CENTRIFUGAL COMPRESSOR HAVING AN ASYMMETRIC SELF-RECIRCULATING CASING TREATMENT
    1.
    发明申请
    CENTRIFUGAL COMPRESSOR HAVING AN ASYMMETRIC SELF-RECIRCULATING CASING TREATMENT 审中-公开
    具有不对称自回收箱处理的离心式压缩机

    公开(公告)号:US20120321440A1

    公开(公告)日:2012-12-20

    申请号:US13578163

    申请日:2011-02-03

    IPC分类号: F01D1/12

    摘要: A centrifugal compressor includes an asymmetric self-recirculating casing treatment that includes, on an inner face of a casing 10, a suction ring groove 1, a ring guide channel 2 and a back-flow ring groove 3 to form a self-recirculating channel. An axial distance Sr from an upstream end face of the suction ring groove 1 to an impeller full blade leading edge 4 or a width br of the suction ring groove 1 is represented as A·sin(α+θ0)+A0 and is distributed in a sinusoidal shape in a circumferential direction, an initial phase angle θ0 is in a range of 0°≦θ0≦360°, and a circumferential angle α of the casing 10 has a definition range of θ0≦α≦θ0+360°. In the expression, A denotes amplitude of distribution of the axial distance Sr or the width br, and A0 denotes an average of the axial distance Sr or the width br.

    摘要翻译: 离心压缩机包括不对称的自再循环壳体处理,其在壳体10的内表面上包括吸入环槽1,环形引导通道2和回流环槽3,以形成自再循环通道。 从吸入环槽1的上游端面到叶轮全叶片前缘4或吸入环槽1的宽度br的轴向距离Sr表示为A·sin(α+η 0)+ A0,为 分布在圆周方向上的正弦形状,初始相位角和角度0在0°< lE;& t; 0≦̸ 360°的范围内,并且壳体10的圆周角度α具有&...的定义范围; 0& ;α≦̸&thetas; 0 + 360°。 在表达式中,A表示轴向距离Sr或宽度br的分布的振幅,A0表示轴向距离Sr或宽度br的平均值。

    Centrifugal compressor having an asymmetric self-recirculating casing treatment
    2.
    发明授权
    Centrifugal compressor having an asymmetric self-recirculating casing treatment 有权
    具有不对称自循环套管处理的离心式压缩机

    公开(公告)号:US09234526B2

    公开(公告)日:2016-01-12

    申请号:US13578137

    申请日:2011-02-03

    IPC分类号: F04D29/42 F04D29/68

    摘要: A centrifugal compressor includes an asymmetric self-recirculating casing treatment that includes, on an inner face of a casing 10, a suction ring groove 1, a ring guide channel 2 and a back-flow ring groove 3 to form a self-recirculating channel. An axial-direction position Sr from an upstream end face of the suction ring groove to an impeller full blade leading edge 4 or a width br of the suction ring groove 1 is represented as A(α·D−β·D)2+A0 and is distributed in a parabolic shape in a circumferential direction. An initial phase angle θ0 is in a range of 0≦θ0≦2π. A circumferential angle α of the casing has a definition range of θ0≦α≦θ0+2π. In the expression, A denotes a parameter of the parabola in the axial-direction position Sr or the width br, and A0 denotes an extreme of the axial-direction position Sr or the width br when corresponding circumferential angle β and the α are equal at an extreme point of distribution of the parabola.

    摘要翻译: 离心压缩机包括不对称的自再循环壳体处理,其在壳体10的内表面上包括吸入环槽1,环形引导通道2和回流环槽3,以形成自再循环通道。 从吸入环槽的上游端面到吸入环槽1的叶轮全叶片前缘4或宽度br的轴向位置Sr表示为A(α·D-&bgr·D)2+ A0并且沿圆周方向以抛物线形状分布。 初始相位角和角度0在0≦̸&Thetas; 0≦̸ 2&pgr的范围内。 外壳的圆周角度α具有&...的定义范围; 0≦̸α≦̸&thetas; 0 + 2&pgr。 在该表达式中,A表示轴向位置Sr或宽度br的抛物线的参数,A0表示当对应的圆周角度&bgr时的轴向位置Sr或宽度br的极端值。 并且α在抛物线的极端分布点处相等。

    CENTRIFUGAL COMPRESSOR HAVING AN ASYMMETRIC SELF-RECIRCULATING CASING TREATMENT
    6.
    发明申请
    CENTRIFUGAL COMPRESSOR HAVING AN ASYMMETRIC SELF-RECIRCULATING CASING TREATMENT 有权
    具有不对称自回收箱处理的离心式压缩机

    公开(公告)号:US20120315127A1

    公开(公告)日:2012-12-13

    申请号:US13578188

    申请日:2011-02-03

    IPC分类号: F01D1/12

    CPC分类号: F04D29/4213 F04D29/685

    摘要: A centrifugal compressor has a casing 7. In the casing 7 is formed a back-flow channel 9 to return fluid from a downstream position of an impeller full blade leading edge 6a to an upstream position of the impeller full blade leading edge 6a. The back-flow channel 9 includes a suction ring groove 9a and a back-flow ring groove 9b. The suction ring groove opens at the downstream position on the inner face 7a of the casing 7, and extends in the circumferential direction. The back-flow ring groove opens at the upstream position on the inner face 7a, and extends in the circumferential direction. Distribution in the circumferential direction of the axial-direction position of the suction ring groove 9a or a width of the suction ring groove 9a is asymmetric with reference to the rotation axis.

    摘要翻译: 离心压缩机具有壳体7.在壳体7中形成有用于将流体从叶轮全叶片前缘6a的下游位置返回到叶轮全叶片前缘6a的上游位置的后部流路9。 背流通道9包括吸入环槽9a和后流环槽9b。 吸入环槽在壳体7的内表面7a的下游位置开口,并且在圆周方向上延伸。 背流环槽在内表面7a上的上游位置开口,并沿圆周方向延伸。 吸入环槽9a的轴向位置的圆周方向的分布或者吸入环槽9a的宽度相对于旋转轴线是不对称的。

    CENTRIFUGAL COMPRESSOR HAVING AN ASYMMETRIC SELF-RECIRCULATING CASING TREATMENT
    7.
    发明申请
    CENTRIFUGAL COMPRESSOR HAVING AN ASYMMETRIC SELF-RECIRCULATING CASING TREATMENT 有权
    具有不对称自回收箱处理的离心式压缩机

    公开(公告)号:US20120308372A1

    公开(公告)日:2012-12-06

    申请号:US13578137

    申请日:2011-02-03

    IPC分类号: F04D29/42

    摘要: A centrifugal compressor includes an asymmetric self-recirculating casing treatment that includes, on an inner face of a casing 10, a suction ring groove 1, a ring guide channel 2 and a back-flow ring groove 3 to form a self-recirculating channel. An axial-direction position Sr from an upstream end face of the suction ring groove to an impeller full blade leading edge 4 or a width br of the suction ring groove 1 is represented as A(α·D−β·D)2+A0 and is distributed in a parabolic shape in a circumferential direction. An initial phase angle θ0 is in a range of 0≦θ0≦2π. A circumferential angle α of the casing has a definition range of θ0≦α≦θ0+2λ. In the expression, A denotes a parameter of the parabola in the axial-direction position Sr or the width br, and A0 denotes an extreme of the axial-direction position Sr or the width br when corresponding circumferential angle β and the α are equal at an extreme point of distribution of the parabola.

    摘要翻译: 离心压缩机包括不对称的自再循环壳体处理,其在壳体10的内表面上包括吸入环槽1,环形引导通道2和回流环槽3,以形成自再循环通道。 从吸入环槽的上游端面到吸入环槽1的叶轮全叶片前缘4或宽度br的轴向位置Sr表示为A(α·D-&bgr·D)2+ A0并且沿圆周方向以抛物线形状分布。 初始相位角和角度0在0≦̸&Thetas; 0≦̸ 2&pgr的范围内。 壳体的圆周角度α具有&...的定义范围; 0≦̸α≦̸&thetas; 0 +2λ。 在该表达式中,A表示轴向位置Sr或宽度br的抛物线的参数,A0表示当对应的圆周角度&bgr时的轴向位置Sr或宽度br的极端; 并且α在抛物线的极端分布点处相等。