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公开(公告)号：US20120119021A1
公开(公告)日：2012-05-17
申请号：US12947482
申请日：2010-11-16
申请人： Donald Burns , Kaushik Rajashekara
发明人： Donald Burns , Kaushik Rajashekara
摘要： One embodiment of the present invention is a unique aircraft. Another embodiment is a unique propulsion system for an aircraft. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft and aircraft propulsion systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译： 本发明的一个实施例是独特的飞机。 另一个实施例是用于飞行器的独特的推进系统。 其他实施例包括用于飞行器和飞机推进系统的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。
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公开(公告)号：US08690099B2
公开(公告)日：2014-04-08
申请号：US12947482
申请日：2010-11-16
申请人： Donald Burns , Kaushik Rajashekara
发明人： Donald Burns , Kaushik Rajashekara
IPC分类号： B64D41/00
摘要： One embodiment of the present invention is a unique aircraft. Another embodiment is a unique propulsion system for an aircraft. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft and aircraft propulsion systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译： 本发明的一个实施例是独特的飞机。 另一个实施例是用于飞行器的独特的推进系统。 其他实施例包括用于飞行器和飞机推进系统的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。
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公开(公告)号：US08684304B2
公开(公告)日：2014-04-01
申请号：US12947424
申请日：2010-11-16
申请人： Donald Burns , Kaushik Rajashekara
发明人： Donald Burns , Kaushik Rajashekara
IPC分类号： B64D41/00
CPC分类号： B64D27/00 , B64D33/00 , B64D35/00 , B64D2205/00 , F02C7/32 , F02C7/36 , Y02T50/44 , Y02T50/823
摘要： One embodiment of the present invention is a unique aircraft. Another embodiment is a unique aircraft propulsion system. Still another embodiment is a unique system for taxiing an aircraft without starting one or more main aircraft propulsion engines. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft taxiing and propulsion systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
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公开(公告)号：US08727270B2
公开(公告)日：2014-05-20
申请号：US12947451
申请日：2010-11-16
申请人： Donald Burns , Kaushik Rajashekara
发明人： Donald Burns , Kaushik Rajashekara
IPC分类号： B64D41/00
CPC分类号： B64D27/16 , B64D41/00 , B64D2041/005 , B64D2205/00 , F02C3/113 , F02C7/32 , F02C7/36 , F05D2220/50 , Y02T50/44 , Y02T50/823 , Y02T90/36
摘要： One embodiment of the present invention is a unique aircraft. Another embodiment is a unique aircraft propulsion system. Still another embodiment is a unique system for taxiing an aircraft without starting one or more main aircraft propulsion engines. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft taxiing and propulsion systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译： 本发明的一个实施例是独特的飞机。 另一个实施例是独特的飞机推进系统。 另一个实施例是用于在不启动一个或多个主飞行器推进发动机的情况下滑行飞行器的独特系统。 其他实施例包括用于飞机滑行和推进系统的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。
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公开(公告)号：US20120153076A1
公开(公告)日：2012-06-21
申请号：US12947451
申请日：2010-11-16
申请人： Donald Burns , Kaushik Rajashekara
发明人： Donald Burns , Kaushik Rajashekara
CPC分类号： B64D27/16 , B64D41/00 , B64D2041/005 , B64D2205/00 , F02C3/113 , F02C7/32 , F02C7/36 , F05D2220/50 , Y02T50/44 , Y02T50/823 , Y02T90/36
摘要： One embodiment of the present invention is a unique aircraft. Another embodiment is a unique aircraft propulsion system. Still another embodiment is a unique system for taxiing an aircraft without starting one or more main aircraft propulsion engines. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft taxiing and propulsion systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译： 本发明的一个实施例是独特的飞机。 另一个实施例是独特的飞机推进系统。 另一个实施例是用于在不启动一个或多个主飞行器推进发动机的情况下滑行飞行器的独特系统。 其他实施例包括用于飞机滑行和推进系统的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。
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公开(公告)号：US20120119020A1
公开(公告)日：2012-05-17
申请号：US12947424
申请日：2010-11-16
申请人： Donald Burns , Kaushik Rajashekara
发明人： Donald Burns , Kaushik Rajashekara
CPC分类号： B64D27/00 , B64D33/00 , B64D35/00 , B64D2205/00 , F02C7/32 , F02C7/36 , Y02T50/44 , Y02T50/823
摘要： One embodiment of the present invention is a unique aircraft. Another embodiment is a unique aircraft propulsion system. Still another embodiment is a unique system for taxiing an aircraft without starting one or more main aircraft propulsion engines. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft taxiing and propulsion systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
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7.发明授权Electrical power system with high-density pulse width modulated (PWM) rectifier 有权具有高密度脉宽调制（PWM）整流器的电力系统公开(公告)号：US08570774B2
公开(公告)日：2013-10-29
申请号：US12511859
申请日：2009-07-29
申请人： Ruxi Wang , Fred Wang , Rolando Burgos , Dushan Boroyevich , Kaushik Rajashekara , Stephen A. Long
发明人： Ruxi Wang , Fred Wang , Rolando Burgos , Dushan Boroyevich , Kaushik Rajashekara , Stephen A. Long
IPC分类号： H02M1/12
摘要： An electrical power system includes an alternating current (AC) power source configured to output an AC signal, a single phase pulse-width modulated (PWM) rectifier coupled to the AC power source and to an electrical load; a DC link capacitor coupled in parallel to the load and the PWM rectifier; and an active ripple energy storage circuit. The active ripple energy storage circuit has a first terminal, a second terminal and a third terminal, the active ripple energy storage circuit being coupled in parallel to the electrical load, the PWM rectifier and the DC link capacitor via the first terminal and the second terminal, the third terminal being coupled to the second terminal, the active ripple energy storage circuit being configured to selectively absorb and discharge at least part of the ripple energy.
摘要翻译： 电力系统包括被配置为输出AC信号的交流（AC）电源，耦合到AC电源和电负载的单相脉宽调制（PWM）整流器; 与负载和PWM整流器并联耦合的直流链路电容器; 和一个有源纹波储能电路。 主动波纹能量存储电路具有第一端子，第二端子和第三端子，主动纹波能量存储电路经由第一端子和第二端子并联耦合到电气负载，PWM整流器和DC链路电容器 ，所述第三端子耦合到所述第二端子，所述有源纹波能量存储电路被配置为选择性地吸收和放电至少部分所述纹波能量。
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8.发明申请ELECTRICAL POWER SYSTEM WITH HIGH-DENSITY PULSE WIDTH MODULATED (PWM) RECTIFIER 有权具有高密度脉冲宽度调制（PWM）整流器的电力系统公开(公告)号：US20100027304A1
公开(公告)日：2010-02-04
申请号：US12511859
申请日：2009-07-29
申请人： Ruxi Wang , Fred Wang , Rolando Burgos , Dushan Boroyevich , Kaushik Rajashekara , Stephen A. Long
发明人： Ruxi Wang , Fred Wang , Rolando Burgos , Dushan Boroyevich , Kaushik Rajashekara , Stephen A. Long
IPC分类号： H02M7/04
摘要： An electrical power system includes an alternating current (AC) power source configured to output an AC signal, a single phase pulse-width modulated (PWM) rectifier coupled to the AC power source and to an electrical load; a DC link capacitor coupled in parallel to the load and the PWM rectifier; and an active ripple energy storage circuit. The active ripple energy storage circuit has a first terminal, a second terminal and a third terminal, the active ripple energy storage circuit being coupled in parallel to the electrical load, the PWM rectifier and the DC link capacitor via the first terminal and the second terminal, the third terminal being coupled to the second terminal, the active ripple energy storage circuit being configured to selectively absorb and discharge at least part of the ripple energy
摘要翻译： 电力系统包括被配置为输出AC信号的交流（AC）电源，耦合到AC电源和电负载的单相脉宽调制（PWM）整流器; 与负载和PWM整流器并联耦合的直流链路电容器; 和一个有源纹波储能电路。 主动波纹能量存储电路具有第一端子，第二端子和第三端子，主动纹波能量存储电路经由第一端子和第二端子并联耦合到电气负载，PWM整流器和DC链路电容器 ，所述第三端子耦合到所述第二端子，所述有源纹波能量存储电路被配置为选择性地吸收和放电所述纹波能量的至少一部分
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公开(公告)号：US20060057442A1
公开(公告)日：2006-03-16
申请号：US11266987
申请日：2005-11-04
申请人： John Noetzel , Karl Haltiner , Kaushik Rajashekara
发明人： John Noetzel , Karl Haltiner , Kaushik Rajashekara
CPC分类号： H01M8/04365 , B60L11/1881 , B60L11/1892 , B60L11/1894 , H01M8/04559 , H01M8/04589 , H01M8/04947 , Y02T90/34 , Y10S429/90
摘要： A method of operating a fuel cell includes the step of selectively connecting and disconnecting the fuel cell to at least one electrical load dependent at least in part upon at least one of a fuel cell voltage, a fuel cell current and a fuel cell temperature.
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公开(公告)号：US20050266282A1
公开(公告)日：2005-12-01
申请号：US10855601
申请日：2004-05-27
申请人： John Noetzel , Kaushik Rajashekara , Harry Husted
发明人： John Noetzel , Kaushik Rajashekara , Harry Husted
CPC分类号： H01M8/0612 , H01M8/04007 , H01M8/04089 , H01M8/04298 , H01M2250/20 , Y02T90/32
摘要： A fuel cell system in accordance with the invention includes a single, central electronic controller (CPU) for controlling at least the Air Handling sub-system, the Reformer sub-system, the Power Electronics sub-system, and the Customer Interface sub-system. The central controller provides a central location for easier serviceability; increases data transport efficiency by eliminating lengthy links between distributed controllers; eliminates the need for multiple mechanical enclosures; allows for controller thermo conditioning in one mechanical enclosure; and reduces parasitic power losses by employing a single power supply.
摘要翻译： 根据本发明的燃料电池系统包括用于至少控制空气处理子系统，重整器子系统，电力电子子系统和客户接口子系统的单个中央电子控制器（CPU） 。 中央控制器提供了便于维修的中心位置; 通过消除分布式控制器之间的冗长链接来提高数据传输效率; 消除了对多个机械外壳的需要; 允许在一个机械外壳中进行控制器热调节; 并通过采用单个电源来减少寄生功率损耗。
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