 F04D29/284

    摘要: A cover disk (1) for a closed rotor of a radial flow machine or diagonal flow machine for defining a flow channel has a wall thickness which has a local maximum along the profile mean line of the meridional cross section of the cover disk between a first front side (2) and a second front side (3) of the cover disk. An outer surface (1.2) of the cover disk remote of the flow channel has in the area of this local maximum a convex curvature with a radius (R2.2) whose ratio (R2.2/D2) to an outer diameter (D2) of the rotor is within a range of 0.05 to 0.5 (0.05

    摘要翻译: 用于限定流动通道的径向流动机器或对角流动机器的闭合转子的盖盘(1)具有壁厚,该壁厚沿着盖盘的子午线横截面的轮廓平均线在第一 盖板的前侧(2)和第二前侧(3)。 远离流道的盖盘的外表面(1.2)在该局部最大的区域中具有半径(R2.2)(R2.2 / D2)与外径(D2)的半径的凸曲面, 的转子在0.05〜0.5(0.05