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公开(公告)号：US07452187B2
公开(公告)日：2008-11-18
申请号：US11199255
申请日：2005-08-09
IPC分类号： F04D29/26
CPC分类号： F04D29/284 , F04D29/30
摘要： A compressor having a defined large diameter impeller having an integral shroud and having a three dimensional gas flow path defined by the impeller hub surface, blades and the shroud and having a large axially oriented inlet or inducer section with aggressive inducer blades, a defined outlet section geometry, and continuous blade geometries between the inlet and outlet sections.
摘要翻译： 具有限定的大直径叶轮的压缩机具有整体式护罩并且具有由叶轮毂表面，叶片和护罩限定的三维气体流动通道，并且具有大的轴向定向的入口或诱导部分，具有积极的诱导叶片，限定的出口部分 几何形状和连续的叶片几何形状。
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公开(公告)号：US07448852B2
公开(公告)日：2008-11-11
申请号：US11199254
申请日：2005-08-09
IPC分类号： F04D29/44
CPC分类号： F04D29/444 , F05D2250/52
摘要： A low solidity vaned airfoil diffuser for a centrifugal compressor wherein each blade has a lean angle greater than zero and wherein the hub stagger angle may be the same as or may be different from the shroud stagger angle for each blade.
摘要翻译： 用于离心式压缩机的低坚固翼型翼型扩散器，其中每个叶片具有大于零的倾斜角，并且其中轮毂交错角度可以与每个叶片的护罩交错角度相同或可以不同。
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公开(公告)号：US08016557B2
公开(公告)日：2011-09-13
申请号：US11903592
申请日：2007-09-24
申请人： Ahmed Abdelwahab , Gordon J. Gerber
发明人： Ahmed Abdelwahab , Gordon J. Gerber
IPC分类号： F04D29/44
CPC分类号： F04D29/444 , F05D2250/52
摘要： An airfoil diffuser for a centrifugal compressor formed by a diffuser passage area and a plurality of diffuser blades located within the diffuser passage area. The diffuser passage area is defined between a hub plate and a shroud of the centrifugal compressor. Each of the diffuser blades has a twisted configuration in a stacking direction as taken between the hub plate and an outer portion of the shroud located opposite to the hub plate. As a result of the twisted configuration, the diffuser blade inlet blade angle decreases from the hub plate to the outer portion of the shroud and solidity measurements at leading edges of the diffuser plates vary between a lower solidity value measured at the hub plate of less than 1.0 and a high solidity value measured at the outer portion of the shroud of no less than 1.0.
摘要翻译： 用于由扩散器通道区域形成的离心式压缩机的翼型扩散器和位于扩散器通道区域内的多个扩散器叶片。 扩散器通道区域限定在离心式压缩机的轮毂板和护罩之间。 每个扩散器叶片在层叠方向之间具有捻合构造，其在轮毂板和位于与毂板相对的罩的外部之间。 作为扭曲结构的结果，扩散器叶片入口叶片角度从轮毂板到护罩的外部部分减小，并且扩散器板的前缘处的坚固性测量在毂板处测量的较低的固体值小于 1.0，并且在护罩的外部部分测量的高坚固度值不小于1.0。
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4.发明授权Systems and methods for gas separation using high-speed permanent magnet motors with centrifugal compressors 有权使用带离心式压缩机的高速永磁电机进行气体分离的系统和方法公开(公告)号：US07785405B2
公开(公告)日：2010-08-31
申请号：US12056887
申请日：2008-03-27
IPC分类号： B01D53/047 , F04D27/00
CPC分类号： B01D53/047 , B01D53/0446 , B01D53/0476 , B01D53/053 , B01D2256/12 , B01D2257/102 , F04D25/06 , F04D25/16 , F04D27/0261
摘要： Systems and processes are provided for gas separation using high-speed permanent magnet variable-speed motors to accelerate and decelerate centrifugal compressors suitable for use in pressure swing adsorption (PSA) or vacuum pressure swing adsorption (VPSA) processes.
摘要翻译： 提供使用高速永磁变速电机进行气体分离的系统和工艺，以加速和减速适用于变压吸附（PSA）或真空变压吸附（VPSA）工艺的离心式压缩机。
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5.发明申请SYSTEMS AND METHODS FOR GAS SEPARATION USING HIGH-SPEED PERMANENT MAGNET MOTORS WITH CENTRIFUGAL COMPRESSORS 有权使用高速永磁电机与离心压缩机进行气体分离的系统和方法公开(公告)号：US20090241771A1
公开(公告)日：2009-10-01
申请号：US12056887
申请日：2008-03-27
IPC分类号： B01D53/047 , B01D46/46 , B01D45/12
CPC分类号： B01D53/047 , B01D53/0446 , B01D53/0476 , B01D53/053 , B01D2256/12 , B01D2257/102 , F04D25/06 , F04D25/16 , F04D27/0261
摘要： Systems and processes are provided for gas separation using high-speed permanent magnet variable-speed motors to accelerate and decelerate centrifugal compressors suitable for use in pressure swing adsorption (PSA) or vacuum pressure swing adsorption (VPSA) processes.
摘要翻译： 提供使用高速永磁变速电机进行气体分离的系统和工艺，以加速和减速适用于变压吸附（PSA）或真空变压吸附（VPSA）工艺的离心式压缩机。
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公开(公告)号：US20080038114A1
公开(公告)日：2008-02-14
申请号：US11903592
申请日：2007-09-24
申请人： Ahmed Abdelwahab , Robert Baker , Gordon Gerber
发明人： Ahmed Abdelwahab , Robert Baker , Gordon Gerber
IPC分类号： F04D29/44
CPC分类号： F04D29/444 , F05D2250/52
摘要： An airfoil diffuser for a centrifugal compressor formed by a diffuser passage area and a plurality of diffuser blades located within the diffuser passage area. The diffuser passage area is defined between a hub plate and a shroud of the centrifugal compressor. Each of the diffuser blades has a twisted configuration in a stacking direction as taken between the hub plate and an outer portion of the shroud located opposite to the hub plate. As a result of the twisted configuration, the diffuser blade inlet blade angle decreases from the hub plate to the outer portion of the shroud and solidity measurements at leading edges of the diffuser plates vary between a lower solidity value measured at the hub plate of less than 1.0 and a high solidity value measured at the outer portion of the shroud of no less than 1.0.
摘要翻译： 用于由扩散器通道区域形成的离心式压缩机的翼型扩散器和位于扩散器通道区域内的多个扩散器叶片。 扩散器通道区域限定在离心式压缩机的轮毂板和护罩之间。 每个扩散器叶片在层叠方向之间具有捻合构造，其在轮毂板和位于与毂板相对的罩的外部之间。 作为扭曲结构的结果，扩散器叶片入口叶片角度从轮毂板到护罩的外部部分减小，并且扩散器板的前缘处的坚固性测量在毂板处测量的较低的固体值小于 1.0，并且在护罩的外部部分测量的高坚固度值不小于1.0。
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公开(公告)号：US20070036647A1
公开(公告)日：2007-02-15
申请号：US11199254
申请日：2005-08-09
申请人： Ahmed Abdelwahab , Robert Baker , Gordon Gerber
发明人： Ahmed Abdelwahab , Robert Baker , Gordon Gerber
IPC分类号： F01D9/00
CPC分类号： F04D29/444 , F05D2250/52
摘要： A low solidity vaned airfoil diffuser for a centrifugal compressor wherein each blade has a lean angle greater than zero and wherein the hub stagger angle may be the same as or may be different from the shroud stagger angle for each blade.
摘要翻译： 用于离心式压缩机的低坚固翼型翼型扩散器，其中每个叶片具有大于零的倾斜角，并且其中轮毂交错角度可以与每个叶片的护罩交错角度相同或可以不同。
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公开(公告)号：US20070036645A1
公开(公告)日：2007-02-15
申请号：US11199255
申请日：2005-08-09
申请人： Robert Baker , Ahmed Abdelwahab , Gordon Gerber
发明人： Robert Baker , Ahmed Abdelwahab , Gordon Gerber
IPC分类号： F04D29/44
CPC分类号： F04D29/284 , F04D29/30
摘要： A compressor having a defined large diameter impeller having an integral shroud and having a three dimensional gas flow path defined by the impeller hub surface, blades and the shroud and having a large axially oriented inlet or inducer section with aggressive inducer blades, a defined outlet section geometry, and continuous blade geometries between the inlet and outlet sections.
摘要翻译： 具有限定的大直径叶轮的压缩机具有整体式护罩并且具有由叶轮毂表面，叶片和护罩限定的三维气体流动通道，并且具有大的轴向定向的入口或诱导部分，具有积极的诱导叶片，限定的出口部分 几何形状和连续的叶片几何形状。
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9.发明授权Method and apparatus for filling a pressure vessel having application to vehicle fueling 有权用于填充应用于车辆加油的压力容器的方法和装置公开(公告)号：US06792981B1
公开(公告)日：2004-09-21
申请号：US10409130
申请日：2003-04-09
IPC分类号： B65B3100
CPC分类号： F17C5/06 , F17C2201/0104 , F17C2201/054 , F17C2205/0326 , F17C2205/0335 , F17C2221/012 , F17C2223/0123 , F17C2223/036 , F17C2227/0135 , F17C2227/0164 , F17C2227/043 , F17C2250/032 , F17C2250/043 , F17C2250/0626 , F17C2250/0636 , F17C2260/025 , F17C2270/0168 , Y02E60/321
摘要： A method and apparatus for introducing a compressed gas into a pressure vessel, for instance, hydrogen into a vehicle fuel tank, in which hydrogen is compressed in an initial and final compressions stages which can be powered by a common source. The initial compression stage can continually operate to compress the gas in a lower pressure storage bank during the time that hydrogen is dispensed to a vehicle fuel tank. In time periods between dispensing, the gas from the lower pressure stage and from the lower pressure storage bank is compressed in the final compression stage and stored in a higher pressure storage bank. When the pressure vessel is to be filled, the compressor compresses the gas from the higher pressure storage bank to fill the vessel.
摘要翻译： 一种用于将压缩气体引入压力容器中的方法和装置，例如氢气进入车辆燃料箱，其中在初始和最终的压缩阶段压缩氢气，该压缩阶段可以由公共源供电。 在将氢气分配到车辆燃料箱的时间期间，初始压缩阶段可以连续地操作以压缩较低压力储存库中的气体。 在分配之间的时间段中，来自较低压力级的气体和来自较低压力储存室的气体在最终压缩阶段被压缩并且储存在较高压力的储存库中。 当压力容器被填充时，压缩机压缩来自高压储存库的气体以填充容器。
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