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    • 1. 发明授权
    • Centrifugal compressor with surge control, and associated method
    • 具有浪涌控制的离心式压缩机及相关方法
    • US07775759B2
    • 2010-08-17
    • US11696294
    • 2007-04-04
    • Borislav SirakovHua ChenNicolas DeschatrettesJunfei YinGary VrbasDennis Thoren
    • Borislav SirakovHua ChenNicolas DeschatrettesJunfei YinGary VrbasDennis Thoren
    • F04D29/44
    • F04D29/4213F04D29/685Y10S415/914
    • A centrifugal compressor for compressing a fluid comprises a compressor wheel having a plurality of circumferentially spaced blades, and a compressor housing in which the compressor wheel is mounted. The compressor housing includes an inlet duct through which the fluid enters in an axial direction and is led by the inlet duct into the compressor wheel, and a wheel shroud located radially adjacent the tips of the blades. A bleed port is defined in the wheel shroud at a location intermediate the leading and trailing edges of the blades for bleeding off a bleed portion of the fluid being compressed by the compressor wheel. A converging injection nozzle is defined in the duct wall upstream of the leading edges of the blades for injecting the bleed portion of the fluid back into the main fluid flow stream approaching the compressor wheel.
    • 用于压缩流体的离心式压缩机包括具有多个周向间隔开的叶片的压缩机叶轮和压缩机壳体,压缩机叶轮安装在该压缩机壳体中。 压缩机壳体包括入口管道,流体通过该入口管道沿着轴向方向进入并且被入口管道引导到压缩机叶轮中,以及轮辐护罩,其位于径向邻近叶片的尖端处。 在叶轮护罩中限定了在叶片的前缘和后缘之间的位置处的排出口,用于排出被压缩机叶轮压缩的流体的排出部分。 会聚注射喷嘴限定在叶片前缘上游的管道壁中,用于将流体的排放部分回流到靠近压缩机叶轮的主流体流中。
    • 3. 发明申请
    • Compressor and Compressor Housing
    • 压缩机和压缩机外壳
    • US20080247870A1
    • 2008-10-09
    • US11697417
    • 2007-04-06
    • Borislav SirakovThomas BoothNicolas DeschatrettesJuniel YinGary VrbasDennis ThorenPeter R. Davies
    • Borislav SirakovThomas BoothNicolas DeschatrettesJuniel YinGary VrbasDennis ThorenPeter R. Davies
    • F01D1/06
    • F04D29/4213F04D25/024F04D27/0215
    • A housing is disclosed for a compressor having a duct defining a main gas flow axis and blades that draw a fluid through the duct. The blades impart to the fluid a momentum along a main gas flow direction and a swirl. The housing includes a volute configured to extend substantially circumferentially around and fluidly communicate with the duct (at a first location). The volute may be configured to direct a fluid portion flowing thereinto from the duct to have a velocity with a component in a first circumferential direction generally aligned with the swirl. The housing may also include at least one conduit, such as a pipe, in fluid communication with the first volute. The conduit may be configured to redirect the fluid portion to have a velocity with a first component along the main gas flow axis in a direction opposite the main gas flow direction and a second component in a second circumferential direction opposite to the first circumferential direction.
    • 公开了一种用于压缩机的壳体,其具有限定主气流轴线的管道和通过管道吸取流体的叶片。 叶片向流体施加沿着主气体流动方向和涡流的动量。 壳体包括构造成大致周向地延伸并且与管道(在第一位置处)流体连通的蜗壳。 蜗壳可以被配置成引导从管道流入其中的流体部分以具有与沿涡流大致对准的第一圆周方向上的部件的速度。 壳体还可以包括与第一蜗壳流体连通的至少一个管道,例如管道。 导管可以被配置为使流体部分重新定向,使得沿与主气体流动方向相反的方向沿着主气体流动轴线具有第一部件的速度,而在与第一圆周方向相反的第二圆周方向上具有第二部件。
    • 4. 发明授权
    • Compressor and compressor housing
    • 压缩机和压缩机外壳
    • US07874789B2
    • 2011-01-25
    • US11697417
    • 2007-04-06
    • Borislav SirakovThomas BoothNicolas DeschatrettesJuniel YinGary VrbasDennis ThorenPeter R. Davies
    • Borislav SirakovThomas BoothNicolas DeschatrettesJuniel YinGary VrbasDennis ThorenPeter R. Davies
    • F04D29/66
    • F04D29/4213F04D25/024F04D27/0215
    • A housing is disclosed for a compressor having a duct defining a main gas flow axis and blades that draw a fluid through the duct. The blades impart to the fluid a momentum along a main gas flow direction and a swirl. The housing includes a volute configured to extend substantially circumferentially around and fluidly communicate with the duct (at a first location). The volute may be configured to direct a fluid portion flowing thereinto from the duct to have a velocity with a component in a first circumferential direction generally aligned with the swirl. The housing may also include at least one conduit, such as a pipe, in fluid communication with the first volute. The conduit may be configured to redirect the fluid portion to have a velocity with a first component along the main gas flow axis in a direction opposite the main gas flow direction and a second component in a second circumferential direction opposite to the first circumferential direction.
    • 公开了一种用于压缩机的壳体,其具有限定主气流轴线的管道和通过管道吸取流体的叶片。 叶片向流体施加沿着主气体流动方向和涡流的动量。 壳体包括构造成大致周向地延伸并且与管道(在第一位置处)流体连通的蜗壳。 蜗壳可以被配置成引导从管道流入其中的流体部分以具有与沿涡流大致对准的第一圆周方向上的部件的速度。 壳体还可以包括与第一蜗壳流体连通的至少一个管道,例如管道。 导管可以被配置为使流体部分重新定向,使得沿与主气体流动方向相反的方向沿着主气体流动轴线具有第一部件的速度,而在与第一圆周方向相反的第二圆周方向上具有第二部件。
    • 5. 发明授权
    • Compressor and compressor housing
    • 压缩机和压缩机外壳
    • US07942625B2
    • 2011-05-17
    • US11696344
    • 2007-04-04
    • Borislav SirakovNicolas DeschairattesJunfei YinNick NolcheffGary VrbasDennis Thoren
    • Borislav SirakovNicolas DeschairattesJunfei YinNick NolcheffGary VrbasDennis Thoren
    • F04D27/02
    • F04D29/4213F02B37/00F02M26/19F04D29/685Y02T10/144
    • A housing is incorporated as part of a compressor having blades that impart to a fluid a momentum along a main gas flow direction and a swirl. The housing includes a channel that has at least one channel wall and defines an axis substantially aligned with the main gas flow direction. The channel is configured to duct at least some of the fluid. The channel wall defines an internal cavity that extends axially within the channel wall. A bleed passage connects and provides fluid communication between the channel and the cavity. The channel wall defines a plurality of injection passages providing fluid communication between the cavity and the channel at a location spaced in a direction opposite the main gas flow direction from both the bleed passage and the blades. The injection passages have a portion configured to direct fluid from the cavity into the channel with a component along the main gas flow direction and a component opposed to the swirl.
    • 作为具有使流体沿着主气体流动方向和涡流赋予动量的叶片的压缩机的一部分,壳体被结合。 壳体包括具有至少一个通道壁并且限定基本上与主气体流动方向对齐的轴线的通道。 通道被配置成管道至少一些流体。 通道壁限定了在通道壁内轴向延伸的内部空腔。 排放通道连接并在通道和空腔之间提供流体连通。 通道壁限定多个注射通道,其在与主气体流动方向相反的方向上与排出通道和叶片相隔开的位置处在空腔和通道之间提供流体连通。 喷射通道具有被配置为将流体从空腔引导到具有沿着主气体流动方向的部件和与涡流相对的部件的通道中的部分。
    • 6. 发明申请
    • Compressor and Compressor Housing
    • 压缩机和压缩机外壳
    • US20080247866A1
    • 2008-10-09
    • US11696344
    • 2007-04-04
    • Borislav SirakovNicolas DeschairattesJuntei YinNick NolcheffGary VrbasDennis Thoren
    • Borislav SirakovNicolas DeschairattesJuntei YinNick NolcheffGary VrbasDennis Thoren
    • F01B25/02
    • F04D29/4213F02B37/00F02M26/19F04D29/685Y02T10/144
    • A housing is incorporated as part of a compressor having blades that impart to a fluid a momentum along a main gas flow direction and a swirl. The housing includes a channel that has at least one channel wall and defines an axis substantially aligned with the main gas flow direction. The channel is configured to duct at least some of the fluid. The channel wall defines an internal cavity that extends axially within the channel wall. A bleed passage connects and provides fluid communication between the channel and the cavity. The channel wall defines a plurality of injection passages providing fluid communication between the cavity and the channel at a location spaced in a direction opposite the main gas flow direction from both the bleed passage and the blades. The injection passages have a portion configured to direct fluid from the cavity into the channel with a component along the main gas flow direction and a component opposed to the swirl.
    • 作为具有使流体沿着主气体流动方向和涡流赋予动量的叶片的压缩机的一部分,壳体被结合。 壳体包括具有至少一个通道壁并且限定基本上与主气体流动方向对齐的轴线的通道。 通道被配置成管道至少一些流体。 通道壁限定了在通道壁内轴向延伸的内部空腔。 排放通道连接并在通道和空腔之间提供流体连通。 通道壁限定多个注射通道,其在与主气体流动方向相反的方向上与排出通道和叶片相隔开的位置处在空腔和通道之间提供流体连通。 喷射通道具有被配置为将流体从空腔引导到具有沿着主气体流动方向的部件和与涡流相对的部件的通道中的部分。