Variable Geometry Supersonic Compressor
    23.
    发明公开

    公开(公告)号:US20240229804A1

    公开(公告)日:2024-07-11

    申请号:US18447852

    申请日:2023-08-10

    发明人: Shawn P. LAWLOR

    摘要: A counter-rotating supersonic compressor. A first subsonic rotor includes a plurality of unshrouded impulse rotor blades operating at sub-sonic conditions. A second, supersonic rotor includes a fixed second rotor portion and an adjustable second rotor portion. The fixed second rotor portion includes a plurality of supersonic passageways having converging-diverging sidewalls, and internal boundary layer bleed passageways. The adjustable second rotor portion includes a plurality of centerbodies which are disposed in the supersonic passageways. Helical movement (circumferential and axial) movement of the adjustable second rotor portion with respect to the fixed second rotor portion enables upstream and downstream movement of the centerbodies in the supersonic passageways. This movement facilitates ease of supersonic startup, and automatic adjustment for changes in operation conditions, such as pressure, temperature, or mass flow rate of a working fluid such as carbon dioxide.

    Supersonic compressor rotor
    24.
    发明授权
    Supersonic compressor rotor 有权
    超音速压缩机转子

    公开(公告)号:US09103345B2

    公开(公告)日:2015-08-11

    申请号:US12639036

    申请日:2009-12-16

    摘要: Provided is a supersonic compressor having a supersonic compressor rotor including a clockable rotor disk allowing restriction or opening of portions of a fluid flow channel of the rotor in order to enhance performance of the rotor during different operational stages, for example rotor start-up or steady state. The supersonic compressor has a first rotor disk, a second rotor disk and a third rotor disk which share a common axis of rotation. The first and second rotor disks are rotatably coupled, and the third rotor disk is disposed between them. The third rotor disk is independently rotatable relative to the first and second disks, and has a raised surface structure for restricting or opening a portion of the flow channel defined by the three rotor disks and at least two vanes. The flow channel contains a supersonic compression ramp and encompasses the raised surface structure.

    摘要翻译: 提供了一种超音速压缩机,其具有超音速压缩机转子,其包括可调节转子盘,其允许限制或打开转子的流体流动通道的部分,以便在不同的操作阶段期间增强转子的性能,例如转子启动或稳定 州。 超音速压缩机具有第一转子盘,第二转子盘和共享公共旋转轴的第三转子盘。 第一和第二转子盘可旋转地连接,第三转子盘设置在它们之间。 第三转子盘相对于第一和第二盘独立地可旋转,并且具有用于限制或打开由三个转子盘和至少两个叶片限定的流动通道的一部分的凸起表面结构。 流动通道包含超音速压缩斜坡并且包括凸起的表面结构。

    Supersonic compressor comprising radial flow path
    25.
    发明授权
    Supersonic compressor comprising radial flow path 有权
    超音速压缩机包括径向流动路径

    公开(公告)号:US09097258B2

    公开(公告)日:2015-08-04

    申请号:US12491602

    申请日:2009-06-25

    摘要: The present invention provides novel supersonic compressors comprising novel supersonic compressor rotors. The supersonic compressor rotors are designed to operate at very high rotational speed wherein the velocity of the gas entering the supersonic compressor rotor is greater than the local speed of sound in the gas, hence the descriptor “supersonic”. The new supersonic compressors comprise at least one supersonic compressor rotor defining an inner cylindrical cavity and an outer rotor rim and at least one radial flow channel allowing fluid communication between the inner cylindrical cavity and the outer rotor rim, said radial flow channel comprising a supersonic compression ramp. The novel supersonic compressor rotors are expected to enhance the performance of supersonic compressors comprising them, and to provide for greater design versatility in systems comprising such novel supersonic compressors.

    摘要翻译: 本发明提供了包含新型超音速压缩机转子的新型超音速压缩机。 超音速压缩机转子设计成以非常高的转速工作,其中进入超音速压缩机转子的气体的速度大于气体中局部的声速,因此描述了“超音速”。 新的超音速压缩机包括至少一个超音速压缩机转子,其限定内圆柱形空腔和外转子边缘以及至少一个径向流动通道,其允许内圆柱形空腔和外转子轮缘之间的流体连通,所述径向流动通道包括超音速压缩 斜坡 期望新颖的超音速压缩机转子增强包括它们的超音速压缩机的性能,并且在包括这种新型超音速压缩机的系统中提供更大的设计通用性。

    Multi-stage centrifugal fan
    26.
    发明授权
    Multi-stage centrifugal fan 有权
    多级离心风机

    公开(公告)号:US08734087B2

    公开(公告)日:2014-05-27

    申请号:US12824905

    申请日:2010-06-28

    申请人: David G. Converse

    发明人: David G. Converse

    IPC分类号: F04D17/12 F04D29/24

    摘要: A multi-stage centrifugal fan is provided and includes first and second stages of a rotor having substantially axially aligned rotor vanes formed to impart energy to a fluid moving in an outward radial direction when the first and second stages of the rotor rotate about a centerline and a stator having stator vanes radially interposed between and substantially axially aligned with the first and second stage rotor vanes.

    摘要翻译: 提供多级离心式风扇,其包括转子的第一级和第二级,该转子具有基本上轴向对齐的转子叶片,其形成为当转子的第一和第二级绕中心线旋转时向沿径向方向移动的流体赋予能量, 定子,其具有径向插入在第一和第二级转子叶片之间且基本上轴向对齐的定子叶片。

    SUPERSONIC COMPRESSOR COMPRISING RADIAL FLOW PATH
    27.
    发明申请
    SUPERSONIC COMPRESSOR COMPRISING RADIAL FLOW PATH 有权
    包括径向流动路径的超级压缩机

    公开(公告)号:US20100329856A1

    公开(公告)日:2010-12-30

    申请号:US12491602

    申请日:2009-06-25

    IPC分类号: F04D21/00 F04D29/28 F04D29/44

    摘要: The present invention provides novel supersonic compressors comprising novel supersonic compressor rotors. The supersonic compressor rotors are designed to operate at very high rotational speed wherein the velocity of the gas entering the supersonic compressor rotor is greater than the local speed of sound in the gas, hence the descriptor “supersonic”. The new supersonic compressors comprise at least one supersonic compressor rotor defining an inner cylindrical cavity and an outer rotor rim and at least one radial flow channel allowing fluid communication between the inner cylindrical cavity and the outer rotor rim, said radial flow channel comprising a supersonic compression ramp. The novel supersonic compressor rotors are expected to enhance the performance of supersonic compressors comprising them, and to provide for greater design versatility in systems comprising such novel supersonic compressors.

    摘要翻译: 本发明提供了包含新型超音速压缩机转子的新型超音速压缩机。 超音速压缩机转子设计成以非常高的转速工作,其中进入超音速压缩机转子的气体的速度大于气体中局部的声速,因此描述了“超音速”。 新的超音速压缩机包括至少一个超音速压缩机转子,其限定内圆柱形空腔和外转子边缘以及至少一个径向流动通道,其允许内圆柱形空腔和外转子轮缘之间的流体连通,所述径向流动通道包括超音速压缩 斜坡 期望新颖的超音速压缩机转子增强包括它们的超音速压缩机的性能,并且在包括这种新型超音速压缩机的系统中提供更大的设计通用性。

    Multi-stage air movers for cooling computer systems and for other uses
    28.
    发明申请
    Multi-stage air movers for cooling computer systems and for other uses 有权
    用于冷却计算机系统和其他用途的多级升降机

    公开(公告)号:US20070211428A1

    公开(公告)日:2007-09-13

    申请号:US11371272

    申请日:2006-03-08

    申请人: Wade Doll

    发明人: Wade Doll

    IPC分类号: H05K7/20

    摘要: Multi-stage air movers for cooling computers and other systems are described herein. In one embodiment, a computer system includes a computer cabinet holding a plurality of computer modules. The computer cabinet includes an air inlet and an air outlet. The computer system further includes a multi-stage air mover configured to move a flow of cooling air from the air inlet, past the plurality of computer modules, and out the computer cabinet via the air outlet.

    摘要翻译: 这里描述了用于冷却计算机和其他系统的多级升空机。 在一个实施例中,计算机系统包括容纳多个计算机模块的计算机机箱。 计算机机柜包括进气口和出气口。 计算机系统还包括多级鼓风机,其被构造成使来自空气入口的冷却空气流经过多个计算机模块,并经由空气出口从计算机机箱移出。

    Friction vacuum pump
    29.
    发明授权
    Friction vacuum pump 失效
    摩擦真空泵

    公开(公告)号:US07011491B2

    公开(公告)日:2006-03-14

    申请号:US10182843

    申请日:2001-01-24

    IPC分类号: F01D1/36

    CPC分类号: F04D17/127 F04D17/168

    摘要: A friction vacuum pump (1) comprises a fixed element (7) bearing rows of stator blades (3) and a rotating element (6) bearing rows of rotor blades (2). The rows of stator blades and rotor blades are arranged concentrically with respect to an axis of rotation (4) of the rotating element (6) and mesh with each other. In order to create in the axial direct a short friction pump, the elements (6, 7) bearing the rows of rotor blades and stator blades extend in a substantially radial manner and the longitudinal axes of the blades (2, 3) extend in a substantially axial manner.

    摘要翻译: 摩擦真空泵(1)包括承载排定子叶片(3)的固定元件(7)和支承转子叶片(2)的转动元件(6)。 定子叶片和转子叶片的排相对于旋转元件(6)的旋转轴线(4)同心地布置并彼此啮合。 为了在轴向直接形成短的摩擦泵,承载转子叶片和定子叶片的行的元件(6,7)以基本上径向的方式延伸,并且叶片(2,3)的纵向轴线以 基本轴向。

    Blower with a plurality of impellers
    30.
    发明申请
    Blower with a plurality of impellers 有权
    鼓风机配有多个叶轮

    公开(公告)号:US20040101399A1

    公开(公告)日:2004-05-27

    申请号:US10348907

    申请日:2003-01-23

    IPC分类号: F01D001/24

    CPC分类号: F04D17/127

    摘要: A blower having a plurality of impellers is described. The blower has two driving devices and two impellers respectively mounted on the two driving devices. The blades of the two impellers, which are radially or axially disposed, are overlapped so as to enhance the heat-dissipating efficiency of the blower.

    摘要翻译: 描述具有多个叶轮的鼓风机。 鼓风机具有分别安装在两个驱动装置上的两个驱动装置和两个叶轮。 径向或轴向设置的两个叶轮的叶片重叠,以提高鼓风机的散热效率。