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41. 发明授权

US07546981B2 Drain system for an aircraft 失效
标题翻译：飞机排水系统
公开(公告)号：US07546981B2
公开(公告)日：2009-06-16
申请号：US11189622
申请日：2005-07-26
申请人： Claus Hoffjann , Hansgeorg Schuldzig , Harald Gruendel , Hans-Juergen Heinrich
发明人： Claus Hoffjann , Hansgeorg Schuldzig , Harald Gruendel , Hans-Juergen Heinrich
IPC分类号： B64D1/00
CPC分类号： B64C1/1453 , B64D11/02
摘要： Drain masts of commercial aircraft need to be heated in order to prevent freezing caused by the low outside temperatures when the aircraft travels at a corresponding altitude. An exemplary embodiment described in the application pertains to a drain system for an aircraft that can be used for draining liquids or gases from the aircraft or for drawing air into the aircraft. In this case, the liquids or gases are heated by means of a coolant that receives its thermal energy from a thermal or electrochemical process being carried out on board the aircraft. Consequently, the waste heat produced by the thermal or electrochemical process being carried out on board the aircraft, for example, a fuel cell process, can be carried off outboard via the drain system. In addition, the coolant can be advantageously utilized for cooling the thermal or electrochemical process.
摘要翻译：商用飞机的排水桅杆需要加热，以防飞机在相应的高度行驶时由外部温度低导致的冻结。本申请中描述的示例性实施例涉及一种用于飞机的排水系统，其可用于从飞行器排出液体或气体或将空气吸入飞行器。在这种情况下，液体或气体通过冷却剂加热，冷却剂从飞机上进行的热或电化学过程接收其热能。因此，通过在飞行器上执行的热或电化学过程产生的废热，例如燃料电池工艺，可以通过排水系统从外部排出。此外，冷却剂可以有利地用于冷却热或电化学过程。

42. 发明申请

US20080128276A1 SUPPLY END BLOCK FOR ROTARY MAGNETRON 有权
标题翻译：用于旋转磁铁的供应端块
公开(公告)号：US20080128276A1
公开(公告)日：2008-06-05
申请号：US11873532
申请日：2007-10-17
申请人： Hans-Juergen Heinrich , Goetz Teschner , Thorsten Sander , Cornell Weidelt , Joern Brueckner
发明人： Hans-Juergen Heinrich , Goetz Teschner , Thorsten Sander , Cornell Weidelt , Joern Brueckner
IPC分类号： C23C14/00
CPC分类号： C23C14/3407 , H01J37/34 , H01J37/3435 , H01J37/3497
摘要： A supply end block to supply a sputter cathode with a coolant and electrical voltage, includes a housing with a coolant connection and a current connection as well as a support shaft mounted to rotate, on which a target tube is fastened. The coolant connection and current connection are brought together directly at a feed site so that the coolant is brought to the potential of the applied electric voltage on entering the housing of the end block. Optimal cooling of the current feed is achieved, and optimal potential equalization of the coolant simultaneously occurs.
摘要翻译：供给具有冷却剂和电压的溅射阴极的供应端块包括具有冷却剂连接和电流连接的壳体以及安装成旋转的支撑轴，目标管被紧固在该壳体上。冷却剂连接和电流连接直接在进料位置组合在一起，使得冷却剂在进入端块的壳体时被施加到施加电压的电位。实现电流进料的最佳冷却，同时发生冷却剂的最佳电位均衡。

43. 发明申请

US20060099477A1 Fuel cell system 有权
标题翻译：燃料电池系统
公开(公告)号：US20060099477A1
公开(公告)日：2006-05-11
申请号：US11225589
申请日：2005-09-13
申请人： Claus Hoffjann , Hansgeorg Schuldzig , Hans-Juergen Heinrich
发明人： Claus Hoffjann , Hansgeorg Schuldzig , Hans-Juergen Heinrich
IPC分类号： H01M8/02 , H01M8/04
CPC分类号： H01M8/04291 , H01M8/00 , H01M8/004 , H01M8/0258 , H01M8/0267 , H01M8/04007 , H01M8/04059 , H01M8/04089 , H01M8/04111 , H01M8/04156 , H01M8/2475 , H01M2008/1095 , H01M2250/20 , Y02T90/32
摘要： For operation, PEMFCs require among other things a compressor for the cathode air, and a system for removing the water which is generated on the cathode side as a result of the electrochemical reaction. According to an embodiment of the present invention the removal of water is supported in that the fuel cell is made to rotate by way of an electric motor so that the water contained in the cathodes of the fuel cell can be extracted by centrifugal force. To this effect the air channels on the cathode side are arranged so as to extend radially or in a spiral shape from the inside towards the outside. In this way the efficiency of the fuel cell can be significantly improved.
摘要翻译：为了操作，PEMFC需要用于阴极空气的压缩机，以及用于去除由于电化学反应而在阴极侧产生的水的系统。根据本发明的一个实施方案，水的除去被支撑，因为燃料电池通过电动机旋转，使得包含在燃料电池的阴极中的水可以通过离心力提取。为此，阴极侧的空气通道被布置成从内向外径向或螺旋形地延伸。以这种方式，可以显着提高燃料电池的效率。

44. 发明申请

US20050271917A1 Electrochemical reactor for aircraft and method for operating the electrochemical reactor 审中-公开
标题翻译：用于飞机的电化学反应器和操作电化学反应器的方法
公开(公告)号：US20050271917A1
公开(公告)日：2005-12-08
申请号：US11135168
申请日：2005-05-23
申请人： Claus Hoffjann , Hans-Georg Schuldzig , Harald Gruendel , Hans-Juergen Heinrich
发明人： Claus Hoffjann , Hans-Georg Schuldzig , Harald Gruendel , Hans-Juergen Heinrich
IPC分类号： B64D11/02 , C02F1/461 , H01M8/04 , H01M8/06 , H01M8/12 , H01M8/18 , H01M8/24 , H01M16/00
CPC分类号： B64D11/02 , B64D2041/005 , H01M8/04007 , H01M8/04164 , H01M8/0612 , H01M8/182 , H01M8/2495 , H01M16/003 , H01M2008/1293 , H01M2250/20 , Y02E60/525 , Y02E60/528 , Y02T90/32 , Y02T90/36
摘要： In present-day aircraft, common containers for storing of the raw materials required for on-board operation, such as oxygen and water, are used. Energy is produced by using generators and turbines. According to one exemplary embodiment of the present invention, an electrochemical reactor for producing energy, hydrogen, oxygen, and clear water is provided, which ensures the on-board supply. According to the invention, hereby released reaction heat is used as additional process heat in an SOSE- and FP-process. In addition, by use of the hydrogen produced in the process, an extra desulphurization unit is eliminated with the fuel processing of the fuel in the FP process. In this manner, large storage volumes and weight can be saved.
摘要翻译：在目前的飞机中，使用用于存储船上操作所需的原材料的常见容器，例如氧气和水。能源是通过使用发电机和涡轮机生产的。根据本发明的一个示例性实施例，提供了用于产生能量，氢，氧和清水的电化学反应器，其确保车载供应。根据本发明，由此释放的反应热用作SOSE-和FP-工艺中的附加工艺热。此外，通过使用在该方法中产生的氢气，在FP处理中燃料的燃料处理消除额外的脱硫装置。以这种方式，可以节省大的存储量和重量。

45. 发明申请

US20050266287A1 Device for producing water on board of an airplane 有权
标题翻译：在飞机上生产水的装置
公开(公告)号：US20050266287A1
公开(公告)日：2005-12-01
申请号：US10532545
申请日：2003-10-21
申请人： Claus Hoffjann , Hans-Juergen Heinrich
发明人： Claus Hoffjann , Hans-Juergen Heinrich
IPC分类号： B64D11/02 , H01M8/04 , H01M8/12
CPC分类号： B64D11/02 , B64D2041/005 , Y02T50/46 , Y02T90/36
摘要： The invention relates to a device for producing water on board of an airplane by means of one or several fuel cells. The inventive water producing device is embodied in the form of one or several high temperature fuel cells (7) and entirely or partially integrated into a jet power unit of the airplane in such a way that the combustion chambers (7A) of said jet power unit of the airplane are entirely or partially substituted by said high temperature fuel cells. The aim of said invention is to develop a combination of fuel cells and a gas turbine which operates exclusively with atmospheric hydrogen and oxygen and is embodied in the form of a jet power unit and/or an auxiliary jet power unit (on-board auxiliary power unit: APU) used for producing compressed air for a cabin and a power supply. For this purpose, said high temperature fuel cells are fed with pure hydrogen on an anode side and with air on a cathode side. The combustion chambers (7A) are fed with an air-hydrogen mixture, enabling at least the hydrogen supply to be adjusted or completely shut off.
摘要翻译：本发明涉及一种用于通过一个或多个燃料电池在飞机上生产水的装置。本发明的水生产装置以一个或多个高温燃料电池（7）的形式实施，并且完全或部分地整合到飞机的喷射动力单元中，使得所述喷射功率的燃烧室（7A）飞机的单位完全或部分地被所述高温燃料电池所取代。所述发明的目的是开发燃料电池和仅具有大气氢和氧气的燃气轮机的组合，并且以喷射动力单元和/或辅助喷射动力单元（车载辅助动力单元：APU）用于生产客舱和电源的压缩空气。为此，所述高温燃料电池在阳极侧供给纯氢，并在阴极侧供给空气。燃烧室（7A）被供给空气 - 氢气混合物，使至少氢气供应被调节或完全切断。

46. 发明申请

US20050253019A1 Method and apparatus for tempering gaseous and/or liquid media in transportation vehicles, particularly in aircraft 失效
标题翻译：在运输车辆，特别是飞机上回火气体和/或液体介质的方法和装置
公开(公告)号：US20050253019A1
公开(公告)日：2005-11-17
申请号：US11115074
申请日：2005-04-25
申请人： Merle Hoehne , Joachim Hoehne , Hans-Juergen Heinrich
发明人： Merle Hoehne , Joachim Hoehne , Hans-Juergen Heinrich
IPC分类号： B64C1/00 , B64D11/02 , F28D20/00
CPC分类号： B64D11/02 , F28D20/003 , Y02E60/142 , Y02E70/30 , Y02T50/46
摘要： For example an aircraft includes a fluid tempering arrangement to supply a gaseous and/or liquid, heated and/or cooled, fluid such as water. At least one thermochemical reservoir is in heat exchange relation with a conduit system, having at least one valve and a controller that controls the transfer of heat between the fluid and the thermochemical reservoir to adjust the temperature of the fluid provided to an outlet. Preferably two interconnected thermochemical reservoirs respectively contain hydride-forming metals having different hydrogen sorption-desorption temperatures. A method involves supplying and chemically storing heat energy in at least one thermochemical reservoir, then performing a reverse reaction to release and transfer heat from at least one thermochemical reservoir to the fluid, preferably involving the sorption and desorption of hydrogen in respective hydride-forming metals in two reservoirs exhibiting different hydrogen reaction temperatures. Heat energy produced electrically during low electrical demand can be chemically stored and later released for heating the fluid during high electrical demand.
摘要翻译：例如，飞行器包括流体回火装置以供应气体和/或液体，加热和/或冷却的流体，例如水。至少一个热化学容器与导管系统处于热交换关系，具有至少一个阀和控制器，该控制器控制流体和热化学容器之间的热传递，以调节提供给出口的流体的温度。优选地，两个互连的热化学容器分别含有具有不同氢吸附 - 解吸温度的氢化物形成金属。一种方法包括在至少一个热化学储存器中提供和化学存储热能，然后进行逆反应以将热量从至少一个热化学储存器释放并传递到流体，优选地涉及在相应的氢化物形成金属中吸附和解吸氢在两个表现出不同氢反应温度的储层中。在低电力需求期间电气产生的热能可以被化学存储并且随后被释放以在高电需求期间加热流体。

47. 发明申请

US20050211842A1 Arrangement and method for the generation of water on board an aircraft 有权
标题翻译：在飞机上生成水的布置和方法
公开(公告)号：US20050211842A1
公开(公告)日：2005-09-29
申请号：US10999052
申请日：2004-11-29
申请人： Claus Hoffjann , Hansgeorg Schuldzig , Hans-Juergen Heinrich
发明人： Claus Hoffjann , Hansgeorg Schuldzig , Hans-Juergen Heinrich
IPC分类号： B64D11/02 , B64D41/00 , H01M8/04 , H01M8/06 , B64D11/00 , B64C1/00
CPC分类号： H01M8/04067 , B64D11/02 , B64D2041/005 , H01M8/04007 , H01M8/04089 , H01M8/04164 , H01M8/04708 , H01M8/04731 , H01M8/04753 , H01M8/0612 , H01M2250/00 , H01M2250/20 , Y02T90/32 , Y02T90/36
摘要： An arrangement and a method are proposed for the generation of water on board an aircraft with the use of one or more fuel cells, whereby low-temperature fuel cells are provided as fuel cells. It is proposed that several single-cell or few-cell fuel cells may form a fuel-cell panel or cell array and several cell panels or cell arrays may be arranged close to the inside of the aircraft fuselage and the cathode side of the at least one fuel cell has a chamber pointing to the exterior of the aircraft for the condensation of the water contained in the air and the anode side has a chamber carrying a combustion gas, for example hydrogen. With the proposed solution, a reduction in the storage capacity for drinking water and its quality-assured provision may be enabled and moreover, with the use of fuel cells as a virtual power station, the energy demand on engine generators, auxiliary power unit (APU) or ram air turbine (RAT) may be reduced.
摘要翻译：提出了一种使用一个或多个燃料电池在飞机上生成水的装置和方法，由此提供低温燃料电池作为燃料电池。提出几个单电池或少电池燃料电池可以形成燃料电池板或电池阵列，并且可以将几个电池板或电池阵列布置成靠近飞机机身的内部并且至少至少一个燃料电池具有指向飞行器外部的室，用于冷凝包含在空气中的水，并且阳极侧具有承载燃烧气体（例如氢气）的室。通过提出的解决方案，可以降低饮用水的储存能力及其质量保证的供应，而且，通过使用燃料电池作为虚拟发电站，对发动机发电机，辅助动力装置（APU）的能源需求）或冲压空气涡轮机（RAT）。

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