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134 条记录 (耗时 0.032 秒)

    Conjugate screw rotor profile
    61.
    发明授权
    Conjugate screw rotor profile 失效
    共轭螺杆转子轮廓

    公开(公告)号：US6139299A

    公开(公告)日：2000-10-31

    申请号：US87576

    申请日：1998-05-29

    申请人： Keshava B. Kumar ,  James W. Bush

    发明人： Keshava B. Kumar ,  James W. Bush

    IPC分类号： F04C18/16 ,  F01C1/08 ,  F04C18/08 ,  F01C1/16

    CPC分类号： F01C1/084

    摘要： The point of tangency of the tip circle of the male rotor and the root circle of the female rotor is used as a starting point in generating the series of curves defining the male and female conjugate rotor profiles. The present invention provides: reduced viscous drag through the use of a departure angle; strengthened female lobes by controlling thickness along the pitch circle; opened root of male rotor to enhance manufacturability and tool life; a tortuous leakage path for gas traveling from a high pressure thread to a low pressure thread; better control of root diameter; and control of the pressure angle independently of the other variables.

    摘要翻译： 将阳转子的尖端圆和母转子的根圆的切线点用作产生限定公和母共轭转子轮廓的一系列曲线的起始点。 本发明提供：通过使用离开角减小粘性阻力; 通过控制节圆的厚度加强雌花瓣; 打开雄性转子根，提高生产性和刀具寿命; 用于从高压螺纹向低压螺纹行进的气体的曲折泄漏路径; 更好地控制根直径; 并独立于其他变量控制压力角。

    Scroll compressor with reverse offset at wrap tips
    62.
    发明授权
    Scroll compressor with reverse offset at wrap tips 失效
    涡旋压缩机在包装尖端具有反向偏移

    公开(公告)号：US6120268A

    公开(公告)日：2000-09-19

    申请号：US931702

    申请日：1997-09-16

    申请人： James W. Bush ,  Alexander Lifson

    发明人： James W. Bush ,  Alexander Lifson

    IPC分类号： F04C18/02 ,  F04C18/04

    CPC分类号： F04C18/0269

    摘要： An improved geometry for scroll wrap inner portion includes a groove which facilitates opening of the compression chambers to the discharge ports early in the cycle of the orbiting scroll. Stated one way, a forward end of the scroll wrap tip is thinner than a portion spaced from the forward end. A first curve defines the forwardmost end of said tip and extends to a forward ledge. A second circular curve is spaced from the forward ledge and extends to a rear ledge. An intermediate curve connects the forward and rear ledges. The rear curve is centered on a second radius, and if the second radius were extended beyond the rear ledge, the extension would move to a position spaced from the forward ledge and towards the opposed wrap. The swing radius for the scroll compressor wrap measured begins at the position wherein the forward ledge of one wrap faces the rear ledge of an opposed wrap begins on one side of zero, then crosses zero with an increasing scroll wrap, and then moves to an opposed side of zero. The inventive scroll compressor wrap achieves more rapid and smooth opening of the compression chambers to the discharge ports.

    摘要翻译： 用于涡旋包裹内部部分的改进的几何形状包括有利于在绕动涡盘的循环中早期将压缩室打开到排出口的凹槽。 以单向方式，涡旋包装尖端的前端比与前端间隔开的部分薄。 第一曲线限定所述尖端的最前端并且延伸到前凸缘。 第二圆形曲线与前凸缘间隔开并延伸到后凸缘。 中间曲线连接前方和后方。 后曲线以第二半径为中心，并且如果第二半径延伸超过后凸缘，则延伸部将移动到与前凸缘间隔开并朝向相对的卷边的位置。 涡旋压缩机外壳的摆动半径开始于其中一个涡卷的前凸缘面向相对的涡卷的后凸缘的位置在零的一侧开始的位置，然后与增加的涡卷卷绕成零，然后移动到相对的 一边为零。 本发明的涡旋压缩机涡卷实现了压缩室到排出口的更快速和平滑的打开。

    Piloted assembly
    65.
    发明授权
    Piloted assembly 失效
    导向装配

    公开(公告)号：US5869914A

    公开(公告)日：1999-02-09

    申请号：US957727

    申请日：1997-10-24

    申请人： David C. Baumann ,  James W. Bush

    发明人： David C. Baumann ,  James W. Bush

    IPC分类号： F04C29/00 ,  H02K5/16 ,  H02K15/02 ,  H02K15/14 ,  H02K15/16 ,  H02K5/00 ,  H02K5/10

    CPC分类号： H02K15/16 ,  Y10T29/49009 ,  Y10T29/49012

    摘要： Two housing members and the stator are precision machined on diameters and assembled such that the machined diameters coact to locate the members which then serve as a reference location for the subsequently assembled parts. The present invention reduces the number of critical machined features compared to a piloted assembly.

    摘要翻译： 两个外壳构件和定子通过直径进行精密加工并组装成使得加工的直径相互协调以定位构件，然后用作随后组装的部件的参考位置。 与引导组件相比，本发明减少了关键加工特征的数量。

    Rotary compressor with discharge chamber pressure relief groove
    66.
    发明授权
    Rotary compressor with discharge chamber pressure relief groove 失效
    带压力释放槽的旋转压缩机

    公开(公告)号：US5823755A

    公开(公告)日：1998-10-20

    申请号：US762372

    申请日：1996-12-09

    申请人： Francis P. Wilson ,  Andrea B. Dacosta ,  James W. Bush

    发明人： Francis P. Wilson ,  Andrea B. Dacosta ,  James W. Bush

    IPC分类号： F04C18/356 ,  F04C29/12

    CPC分类号： F04C29/12 ,  F04C18/3564

    摘要： The annular piston of a rolling piston compressor coacts with a groove in valving action such that the groove serves as a supplemental discharge flow area but gas therein is prevented from constituting part of the suction flow. The groove may be in the motor end bearing and/or pump end bearing and permits flow from the compression chamber to the interior of the piston which is in fluid communication with the interior of the shell while the compression chamber is undergoing discharge.

    摘要翻译： 滚动活塞式压缩机的环形活塞在阀动作中与槽共同作用，使得槽用作补充排出流动区域，但是其中的气体被阻止构成吸入流的一部分。 凹槽可以在马达端轴承和/或泵端轴承中，并且允许从压缩室流到活塞的内部，当压缩室正在经历放电时，其与壳体内部流体连通。

    Compressor end shell
    68.
    发明授权
    Compressor end shell 失效
    压缩机端壳

    公开(公告)号：US5391054A

    公开(公告)日：1995-02-21

    申请号：US912356

    申请日：1992-07-13

    申请人： James W. Bush

    发明人： James W. Bush

    IPC分类号： F04B39/00 ,  F04B39/12 ,  F04C23/00 ,  F01D25/24

    CPC分类号： F04B39/0033 ,  F04B39/121 ,  F04C23/008 ,  Y10S220/13 ,  Y10S417/902

    摘要： An end shell for a hermetic compressor is formed from a sheet of metal. When formed, the end shell has a spherical surface which extends for at least 230.degree. of the circumference of said end shell. If necessary or desired, a portion of up to 90.degree. of the circumference of said end shell can be formed as a cylindrical segment in order to provide a radial discharge or the like.

    摘要翻译： 用于密封式压缩机的端壳由一片金属制成。 当形成时，端壳具有球形表面，其延伸至所述端壳的圆周的至少230°。 如果需要或需要，可以将所述端壳的圆周高达90°的部分形成为圆柱形部分，以便提供径向放电等。