Skinning of progressive cavity apparatus
    1.
    发明授权
    Skinning of progressive cavity apparatus 有权
    渐进式腔体装置的剥皮

    公开(公告)号:US08337182B2

    公开(公告)日:2012-12-25

    申请号:US11542052

    申请日:2006-10-03

    摘要: A skinned rotor 201 or skinned stator 305 of a progressive cavity apparatus is described. A rotor 201 can be skinned by threading a sleeve 210 with a profiled helical outer 212 and profiled helical inner 214 surface onto a core 202 with a profiled helical outer surface 204. A rotor (1301, 1401) can also be skinned by inserting a non-helical core (1302, 1402) into a non-helical longitudinal bore (1314, 1414) of a sleeve (1310, 1410) with a profiled helical outer surface (1312, 1412). A stator 305 can be skinned by threading a tubular liner 310 with profiled helical inner 314 and profiled helical outer 312 surfaces into a profiled helical bore 308 of a tube 306. A stator (2405, 2505) can also be skinned by inserting a tubular liner (2410, 2510) with a non-helical outer surface (2412, 2512) into a non-helical bore (2408, 2508) of a tube (2406, 2506).

    摘要翻译: 描述了渐进式腔体装置的皮肤转子201或皮肤定子305。 转子201可以通过将具有异型螺旋形外壳212和成型螺旋形内部214表面的套筒210穿过具有成型螺旋形外表面204的芯体202而被剥皮。转子(1301,1401)也可以通过插入非转子 螺旋形芯(1302,1402)转换成具有异型螺旋形外表面(1312,1412)的套筒(1310,1410)的非螺旋形纵向孔(1314,1414)。 可以通过将具有异型螺旋内部314的管状衬垫310和成型的螺旋形外部312表面螺纹连接到管306的成型螺旋孔308中来将定子305剥皮。定子(2405,2505)也可以通过插入管状衬垫 (2410,2510),其具有非螺旋形外表面(2412,2512)到管(2406,2506)的非螺旋孔(2408,2508)中。

    Skinning of progressive cavity apparatus
    2.
    发明申请
    Skinning of progressive cavity apparatus 有权
    渐进式腔体装置的剥皮

    公开(公告)号:US20090016893A1

    公开(公告)日:2009-01-15

    申请号:US11542052

    申请日:2006-10-03

    IPC分类号: F03B3/12

    摘要: A skinned rotor 201 or skinned stator 305 of a progressive cavity apparatus is described. A rotor 201 can be skinned by threading a sleeve 210 with a profiled helical outer 212 and profiled helical inner 214 surface onto a core 202 with a profiled helical outer surface 204. A rotor (1301, 1401) can also be skinned by inserting a non-helical core (1302, 1402) into a non-helical longitudinal bore (1314, 1414) of a sleeve (1310, 1410) with a profiled helical outer surface (1312, 1412). A stator 305 can be skinned by threading a tubular liner 310 with profiled helical inner 314 and profiled helical outer 312 surfaces into a profiled helical bore 308 of a tube 306. A stator (2405, 2505) can also be skinned by inserting a tubular liner (2410, 2510) with a non-helical outer surface (2412, 2512) into a non-helical bore (2408, 2508) of a tube (2406, 2506).

    摘要翻译: 描述了渐进式腔体装置的皮肤转子201或皮肤定子305。 转子201可以通过将具有异型螺旋形外壳212和成型螺旋形内部214表面的套筒210穿过具有成型螺旋形外表面204的芯体202而被剥皮。转子(1301,1401)也可以通过插入非转子 螺旋形芯(1302,1402)转换成具有异型螺旋形外表面(1312,1412)的套筒(1310,1410)的非螺旋形纵向孔(1314,1414)。 可以通过将具有异型螺旋内部314的管状衬垫310和成型的螺旋形外部312表面螺纹连接到管306的成型螺旋孔308中来将定子305剥皮。定子(2405,2505)也可以通过插入管状衬垫 (2410,2510),其具有非螺旋形外表面(2412,2512)到管(2406,2506)的非螺旋孔(2408,2508)中。

    ROTOR OF PROGRESSIVE CAVITY APPRATUS AND METHOD OF FORMING
    3.
    发明申请
    ROTOR OF PROGRESSIVE CAVITY APPRATUS AND METHOD OF FORMING 有权
    渐进式转杯装置的转子及其形成方法

    公开(公告)号:US20080264593A1

    公开(公告)日:2008-10-30

    申请号:US11740978

    申请日:2007-04-27

    IPC分类号: B22D19/00 B22D25/02 F04C29/00

    CPC分类号: F04C2/1075 F04C2230/27

    摘要: Cast material rotor (200,300,500,800) with profiled helical outer surface (208,308,508,808). Cast material layer (502,802) can be disposed between core (504,804) and tube (506,806). Profiled helical outer surface (208,308) can be in tube 206 or cast material layer 302, respectively. Method of forming rotor 200 can include filling void between outer surface 212 of core 204 and longitudinal bore 210 of tube 206 having profiled helical outer surface 208 with cast material 202 in fluid state, and solidifying cast material 202. Tube 206 can be disposed within profiled helical bore 714 of mold 700, e.g., before solidifying cast material 202. Method of forming rotor 300 can include filling void between outer surface 312 of core 304 and profiled helical bore 714 in mold 700 with cast material 302 in fluid state, solidifying cast material 302 to impart profiled helical outer surface 308 thereto, and removing mold 700 from cast material 302.

    摘要翻译: 铸造材料转子(200,300,500,800),具有异型螺旋形外表面(208,308,508,808)。 铸造材料层(502,802)可以设置在芯(504,804)和管(506,806)之间。 分形螺旋形外表面(208,308)可以分别在管206或铸造材料层302中。 形成转子200的方法可以包括在芯体204的外表面212和管206的纵向孔210之间的填充空隙,其具有异型螺旋形外表面208,铸造材料202处于流体状态,并且固化铸造材料202。 管206可以设置在模具700的成型螺旋孔714内,例如在固化铸造材料202之前。 形成转子300的方法可以包括在芯304的外表面312和模具700中的成型螺旋孔714之间填充空隙,铸造材料302处于流体状态,固化铸造材料302以赋予成型的螺旋形外表面308,并且将模具700从 铸造材料302。

    Rotor of progressive cavity apparatus and method of forming
    4.
    发明授权
    Rotor of progressive cavity apparatus and method of forming 有权
    渐进式腔体转子和成型方法

    公开(公告)号:US08257633B2

    公开(公告)日:2012-09-04

    申请号:US11740978

    申请日:2007-04-27

    IPC分类号: B22D19/00

    CPC分类号: F04C2/1075 F04C2230/27

    摘要: Cast material rotor (200,300,500,800) with profiled helical outer surface (208,308,508,808). Cast material layer (502,802) can be disposed between core (504,804) and tube (506,806). Profiled helical outer surface (208,308) can be in tube 206 or cast material layer 302, respectively. Method of forming rotor 200 can include filling void between outer surface 212 of core 204 and longitudinal bore 210 of tube 206 having profiled helical outer surface 208 with cast material 202 in fluid state, and solidifying cast material 202. Tube 206 can be disposed within profiled helical bore 714 of mold 700, e.g., before solidifying cast material 202. Method of forming rotor 300 can include filling void between outer surface 312 of core 304 and profiled helical bore 714 in mold 700 with cast material 302 in fluid state, solidifying cast material 302 to impart profiled helical outer surface 308 thereto, and removing mold 700 from cast material 302.

    摘要翻译: 铸造材料转子(200,300,500,800),具有异型螺旋形外表面(208,308,508,808)。 铸造材料层(502,802)可以设置在芯(504,804)和管(506,806)之间。 分形螺旋形外表面(208,308)可以分别在管206或铸造材料层302中。 形成转子200的方法可以包括在芯体204的外表面212和管206的纵向孔210之间的填充空隙,其具有异型螺旋形外表面208,铸造材料202处于流体状态,并且固化铸造材料202.管206可以设置在型材 模具700的螺旋孔714,例如在固化铸造材料202之前。形成转子300的方法可以包括在芯304的外表面312和模具700中的成型螺旋孔714之间填充空隙,铸造材料302处于流体状态,固化铸造材料 302以赋予轮廓螺旋形外表面308,并且从铸造材料302移除模具700。

    Method of fabricating a high temperature progressive cavity motor or pump component
    7.
    发明授权
    Method of fabricating a high temperature progressive cavity motor or pump component 有权
    制造高温渐进式电机或泵组件的方法

    公开(公告)号:US08444901B2

    公开(公告)日:2013-05-21

    申请号:US11967985

    申请日:2007-12-31

    摘要: The present application discloses a progressive cavity motor or pump component, either stator or rotor, which provides a high glass transition temperature polymeric surface on the component which becomes resilient at or below the expected operating temperature of the motor or pump, but which remains solid at ambient temperatures, along with a method of fabricating either a stator or a rotor with such surface characteristics. Since the surface becomes resilient, the progressive cavity pump operates efficiently at temperatures above the glass transition temperature of the selected polymeric surface.

    摘要翻译: 本申请公开了一种渐进腔电动机或泵组件,定子或转子,其在部件上提供高玻璃化转变温度聚合物表面,其在等于或低于电动机或泵的预期操作温度下变得弹性,但是在 环境温度以及制造具有这种表面特性的定子或转子的方法。 由于表面变得弹性,所以渐进式空腔泵在高于选定聚合物表面的玻璃化转变温度的温度下有效地工作。

    Manufacturing method for high temperature fiber optic accelerometer
    8.
    发明授权
    Manufacturing method for high temperature fiber optic accelerometer 有权
    高温光纤加速度计的制造方法

    公开(公告)号:US07155101B2

    公开(公告)日:2006-12-26

    申请号:US10843097

    申请日:2004-05-11

    IPC分类号: G02B6/00 G02B6/36 G01P15/00

    CPC分类号: G01P15/093 G02B6/14

    摘要: A method of making a fiber optic accelerometer includes (a) drawing an optical fiber through a resin; (b) winding the resin coated fiber onto a disc mounted on an assembly having a central shaft; and (c) curing the resin-coated fiber. The optical fiber may be drawn through a resin by providing a container filled with a resin having an orifice therethrough and drawing the fiber through the orifice. The resin may be cured such that the fiber is bonded to the disc by curing the resin to the fiber and the disc at the same time.

    摘要翻译: 制造光纤加速度计的方法包括:(a)通过树脂拉制光纤; (b)将树脂涂覆的纤维卷绕到安装在具有中心轴的组件上的盘上; 和(c)固化树脂被覆纤维。 通过提供填充有具有孔口的树脂的容器并通过孔口拉出纤维,可以将光纤拉伸通过树脂。 树脂可以被固化,使得纤维通过将树脂固化到纤维和盘同时粘合到盘上。