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1. 发明申请

US20140012674A1 Heads-up billboard 审中-公开
标题翻译：头顶广告牌
公开(公告)号：US20140012674A1
公开(公告)日：2014-01-09
申请号：US13815769
申请日：2013-03-15
申请人： Gregory A. Piccionielli , Michael M. Gerardi
发明人： Gregory A. Piccionielli , Michael M. Gerardi
IPC分类号： G02B27/01 , G06Q30/02
CPC分类号： G02B27/017 , G06Q30/0257 , H01M8/0247 , H01M8/028 , H01M8/04007 , H01M8/04022 , H01M8/04111 , H01M8/04141 , H01M8/04291 , H01M8/0662 , H01M2008/1293 , H01M2250/00 , H01M2250/40 , H01M2250/405 , H01M2300/0074 , Y02B90/16 , Y02E60/56 , Y10S429/901
摘要： A method of providing visual information to a human viewer includes the steps of defining a range of distances from a surface and a range of viewing angles with respect to the surface, determining the location and viewing angle of a human viewer with respect to the surface, and providing a virtual image to the human viewer via a visual display device worn by the human viewer when the location and viewing angle of the human viewer with respect to the surface is determined to be within the defined range of distances and viewing angles, such that the virtual image is perceived to be defined on the surface by the human viewer.
摘要翻译：向人类观察者提供视觉信息的方法包括以下步骤：确定相对于表面的表面和视角范围的距离范围，确定人类观看者相对于表面的位置和视角，以及当人类观察者相对于表面的位置和视角被确定在所定义的距离和视角范围内时，通过人类观察者佩戴的视觉显示装置向人类观看者提供虚拟图像，使得感觉到虚拟图像被人类观察者在表面上被定义。

2. 发明授权

US08016228B2 Combined fuel cell aircraft auxiliary power unit and environmental control system 有权
标题翻译：燃料电池组合机组辅助动力装置和环境控制系统
公开(公告)号：US08016228B2
公开(公告)日：2011-09-13
申请号：US12106799
申请日：2008-04-21
申请人： Lars Fucke , David L. Daggett
发明人： Lars Fucke , David L. Daggett
IPC分类号： B64D41/00 , B64D13/00
CPC分类号： H01M8/04111 , B64D13/06 , B64D41/00 , B64D2013/0611 , B64D2041/005 , H01M8/04014 , H01M2008/1293 , H01M2250/20 , H01M2250/407 , Y02E60/525 , Y02E60/563 , Y02T50/44 , Y02T50/53 , Y02T50/56 , Y02T90/32 , Y02T90/36 , Y10S429/901
摘要： Combined aircraft hybrid fuel cell auxiliary power unit and environmental control system and methods are disclosed. In one embodiment, a method includes chemically converting a portion of combustible fuel into electrical energy. An unutilized portion of fuel emitted by the chemical conversion of combustible fuel is combusted to thermal power. The heated gas is used to drive a power recovery turbine connected to a drive shaft. A source of input oxidizing gas is compressed and is used to help chemically convert the combustible fuel into electrical energy. The heated gas is used to mechanically drive the power recovery turbine which is coupled to a generator to produce electrical energy.
摘要翻译：公开了组合式飞机混合燃料电池辅助动力装置及环境控制系统及方法。在一个实施例中，一种方法包括将可燃燃料的一部分化学转化为电能。通过可燃燃料的化学转化发出的燃料的未利用部分燃烧成热力。加热的气体用于驱动连接到驱动轴的动力回收涡轮机。输入氧化气体源被压缩并用于帮助将可燃燃料化学转化为电能。加热的气体用于机械地驱动耦合到发电机的功率回收涡轮机以产生电能。

3. 发明申请

US20080124592A1 Combined energy storage and fuel generation with reversible fuel cells 有权
公开(公告)号：US20080124592A1
公开(公告)日：2008-05-29
申请号：US12005344
申请日：2007-12-27
申请人： K.R. Sridhar , Matthias Gottmann
发明人： K.R. Sridhar , Matthias Gottmann
IPC分类号： H01M8/02 , C25B1/00
CPC分类号： H01M8/186 , C25B9/08 , H01M8/04201 , H01M8/0656 , H01M16/003 , H01M2008/1095 , H01M2008/1293 , Y02E60/528 , Y02P20/133 , Y10S429/901
摘要： An electrochemical system includes a reversible fuel cell system which generates electrical energy and reactant product from fuel and oxidizer in a fuel cell mode and which generates the fuel and oxidant from the reactant product and the electrical energy in an electrolysis mode. The system also includes a reactant product delivery device which is adapted to supply the reactant product to the reversible fuel cell system operating in the electrolysis mode, in addition to or instead of the reactant product generated by the reversible fuel cell system in the fuel cell mode, and a fuel removal device which is adapted to remove the fuel generated by the reversible fuel cell system operating in the electrolysis mode from the electrochemical system.

4. 发明授权

US07067208B2 Load matched power generation system including a solid oxide fuel cell and a heat pump and an optional turbine 有权
公开(公告)号：US07067208B2
公开(公告)日：2006-06-27
申请号：US10300021
申请日：2002-11-20
申请人： Matthias Gottmann , James F. McElroy
发明人： Matthias Gottmann , James F. McElroy
IPC分类号： H01M8/04 , H01M8/12
CPC分类号： H01M8/0662 , H01M8/0247 , H01M8/028 , H01M8/04007 , H01M8/04022 , H01M8/04111 , H01M8/04141 , H01M8/04291 , H01M2008/1293 , H01M2250/00 , H01M2250/40 , H01M2250/405 , H01M2300/0074 , Y02B90/16 , Y02E60/56 , Y10S429/901
摘要： Solid oxide fuel cell power generation systems which are capable of producing high-quality heat are used to drive refrigeration systems. The amount of electrical energy produced and the cooling capacity obtainable are well matched to electronic data center power and cooling needs. The power generation system includes a solid oxide fuel cell stack, a heat pump and an optional turbine.

5. 发明申请

US20040043268A1 Space heating system with fuel cells and a connection to a public electrical network 有权
标题翻译：具有燃料电池的空间加热系统和与公共电网的连接
公开(公告)号：US20040043268A1
公开(公告)日：2004-03-04
申请号：US10653736
申请日：2003-09-02
申请人： Sulzer Hexis AG
发明人： Stefan Genswein , Rene Dittli
IPC分类号： H01M008/04 , F24D005/00
CPC分类号： H01M8/04007 , H01M8/04089 , H01M8/04619 , H01M8/04753 , H01M8/0494 , H01M8/04955 , H01M2250/405 , Y02B90/16 , Y02P70/56 , Y10S429/90 , Y10S429/901
摘要： The space heating system with fuel cells (11) has a connection to a public electrical network (50). In this system a fuel (B) can be supplied to the fuel cells in gaseous form through a main gas valve (200) for the production of thermal and electrical energy. The main gas valve has a control which, on an interruption of the current supplied, results in an automatic operating shutdown. The possibilities exist for the system to feed the electrical energy at least partly into the network and to deliver the thermal energy to a heating circuit which is operable with electrical energy from the network. An electrical inverter (4), with which direct current of the fuel cells can be converted into alternating current, can be operated in two operating states, on the one hand, for a feed into the public network, and, on the other hand, for a feed into the island network of the system. Means are provided with respect to a power cut of the public network by which a short-term maintenance of necessary functions of the space heating systemnullthe fuel supply into the fuel cells having first prioritynullis ensured without support by, for example, galvanic batteries. Moreover, controls and circuits are provided with which at least the necessary functions of the space heating system can continue to be maintained by means of electrical energy from the fuel cells.
摘要翻译：具有燃料电池（11）的空间加热系统具有与公共电网（50）的连接。在该系统中，可以通过主气阀（200）将燃料（B）以气体形式供应到用于产生热能和电能的燃料电池。主气阀具有在所供给的电流中断时导致自动运行停机的控制。系统存在至少部分地将电能馈送到网络中并将热能传递到加热电路的可能性，加热电路可利用来自网络的电能来操作。燃料电池的直流电可以转换为交流电的电力逆变器（4）可以一方面用于进入公共网络的两个操作状态，另一方面，用于进入岛屿网络的系统。提供了关于公共网络的电力切断的手段，其中通过短路维护空间加热系统的必要功能（具有第一优先级的燃料电池中的燃料供应）被确保，而不由例如电流电池此外，提供了控制和电路，借助于来自燃料电池的电能可以继续保持空间加热系统的至少必要功能。

6. 发明申请

US20030224238A1 High-temperature compliant compression seal 有权
标题翻译：高温柔性压缩密封
公开(公告)号：US20030224238A1
公开(公告)日：2003-12-04
申请号：US10369322
申请日：2003-02-20
申请人： Ion America Corporation
发明人： John Finn , K. R. Sridhar
IPC分类号： H01M002/08
CPC分类号： H01M8/0662 , H01M8/0247 , H01M8/028 , H01M8/04007 , H01M8/04022 , H01M8/04111 , H01M8/04141 , H01M8/04291 , H01M2008/1293 , H01M2250/00 , H01M2250/40 , H01M2250/405 , H01M2300/0074 , Y02B90/16 , Y02E60/56 , Y10S429/901
摘要： A sealing arrangement contains a first mating surface, a second mating surface, and a felt sealing member contacting the first and the second mating surface. The arrangement may be used in a solid oxide fuel cell.
摘要翻译：密封装置包括第一配合表面，第二配合表面和接触第一和第二配合表面的毡密封构件。该装置可用于固体氧化物燃料电池。

7. 发明申请

US20030207164A1 Fuel cell for airship power generation and heating 失效
标题翻译：用于飞艇发电和加热的燃料电池
公开(公告)号：US20030207164A1
公开(公告)日：2003-11-06
申请号：US10428804
申请日：2003-05-05
申请人： ION AMERICA CORPORATION
发明人： James Frederick McElroy , K.R. Sridhar
IPC分类号： H01M008/04 , H01M008/18 , H01M008/12
CPC分类号： H01M8/186 , B64C39/024 , B64C2201/022 , B64C2201/042 , B64C2201/101 , B64C2201/127 , B64C2201/148 , B64C2201/165 , B64D27/24 , B64D2041/005 , B64D2211/00 , H01M8/04007 , H01M8/2475 , H01M2250/20 , Y02E60/528 , Y02T50/44 , Y02T50/55 , Y02T50/62 , Y02T90/32 , Y02T90/36 , Y10S429/901
摘要： A neutrally buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and a fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprising providing a fuel and a oxidizer to a solid oxide fuel cell to generate power, and providing heat from the fuel cell to a remotely located lifting body, wherein the lifting body allows the airship to remain neutrally buoyant in air.
摘要翻译：一个中性浮力的飞艇，如飞艇，包含一个提升机体，允许飞艇在空气中保持中性浮力，而位于飞艇上的燃料电池。一种在中性浮力飞艇中产生动力的方法，包括向固体氧化物燃料电池提供燃料和氧化剂以产生动力，并将热量从燃料电池提供到位于远处的提升体，其中提升体允许飞艇在空气中保持中性浮力。

8. 发明申请

US20030165732A1 Environmentally tolerant anode catalyst for a solid oxide fuel cell 有权
标题翻译：用于固体氧化物燃料电池的环境耐受性阳极催化剂
公开(公告)号：US20030165732A1
公开(公告)日：2003-09-04
申请号：US10368348
申请日：2003-02-20
申请人： ION AMERICA CORPORATION
发明人： James F. McElroy
IPC分类号： H01M004/86 , H01M008/12 , H01M008/04 , H01M008/10
CPC分类号： H01M8/0662 , H01M8/0247 , H01M8/028 , H01M8/04007 , H01M8/04022 , H01M8/04111 , H01M8/04141 , H01M8/04291 , H01M2008/1293 , H01M2250/00 , H01M2250/40 , H01M2250/405 , H01M2300/0074 , Y02B90/16 , Y02E60/56 , Y10S429/901
摘要： A solid oxide fuel cell includes a cathode, a solid ceramic electrolyte, and an anode comprising a cermet containing an environment tolerant catalyst, such as a fuel starvation and/or a sulfur tolerant catalyst.
摘要翻译：固体氧化物燃料电池包括阴极，固体陶瓷电解质和包含含有耐环境性催化剂例如燃料不足和/或耐硫催化剂的金属陶瓷的阳极。

9. 发明授权

US07781112B2 Combined energy storage and fuel generation with reversible fuel cells 有权
标题翻译：组合储能和燃料发电与可逆燃料电池
公开(公告)号：US07781112B2
公开(公告)日：2010-08-24
申请号：US12005344
申请日：2007-12-27
申请人： K. R. Sridhar , Matthias Gottmann
发明人： K. R. Sridhar , Matthias Gottmann
IPC分类号： H01M8/18 , H01M8/10
CPC分类号： H01M8/186 , C25B9/08 , H01M8/04201 , H01M8/0656 , H01M16/003 , H01M2008/1095 , H01M2008/1293 , Y02E60/528 , Y02P20/133 , Y10S429/901
摘要： An electrochemical system includes a reversible fuel cell system which generates electrical energy and reactant product from fuel and oxidizer in a fuel cell mode and which generates the fuel and oxidant from the reactant product and the electrical energy in an electrolysis mode. The system also includes a reactant product delivery device which is adapted to supply the reactant product to the reversible fuel cell system operating in the electrolysis mode, in addition to or instead of the reactant product generated by the reversible fuel cell system in the fuel cell mode, and a fuel removal device which is adapted to remove the fuel generated by the reversible fuel cell system operating in the electrolysis mode from the electrochemical system.
摘要翻译：电化学系统包括可逆燃料电池系统，其以燃料电池模式从燃料和氧化剂产生电能和反应物产物，并且以电解模式从反应物产物和电能产生燃料和氧化剂。该系统还包括反应物产品输送装置，其适于将反应物产物供应到以电解模式操作的可逆燃料电池系统，除了或代替由燃料电池模式中的可逆燃料电池系统产生的反应物产物以及燃料去除装置，其适于从电化学系统去除由在电解模式中运行的可逆燃料电池系统产生的燃料。

10. 发明申请

US20090305092A1 COMBINED FUEL CELL AIRCRAFT AUXILIARY POWER UNIT AND ENVIRONMENTAL CONTROL SYSTEM 有权
标题翻译：组合燃料电池飞机辅助电源和环境控制系统
公开(公告)号：US20090305092A1
公开(公告)日：2009-12-10
申请号：US12106799
申请日：2008-04-21
申请人： Lars Fucke , David L. Daggett
发明人： Lars Fucke , David L. Daggett
IPC分类号： H01M8/04
CPC分类号： H01M8/04111 , B64D13/06 , B64D41/00 , B64D2013/0611 , B64D2041/005 , H01M8/04014 , H01M2008/1293 , H01M2250/20 , H01M2250/407 , Y02E60/525 , Y02E60/563 , Y02T50/44 , Y02T50/53 , Y02T50/56 , Y02T90/32 , Y02T90/36 , Y10S429/901
摘要： Combined aircraft hybrid fuel cell auxiliary power unit and environmental control system and methods are disclosed. In one embodiment, a method includes chemically converting a portion of combustible fuel into electrical energy. An unutilized portion of fuel emitted by the chemical conversion of combustible fuel is combusted to thermal power. The heated gas is used to drive a power recovery turbine connected to a drive shaft. A source of input oxidizing gas is compressed and is used to help chemically convert the combustible fuel into electrical energy. The heated gas is used to mechanically drive the power recovery turbine which is coupled to a generator to produce electrical energy.
摘要翻译：公开了组合式飞机混合燃料电池辅助动力装置及环境控制系统及方法。在一个实施例中，一种方法包括将可燃燃料的一部分化学转化为电能。通过可燃燃料的化学转化发出的燃料的未利用部分燃烧成热力。加热的气体用于驱动连接到驱动轴的动力回收涡轮机。输入氧化气体源被压缩并用于帮助将可燃燃料化学转化为电能。加热的气体用于机械地驱动耦合到发电机的功率回收涡轮机以产生电能。

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