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    Overhung axial flow compressor, reactor and method
    81.
    发明授权
    Overhung axial flow compressor, reactor and method 有权
    悬臂式流量压缩机，电抗器及方法

    公开(公告)号：US08361407B2

    公开(公告)日：2013-01-29

    申请号：US12888906

    申请日：2010-09-23

    申请人： Joseph Cruickshank ,  Massimo Camatti ,  Ronald John DeGroot

    发明人： Joseph Cruickshank ,  Massimo Camatti ,  Ronald John DeGroot

    IPC分类号： B01J3/00 ,  B01J19/00 ,  F25B9/00 ,  F25B1/06 ,  F25B31/00 ,  F25J1/00 ,  B23P15/00

    CPC分类号： F04D29/522 ,  F04D29/563 ,  F04D29/644 ,  Y10T29/49236

    摘要： Overhung axial compressor, chemical reactor and method for compressing a fluid. The overhung axial compressor includes a casing configured to be vertically split along a vertical axis for access to an inside of the casing and a removable cartridge. The removable cartridge is configured to fit inside the casing and to be detachably attached to the casing. The removable cartridge includes a shaft disposed along a horizontal axis, the shaft being configured to rotate about the horizontal axis, a bearing system attached to the removable cartridge and configured to rotationally support a first end of the shaft, and plural blades disposed toward a second end of the shaft such that the second end is overhung inside the casing. The compressor also includes a guide vane mechanism configured to connect to the removable cartridge, the guide vane mechanism being configured to adjust a flow of a fluid to the plural blades.

    摘要翻译： 悬臂式压缩机，化学反应器和压缩流体的方法。 悬臂轴向压缩机包括壳体，其构造成沿着垂直轴线垂直分开，以便进入壳体的内部和可拆卸的盒。 可拆卸的盒被配置为装配在壳体内部并且可拆卸地附接到壳体。 所述可移除筒包括沿着水平轴线设置的轴，所述轴被构造成围绕水平轴线旋转;轴承系统，其附接到所述可移除筒体并且构造成旋转地支撑所述轴的第一端;以及多个叶片， 轴的端部，使得第二端悬挂在壳体内。 所述压缩机还包括构造成连接到所述可移除筒的引导叶片机构，所述导叶机构构造成调节流体到所述多个叶片的流动。

    Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane
    82.
    发明申请
    Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane 有权
    具有用于能量转换机的小翼的引导叶片和用于转换能量的机器，所述能量包括导向叶片

    公开(公告)号：US20120269623A1

    公开(公告)日：2012-10-25

    申请号：US13516299

    申请日：2010-08-23

    申请人： Trevor Milne

    发明人： Trevor Milne

    IPC分类号： F01D9/00

    CPC分类号： F01D9/041 ,  F01D5/141 ,  F01D5/20 ,  F01D11/005 ,  F01D17/162 ,  F04D29/083 ,  F04D29/164 ,  F04D29/542 ,  F04D29/544 ,  F04D29/563 ,  F05D2240/12 ,  F05D2240/55

    摘要： An energy converting machine includes a guide vane. The guide vane includes a guide vane body for guiding a streaming fluid. The guide vane body has a pressure surface and a suction surface, a trailing edge and a leading edge, and a winglet for reducing leakage of the streaming fluid from the pressure surface to the suction surface. The winglet is arranged at a longitudinal end of the guide vane body. The winglet extents from the trailing edge to the leading edge and is arranged at the pressure surface. The winglet is free of protrusions beyond the leading edge and beyond the trailing edge.

    摘要翻译： 能量转换机包括导叶。 导向叶片包括用于引导流动流体的导向叶片主体。 导叶体具有压力表面和吸力表面，后缘和前缘，以及用于减少流动流体从压力表面到吸入表面的泄漏的小翼。 小翼布置在导叶体的纵向端部。 小翼从后缘延伸到前缘，并布置在压力表面。 小翼没有突出超出前缘并超出后缘。

    VARIABLE VANE FOR GAS TURBINE ENGINE
    83.
    发明申请
    VARIABLE VANE FOR GAS TURBINE ENGINE 有权
    用于气体涡轮发动机的变速箱

    公开(公告)号：US20120263571A1

    公开(公告)日：2012-10-18

    申请号：US13340983

    申请日：2011-12-30

    申请人： Robert A. Ress, JR.

    发明人： Robert A. Ress, JR.

    IPC分类号： F04D29/56

    CPC分类号： F04D29/563 ,  F01D17/14 ,  F01D17/162 ,  F05D2220/32 ,  F05D2240/12

    摘要： A turbomachine includes a variably positioned vane, an outer spindle integral with a vane outer button, where the vane is coupled to the vane outer button, an annular sleeve defining the spindle, where the annular sleeve contacts the vane outer button at a radially inward extent and contacts a turbine casing at a radially outward extent. The annular sleeve includes a wall portion having an aperture and the spindle extends through the aperture. A nut engages spindle threads, where the nut applies force to the wall portion toward the radially inward extent. An end of the spindle extends through the turbine casing, and a cantilever rotation actuator is coupled to the end of the spindle. A first bearing and second bearing engage the annular sleeve. A vane inner button is coupled to the vane, and a third bearing engages the vane inner button.

    摘要翻译： 涡轮机包括可变定位的叶片，与叶片外部按钮一体的外部心轴，其中叶片联接到叶片外部按钮，限定心轴的环形套筒，其中环形套筒以径向向内的程度接触叶片外部按钮 并且在径向向外的范围内接触涡轮机壳体。 环形套筒包括具有孔的壁部分，并且心轴延伸穿过孔。 螺母接合主轴螺纹，其中螺母朝向径向向内的程度向壁部施加力。 主轴的端部延伸穿过涡轮机壳体，并且悬臂旋转致动器联接到主轴的端部。 第一轴承和第二轴承接合环形套筒。 叶片内按钮联接到叶片，并且第三轴承接合叶片内按钮。

    CONTROL OF COMPRESSION SYSTEM WITH INDEPENDENTLY ACTUATED INLET GUIDE AND/OR STATOR VANES
    84.
    发明申请
    CONTROL OF COMPRESSION SYSTEM WITH INDEPENDENTLY ACTUATED INLET GUIDE AND/OR STATOR VANES 有权
    具有独立执行的入口指南和/或定期视窗的压缩系统的控制

    公开(公告)号：US20120259528A1

    公开(公告)日：2012-10-11

    申请号：US13083056

    申请日：2011-04-08

    申请人： Karl Dean Minto

    发明人： Karl Dean Minto

    IPC分类号： F02C9/00

    CPC分类号： F04D29/563 ,  F01D17/16 ,  F02C9/20 ,  F04D27/0246

    摘要： A compression system includes a compressor with adjustable inlet guide vanes (IGVs) and variable stator vanes (VSVs) that are adjustable independently of each other. IGV and VSV control units produce respective IGV and VSV reference commands responsive to respective first and second inputs that may be responsive to measured properties of the compression system. The second input may be provided by a model of the compressor or of the compression system responsive to measured properties. The second input may particularly be an estimate of a property not directly observable, such as stall margin or efficiency.

    摘要翻译： 压缩系统包括具有可调节入口导向叶片（IGV）的压缩机和可独立调节的可变定子叶片（VSV）。 IGV和VSV控制单元产生响应于相应的第一和第二输入的IGV和VSV参考命令，其可以响应于压缩系统的测量属性。 第二输入可以由压缩机或压缩系统的模型提供，以响应于测量的属性。 第二输入可以特别地是不能直接观察到的属性的估计，例如失速余量或效率。

    VARIABLE GEOMETRY VANE SYSTEM FOR GAS TURBINE ENGINES
    87.
    发明申请
    VARIABLE GEOMETRY VANE SYSTEM FOR GAS TURBINE ENGINES 有权
    用于气体涡轮发动机的可变几何风扇系统

    公开(公告)号：US20120171020A1

    公开(公告)日：2012-07-05

    申请号：US13339047

    申请日：2011-12-28

    申请人： Brian Peck ,  Edward Claude Rice

    发明人： Brian Peck ,  Edward Claude Rice

    IPC分类号： F04D29/56

    CPC分类号： F01D17/162 ,  F01D17/165 ,  F04D29/462 ,  F04D29/563

    摘要： One embodiment of the present invention is a unique variable geometry vane system. Another embodiment is a unique gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and turbomachinery variable geometry vane systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.

    摘要翻译： 本发明的一个实施例是独特的可变几何叶片系统。 另一个实施例是独特的燃气涡轮发动机。 其他实施例包括用于燃气涡轮发动机和涡轮机械可变几何叶片系统的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。

    SYSTEM AND METHOD FOR OPERATING A COMPRESSOR
    88.
    发明申请
    SYSTEM AND METHOD FOR OPERATING A COMPRESSOR 审中-公开
    压缩机操作的系统和方法

    公开(公告)号：US20120134783A1

    公开(公告)日：2012-05-31

    申请号：US12956461

    申请日：2010-11-30

    申请人： Dwight E. Davidson ,  Paul G. Delvernois

    发明人： Dwight E. Davidson ,  Paul G. Delvernois

    IPC分类号： F01D17/12

    CPC分类号： F04D27/002 ,  F04D27/0246 ,  F04D29/321 ,  F04D29/522 ,  F04D29/563

    摘要： A compressor includes a first stage of stator vanes having a first position and a second stage of stator vanes downstream from the first stage of stator vanes having a second position. A first actuator is engaged with the first stage of stator vanes, and a second actuator is engaged with the second stage of stator vanes. A method for operating a compressor includes adjusting a first position of a first plurality of stator vanes and adjusting a second position of a second plurality of stator vanes separately from the first position of the first plurality of stator vanes.

    摘要翻译： 压缩机包括具有第一位置的第一级定子叶片和具有第二位置的定子叶片的第一级下游的定子叶片的第二级。 第一致动器与定子叶片的第一级接合，第二致动器与定子叶片的第二级接合。 一种用于操作压缩机的方法包括调节第一多个定子叶片的第一位置并且与第一多个定子叶片的第一位置分开地调节第二多个定子叶片的第二位置。