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    Scroll compressor with fluid injection feature
    1.
    发明授权
    Scroll compressor with fluid injection feature 有权
    带流体注入功能的涡旋压缩机

    公开(公告)号：US08764423B2

    公开(公告)日：2014-07-01

    申请号：US13528285

    申请日：2012-06-20

    申请人： Kirill M. Ignatiev ,  James F. Fogt

    发明人： Kirill M. Ignatiev ,  James F. Fogt

    IPC分类号： F03C2/00 ,  F03C4/00 ,  F04C18/00

    CPC分类号： F04C18/0215 ,  F04C18/0253 ,  F04C18/0261 ,  F04C23/008 ,  F04C27/005 ,  F04C29/0007 ,  F04C29/02 ,  F04C2240/50 ,  Y10S418/01

    摘要： A compressor may include a shell assembly, a first scroll member located within the shell assembly and including a first end plate and a first spiral wrap extending from the first end plate, and a second scroll member located within the shell assembly, supported for orbital movement relative to the first scroll member and including a second end plate and a second spiral wrap extending from the second end plate and meshingly engaged with the first spiral wrap to form compression pockets. The first scroll member may define a fluid injection port and the second scroll member may define a passage in communication with the fluid injection port and at least one of the compression pockets to provide pressurized vapor from the fluid injection port to the at least one of the compression pockets.

    摘要翻译： 压缩机可以包括壳体组件，位于壳体组件内的第一涡旋构件，并且包括第一端板和从第一端板延伸的第一螺旋形涡卷，以及位于壳组件内的第二涡旋构件，支撑用于轨道运动 相对于第一涡旋构件并且包括第二端板和从第二端板延伸并与第一螺旋形卷绕物啮合地形成压缩腔的第二螺旋形涡卷。 第一涡旋构件可以限定流体喷射端口，并且第二涡旋构件可以限定与流体喷射端口和至少一个压缩凹穴连通的通道，以将压力蒸汽从流体喷射端口提供到至少一个 压缩口袋。

    SCROLL COMPRESSOR
    2.
    发明申请
    SCROLL COMPRESSOR 有权
    滚动压缩机

    公开(公告)号：US20120258004A1

    公开(公告)日：2012-10-11

    申请号：US13528285

    申请日：2012-06-20

    申请人： Kirill M. Ignatiev ,  James F. Fogt ,  Masao Akei

    发明人： Kirill M. Ignatiev ,  James F. Fogt ,  Masao Akei

    IPC分类号： F04C2/00

    CPC分类号： F04C18/0215 ,  F04C18/0253 ,  F04C18/0261 ,  F04C23/008 ,  F04C27/005 ,  F04C29/0007 ,  F04C29/02 ,  F04C2240/50 ,  Y10S418/01

    摘要： A compressor may include a shell assembly, a first scroll member located within the shell assembly and including a first end plate and a first spiral wrap extending from the first end plate, and a second scroll member located within the shell assembly, supported for orbital movement relative to the first scroll member and including a second end plate and a second spiral wrap extending from the second end plate and meshingly engaged with the first spiral wrap to form compression pockets. The first scroll member may define a fluid injection port and the second scroll member may define a passage in communication with the fluid injection port and at least one of the compression pockets to provide pressurized vapor from the fluid injection port to the at least one of the compression pockets.

    摘要翻译： 压缩机可以包括壳体组件，位于壳体组件内的第一涡旋构件，并且包括第一端板和从第一端板延伸的第一螺旋形涡卷，以及位于壳组件内的第二涡旋构件，支撑用于轨道运动 相对于第一涡旋构件并且包括第二端板和从第二端板延伸并与第一螺旋形卷绕物啮合地形成压缩腔的第二螺旋形涡卷。 第一涡旋构件可以限定流体喷射端口，并且第二涡旋构件可以限定与流体喷射端口和至少一个压缩凹穴连通的通道，以将压力蒸汽从流体喷射端口提供到至少一个 压缩口袋。

    Scroll Compressor
    3.
    发明申请
    Scroll Compressor 有权
    涡旋压缩机

    公开(公告)号：US20090191080A1

    公开(公告)日：2009-07-30

    申请号：US12420519

    申请日：2009-04-08

    申请人： Kirill M. Ignatiev ,  James F. Fogt ,  Masao Akei

    发明人： Kirill M. Ignatiev ,  James F. Fogt ,  Masao Akei

    IPC分类号： F04C18/02 ,  F04C29/12

    CPC分类号： F04C18/0215 ,  F04C18/0253 ,  F04C18/0261 ,  F04C23/008 ,  F04C27/005 ,  F04C29/0007 ,  F04C29/02 ,  F04C2240/50 ,  Y10S418/01

    摘要： A scroll compressor an orbiting scroll member including a second end plate, a second wrap extending from the second end plate and meshingly engaged with the first wrap to form a suction pocket in fluid communication with a suction pressure region of the compressor, intermediate compression pockets, and a discharge pocket in fluid communication with the discharge passage. An auxiliary passage is in fluid communication with one of the intermediate compression pockets to provide pressurized fluid to the chamber to deflect the first end plate and the first wrap axially toward the orbiting scroll member.

    摘要翻译： 涡旋压缩机包括具有第二端板的动涡旋件，从第二端板延伸并与第一包裹物啮合的第二卷绕件，以形成与压缩机的吸入压力区域流体连通的吸入口，中间压缩袋 以及与排出通道流体连通的排出口。 辅助通道与中间压缩袋中的一个流体连通，以向腔室提供加压流体，以使第一端板和第一涡卷轴向偏向绕动涡旋件。

    SCROLL COMPRESSOR
    4.
    发明申请
    SCROLL COMPRESSOR 有权
    滚动压缩机

    公开(公告)号：US20110044834A1

    公开(公告)日：2011-02-24

    申请号：US12938848

    申请日：2010-11-03

    申请人： Kirill M. Ignatiev

    发明人： Kirill M. Ignatiev

    IPC分类号： F01C21/04 ,  F01C1/02

    CPC分类号： F04C18/0215 ,  F04C18/0253 ,  F04C18/0261 ,  F04C23/008 ,  F04C27/005 ,  F04C29/0007 ,  F04C29/02 ,  F04C2240/50 ,  Y10S418/01

    摘要： A compressor may include a shell assembly, a first scroll member, and a second scroll member. The first scroll member may be located within the shell assembly and may include a first end plate and a first spiral wrap extending from a first side of the first end plate. The first end plate may define an oil groove extending into the first side. The second scroll member may be located within the shell assembly and supported for orbital movement relative to the first scroll member. The second scroll member may include a second end plate and a second spiral wrap extending from the second end plate and meshingly engaged with the first spiral wrap to form compression pockets.

    摘要翻译： 压缩机可以包括壳体组件，第一涡旋构件和第二涡旋构件。 第一涡旋构件可以位于壳体组件内，并且可以包括从第一端板的第一侧延伸的第一端板和第一螺旋形涡卷。 第一端板可以限定延伸到第一侧的油槽。 第二涡旋构件可以位于壳体组件内并被支撑用于相对于第一涡旋构件进行轨道运动。 第二涡旋构件可以包括第二端板和从第二端板延伸的第二螺旋形涡卷，并与第一螺旋涡卷啮合地形成压缩腔。

    Scroll compressor for natural gas
    5.
    发明授权
    Scroll compressor for natural gas 有权
    涡旋压缩机用于天然气

    公开(公告)号：US06257840B1

    公开(公告)日：2001-07-10

    申请号：US09435532

    申请日：1999-11-08

    申请人： Kirill M. Ignatiev ,  James F. Fogt ,  Kenneth L. Feathers

    发明人： Kirill M. Ignatiev ,  James F. Fogt ,  Kenneth L. Feathers

    IPC分类号： F04B4900

    CPC分类号： F04C29/04 ,  F04C18/0215 ,  F04C23/008 ,  F04C29/023 ,  F04C29/026 ,  F04C2240/603

    摘要： A scroll type compressor has both a high pressure lubricant sump and a low pressure lubricant sump. Lubricant from the low pressure lubricant sump is supplied to the various bearings, thrust surfaces and other moving components of the compressor. It is then rested in such a way that it can absorb heat from the motor windings thus maintaining the operating temperature of the motor. Lubricant from the high pressure sump is supplied to the moving compression chambers defined by the scrolls at a point intermediate suction and discharge. The lubricant supplied from the high pressure sump is first cooled and then used to cool the low pressure sump prior to being supplied to the moving compression chambers. The compressed gas is routed through two lubricant separators and a gas cooler prior to being supplied for its intended use.

    摘要翻译： 涡旋式压缩机具有高压润滑油底壳和低压润滑油底壳。 来自低压润滑剂油槽的润滑剂被供应到压缩机的各种轴承，推力表面和其它运动部件。 然后它以这样的方式安置，使得它可以吸收来自电动机绕组的热量，从而保持电动机的工作温度。 来自高压油槽的润滑剂在抽吸和排出的中点被供给到由涡旋件限定的移动压缩室。 首先将从高压贮槽供应的润滑剂冷却，然后在供给到移动的压缩室之前用于冷却低压贮槽。 压缩气体在供给其预期用途之前通过两个润滑剂分离器和气体冷却器。

    Scroll compressor including lubrication features
    6.
    发明授权
    Scroll compressor including lubrication features 有权
    涡旋压缩机包括润滑功能

    公开(公告)号：US08226387B2

    公开(公告)日：2012-07-24

    申请号：US12938848

    申请日：2010-11-03

    申请人： Kirill M. Ignatiev

    发明人： Kirill M. Ignatiev

    IPC分类号： F03C2/00 ,  F03C4/00 ,  F04C18/00

    CPC分类号： F04C18/0215 ,  F04C18/0253 ,  F04C18/0261 ,  F04C23/008 ,  F04C27/005 ,  F04C29/0007 ,  F04C29/02 ,  F04C2240/50 ,  Y10S418/01

    摘要： A compressor may include a shell assembly, a first scroll member, and a second scroll member. The first scroll member may be located within the shell assembly and may include a first end plate and a first spiral wrap extending from a first side of the first end plate. The first end plate may define an oil groove extending into the first side. The second scroll member may be located within the shell assembly and supported for orbital movement relative to the first scroll member. The second scroll member may include a second end plate and a second spiral wrap extending from the second end plate and meshingly engaged with the first spiral wrap to form compression pockets.

    摘要翻译： 压缩机可以包括壳体组件，第一涡旋构件和第二涡旋构件。 第一涡旋构件可以位于壳体组件内，并且可以包括从第一端板的第一侧延伸的第一端板和第一螺旋形涡卷。 第一端板可以限定延伸到第一侧的油槽。 第二涡旋构件可以位于壳体组件内并被支撑用于相对于第一涡旋构件进行轨道运动。 第二涡旋构件可以包括第二端板和从第二端板延伸的第二螺旋形涡卷，并与第一螺旋涡卷啮合地形成压缩腔。