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1.发明申请ROTARY COMPRESSOR-EXPANDER SYSTEMS AND ASSOCIATED METHODS OF USE AND MANUFACTURE, INCLUDING INTEGRAL HEAT EXCHANGER SYSTEMS 有权旋转压缩机 - 膨胀机系统及相关使用和制造方法，包括整体热交换器系统公开(公告)号：US20110209477A1
公开(公告)日：2011-09-01
申请号：US13038360
申请日：2011-03-01
IPC分类号： F01C13/00
CPC分类号： F01C1/22 , F01C11/002 , F01C21/06 , Y02T10/16 , Y10T29/49245
摘要： The present technology is directed generally to rotary displacement systems and associated methods of use and manufacture. The systems can be used to compress and/or expand compressible fluids. In some embodiments, the rotary displacement systems include a chamber housing having a pressure-modifying chamber with a first port and a second port, a first passageway in fluid communication with the chamber via the first port, and a second passageway in fluid communication with the chamber via the second port. The systems can further include a shaft positioned within the chamber housing and rotatable relative to the chamber housing about a rotational axis, and a rotor comprising no more than two lobes. The rotor can be carried by and rotatable relative to the shaft, and can be alternately operable in a first mode in which flow is provided from the first passageway to the second passageway via the chamber and in a second mode in which flow is provided from the second passageway to the first passageway via the chamber.
摘要翻译： 本技术主要针对旋转位移系统和相关的使用和制造方法。 该系统可用于压缩和/或膨胀可压缩流体。 在一些实施例中，旋转位移系统包括具有第一端口和第二端口的压力调节室的腔室壳体，经由第一端口与腔室流体连通的第一通道，以及与腔室流体连通的第二通道， 通过第二个端口。 所述系统还可以包括定位在腔室壳体内并且围绕旋转轴线相对于腔室壳体可旋转的轴，以及包括不超过两个叶片的转子。 转子可以相对于轴承载并可转动，并且可以在第一模式中交替地操作，在第一模式中，第一模式从第一通道到第二通道经由室被提供，并且在第二模式中， 经由腔室到达第一通道的第二通道。
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2.发明申请ROTARY COMPRESSOR-EXPANDER SYSTEMS AND ASSOCIATED METHODS OF USE AND MANUFACTURE, INCLUDING TWO-LOBED ROTOR SYSTEMS 审中-公开旋转式压缩机 - 膨胀机系统及相关的使用和制造方法，包括两轴转子系统公开(公告)号：US20110217197A1
公开(公告)日：2011-09-08
申请号：US13038358
申请日：2011-03-01
CPC分类号： F01C1/22 , F01C11/002 , F01C21/06 , Y02T10/16 , Y10T29/49245
摘要： The present technology is directed generally to rotary displacement systems and associated methods of use and manufacture. The systems can be used to compress and/or expand compressible fluids. In some embodiments, the rotary displacement systems include a chamber housing having a pressure-modifying chamber with a first port and a second port, a first passageway in fluid communication with the chamber via the first port, and a second passageway in fluid communication with the chamber via the second port. The systems can further include a shaft positioned within the chamber housing and rotatable relative to the chamber housing about a rotational axis, and a rotor comprising no more than two lobes. The rotor can be carried by and rotatable relative to the shaft, and can be alternately operable in a first mode in which flow is provided from the first passageway to the second passageway via the chamber and in a second mode in which flow is provided from the second passageway to the first passageway via the chamber.
摘要翻译： 本技术主要针对旋转位移系统和相关的使用和制造方法。 该系统可用于压缩和/或膨胀可压缩流体。 在一些实施例中，旋转位移系统包括具有第一端口和第二端口的压力调节室的腔室壳体，经由第一端口与腔室流体连通的第一通道，以及与腔室流体连通的第二通道， 通过第二个端口。 所述系统还可以包括定位在腔室壳体内并且围绕旋转轴线相对于腔室壳体可旋转的轴，以及包括不超过两个叶片的转子。 转子可以相对于轴承载并可转动，并且可以在第一模式中交替地操作，在第一模式中，第一模式从第一通道到第二通道经由室被提供，并且在第二模式中， 经由腔室到达第一通道的第二通道。
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3.发明授权Rotary compressor-expander systems and associated methods of use and manufacture, including integral heat exchanger systems 有权旋转压缩机 - 膨胀机系统及相关的使用和制造方法，包括整体热交换器系统公开(公告)号：US09062548B2
公开(公告)日：2015-06-23
申请号：US13038360
申请日：2011-03-01
CPC分类号： F01C1/22 , F01C11/002 , F01C21/06 , Y02T10/16 , Y10T29/49245
摘要： The present technology is directed generally to rotary displacement systems and associated methods of use and manufacture. The systems can be used to compress and/or expand compressible fluids. In some embodiments, the rotary displacement systems include a chamber housing having a pressure-modifying chamber with a first port and a second port, a first passageway in fluid communication with the chamber via the first port, and a second passageway in fluid communication with the chamber via the second port. The systems can further include a shaft positioned within the chamber housing and rotatable relative to the chamber housing about a rotational axis, and a rotor comprising no more than two lobes. The rotor can be carried by and rotatable relative to the shaft, and can be alternately operable in a first mode in which flow is provided from the first passageway to the second passageway via the chamber and in a second mode in which flow is provided from the second passageway to the first passageway via the chamber.
摘要翻译： 本技术主要针对旋转位移系统和相关的使用和制造方法。 该系统可用于压缩和/或膨胀可压缩流体。 在一些实施例中，旋转位移系统包括具有第一端口和第二端口的压力调节室的腔室壳体，经由第一端口与腔室流体连通的第一通道，以及与腔室流体连通的第二通道， 通过第二个端口。 所述系统还可以包括定位在腔室壳体内并且围绕旋转轴线相对于腔室壳体可旋转的轴，以及包括不超过两个叶片的转子。 转子可以相对于轴承载并可转动，并且可以在第一模式中交替地操作，在第一模式中，第一模式从第一通道到第二通道经由室被提供，并且在第二模式中， 经由腔室到达第一通道的第二通道。
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4.发明授权Rotary compressor-expander systems and associated methods of use and manufacture 有权旋转压缩机 - 膨胀机系统及相关使用和制造方法公开(公告)号：US09057265B2
公开(公告)日：2015-06-16
申请号：US13038345
申请日：2011-03-01
CPC分类号： F01C1/22 , F01C11/002 , F01C21/06 , Y02T10/16 , Y10T29/49245
摘要： The present technology is directed generally to rotary displacement systems and associated methods of use and manufacture. The systems can be used to compress and/or expand compressible fluids. In some embodiments, the rotary displacement systems include a chamber housing having a pressure-modifying chamber with a first port and a second port, a first passageway in fluid communication with the chamber via the first port, and a second passageway in fluid communication with the chamber via the second port. The systems can further include a shaft positioned within the chamber housing and rotatable relative to the chamber housing about a rotational axis, and a rotor comprising no more than two lobes. The rotor can be carried by and rotatable relative to the shaft, and can be alternately operable in a first mode in which flow is provided from the first passageway to the second passageway via the chamber and in a second mode in which flow is provided from the second passageway to the first passageway via the chamber.
摘要翻译： 本技术主要针对旋转位移系统和相关的使用和制造方法。 该系统可用于压缩和/或膨胀可压缩流体。 在一些实施例中，旋转位移系统包括具有第一端口和第二端口的压力调节室的腔室壳体，经由第一端口与腔室流体连通的第一通道，以及与腔室流体连通的第二通道， 通过第二个端口。 所述系统还可以包括定位在腔室壳体内并且围绕旋转轴线相对于腔室壳体可旋转的轴，以及包括不超过两个叶片的转子。 转子可以相对于轴承载并可转动，并且可以在第一模式中交替地操作，在第一模式中，第一模式从第一通道到第二通道经由室被提供，并且在第二模式中， 经由腔室到达第一通道的第二通道。
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5.发明申请ROTARY COMPRESSOR-EXPANDER SYSTEMS AND ASSOCIATED METHODS OF USE AND MANUFACTURE 有权旋转式压缩机 - 膨胀机系统及相关使用和制造方法公开(公告)号：US20110209480A1
公开(公告)日：2011-09-01
申请号：US13038345
申请日：2011-03-01
CPC分类号： F01C1/22 , F01C11/002 , F01C21/06 , Y02T10/16 , Y10T29/49245
摘要： The present technology is directed generally to rotary displacement systems and associated methods of use and manufacture. The systems can be used to compress and/or expand compressible fluids. In some embodiments, the rotary displacement systems include a chamber housing having a pressure-modifying chamber with a first port and a second port, a first passageway in fluid communication with the chamber via the first port, and a second passageway in fluid communication with the chamber via the second port. The systems can further include a shaft positioned within the chamber housing and rotatable relative to the chamber housing about a rotational axis, and a rotor comprising no more than two lobes. The rotor can be carried by and rotatable relative to the shaft, and can be alternately operable in a first mode in which flow is provided from the first passageway to the second passageway via the chamber and in a second mode in which flow is provided from the second passageway to the first passageway via the chamber.
摘要翻译： 本技术主要针对旋转位移系统和相关的使用和制造方法。 该系统可用于压缩和/或膨胀可压缩流体。 在一些实施例中，旋转位移系统包括具有第一端口和第二端口的压力调节室的腔室壳体，经由第一端口与腔室流体连通的第一通道，以及与腔室流体连通的第二通道， 通过第二个端口。 所述系统还可以包括定位在腔室壳体内并且围绕旋转轴线相对于腔室壳体可旋转的轴，以及包括不超过两个叶片的转子。 转子可以相对于轴承载并可旋转，并且可以在第一模式中交替地操作，在第一模式中，第一模式从第一通道到第二通道经由腔室提供流动，并且在第二模式中， 经由腔室到达第一通道的第二通道。
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6.发明申请PNEUMATIC GEARBOX WITH VARIABLE SPEED TRANSMISSION AND ASSOCIATED SYSTEMS AND METHODS 审中-公开具有变速传动及相关系统和方法的气动齿轮箱公开(公告)号：US20120119510A1
公开(公告)日：2012-05-17
申请号：US13183427
申请日：2011-07-14
申请人： Brian Von Herzen , Scott R. Frazier
发明人： Brian Von Herzen , Scott R. Frazier
CPC分类号： F03D9/28 , F03D9/007 , F03D9/008 , F03D9/17 , F03D9/25 , F03D13/25 , F03D15/10 , F05B2210/401 , F05B2240/243 , F05B2250/25 , F05B2260/42 , H02S10/12 , Y02E10/46 , Y02E10/72 , Y02E60/15 , Y02E60/17
摘要： The present technology is directed generally to pneumatic gearbox systems with variable speed transmission and associated systems and methods. In selected embodiments, pneumatic gearbox systems can include a variable input power source and a compressor operatively coupled thereto. The compressor can be configured to compress a fluid at a first cyclic frequency from the variable power input power source. The system can further include a storage vessel in fluid communication with the compressor and an expander in fluid communication with the storage vessel. The storage vessel can be configured to retain a volume of the fluid after compression until the expander draws upon it to expand the fluid at a second cyclic frequency different from the first cyclic frequency. The second cyclic frequency can be configured to synchronize with that of an electrical generator.
摘要翻译： 本技术主要针对具有变速传动和相关系统和方法的气动变速箱系统。 在所选择的实施例中，气动变速箱系统可以包括可变输入动力源和与其可操作耦合的压缩机。 压缩机可以被配置为从可变功率输入电源以第一循环频率压缩流体。 该系统还可以包括与压缩机流体连通的储存容器和与储存容器流体连通的膨胀器。 储存容器可以被配置成在压缩之后保持一定体积的流体，直到膨胀器吸附在其上，以使流体以不同于第一循环频率的第二循环频率膨胀。 第二循环频率可以被配置成与发电机同步。
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公开(公告)号：US5681011A
公开(公告)日：1997-10-28
申请号：US111095
申请日：1993-08-24
申请人： Scott R. Frazier
发明人： Scott R. Frazier
摘要： The present invention comprises a method for injecting a heavier payload into orbit than is possible using a traditional method and the same rocket booster launch vehicle. The method of the present invention does not utilize a parking orbit and does not perform orbital injection at perigee or apogee of the desired orbit. Rather, in the present method the flight path angle is positive at the final lower stage booster burn so as to boost the perigee kick motor and payload into a suborbital trajectory having a low perigee, which may be below the surface of the Earth. In the preferred embodiment, the launch vehicle maintains a negative flight path angle during the PKM burn. The PKM burn does not occur at perigee, but perigee is at the desired location when the PKM burn is complete. Use of this method increases the payload capacity of some launch vehicles by up to fifty percent (50%).
摘要翻译： 本发明包括一种使用传统方法和相同的火箭助推器运载火箭将较重的有效载荷注入轨道的方法。 本发明的方法不利用停车轨道，并且不在所需轨道的近地点或远地点进行轨道射入。 相反，在本方法中，在最后的较低级助燃器燃烧时，飞行路径角度为正，以便将近地点踢脚马达和有效载荷提升为具有低近地点的眶下轨迹，该轨迹可能低于地球表面。 在优选实施例中，运载火箭在PKM燃烧期间保持负飞行路径角。 PKM烧伤不会发生在近地点，但是当PKM燃烧完成时，近地点位于所需的位置。 使用这种方法将一些运载火箭的有效负载能力提高了百分之五十（50％）。
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