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1. 发明申请

US20120161512A1 METHOD FOR SUPPLYING ENERGY TO AN AIRCRAFT 审中-公开
标题翻译：向飞机提供能源的方法
公开(公告)号：US20120161512A1
公开(公告)日：2012-06-28
申请号：US13334531
申请日：2011-12-22
申请人： Dirk Metzler , Matthias Ludwig , Ralf Cremer , Jacques Herzog , Georg Ried
发明人： Dirk Metzler , Matthias Ludwig , Ralf Cremer , Jacques Herzog , Georg Ried
IPC分类号： H02G3/00
CPC分类号： B64D41/00 , B64D2041/005 , H01M8/04223 , H01M8/04225 , H01M2250/20 , Y02T50/44 , Y02T90/32 , Y02T90/36
摘要： The present invention relates to an energy supply system of an aircraft comprising a fuel cell and having one or more consumers which are or can be connected to the fuel cell such that they are supplied with energy directly or indirectly from the fuel cell in emergency operation as well has having at least one active energy store which is or can be connected to at least one of the consumers such that the consumer(s) is/are supplied with energy from the active energy store at least at times.
摘要翻译：本发明涉及一种包括燃料电池并且具有一个或多个消耗者的飞行器的能量供应系统，该消费者可以或可以连接到燃料电池，使得它们在紧急操作中直接或间接地从燃料电池供应，作为至少有一个有效能量存储器是或可以连接到消费者中的至少一个，使得消费者至少有时从活动能量存储器供应能量。

2. 发明申请

US20090104493A1 Energy supply system of an aircraft 审中-公开
标题翻译：一架飞机的能源供应系统
公开(公告)号：US20090104493A1
公开(公告)日：2009-04-23
申请号：US12009010
申请日：2008-01-16
申请人： Dirk Metzler , Matthias Ludwig , Ralf Cremer , Jacques Herzog , Georg Ried
发明人： Dirk Metzler , Matthias Ludwig , Ralf Cremer , Jacques Herzog , Georg Ried
IPC分类号： H01M8/04 , H01M8/00
CPC分类号： B64D41/00 , B64D2041/005 , H01M8/04223 , H01M8/04225 , H01M2250/20 , Y02T50/44 , Y02T90/32 , Y02T90/36
摘要： The present invention relates to an energy supply system of an aircraft comprising a fuel cell and having one or more consumers which are or can be connected to the fuel cell such that they are supplied with energy directly or indirectly from the fuel cell in emergency operation as well has having at least one active energy store which is or can be connected to at least one of the consumers such that the consumer(s) is/are supplied with energy from the active energy store at least at times.
摘要翻译：本发明涉及一种包括燃料电池并且具有一个或多个消耗者的飞行器的能量供应系统，该消费者可以或可以连接到燃料电池，使得它们在紧急操作中直接或间接地从燃料电池供应，作为至少有一个有效能量存储器是或可以连接到消费者中的至少一个，使得消费者至少有时从活动能量存储器供应能量。

3. 发明授权

US09617006B2 Emergency power system for an aircraft 有权
公开(公告)号：US09617006B2
公开(公告)日：2017-04-11
申请号：US13139066
申请日：2009-12-11
申请人： Ralf Brugger , Jörn Frick , Jacques Herzog , Dirk Metzler
发明人： Ralf Brugger , Jörn Frick , Jacques Herzog , Dirk Metzler
IPC分类号： B64D41/00 , B64D13/00 , B64D13/08 , B60H1/14 , B64D13/06
CPC分类号： B64D13/08 , B60H1/143 , B64D41/00 , B64D2013/0611 , B64D2041/002 , B64D2041/005 , Y02T90/36
摘要： The present invention relates to an emergency power system for an aircraft having at least one fuel cell unit for producing electric power, wherein the fuel cell unit is cooled via at least one cooling circuit which includes at least one heat exchanger, and wherein the heat exchanger is connected to at least one air distribution system of the aircraft cabin so that exhaust air heated by the heat exchanger in the operation of the emergency power system can be distributed via the air distribution system in the aircraft cabin.

4. 发明申请

US20110240795A1 EMERGENCY POWER SYSTEM FOR AN AIRCRAFT 有权
标题翻译：用于飞机的紧急动力系统
公开(公告)号：US20110240795A1
公开(公告)日：2011-10-06
申请号：US13139066
申请日：2009-12-11
申请人： Ralf Brugger , Jörn Frick , Jacques Herzog , Dirk Metzler
发明人： Ralf Brugger , Jörn Frick , Jacques Herzog , Dirk Metzler
IPC分类号： B64D41/00 , B64D13/00
CPC分类号： B64D13/08 , B60H1/143 , B64D41/00 , B64D2013/0611 , B64D2041/002 , B64D2041/005 , Y02T90/36
摘要： The present invention relates to an emergency power system for an aircraft having at least one fuel cell unit for producing electric power, wherein the fuel cell unit is cooled via at least one cooling circuit which includes at least one heat exchanger, and wherein the heat exchanger is connected to at least one air distribution system of the aircraft cabin so that exhaust air heated by the heat exchanger in the operation of the emergency power system can be distributed via the air distribution system in the aircraft cabin.
摘要翻译：本发明涉及一种用于具有至少一个用于产生电力的燃料电池单元的用于飞行器的应急电力系统，其中所述燃料电池单元经由至少一个包括至少一个热交换器的冷却回路冷却，并且其中所述热交换器连接到飞机机舱的至少一个空气分配系统，使得在应急电力系统的操作中由热交换器加热的废气可以经由飞机机舱中的空气分配系统分配。

5. 发明申请

US20060029849A1 System for water reclamation from an exhaust gas flow of a fuel cell of an aircraft 审中-公开
标题翻译：用于从飞行器的燃料电池的废气流中回收水的系统
公开(公告)号：US20060029849A1
公开(公告)日：2006-02-09
申请号：US11184221
申请日：2005-07-18
申请人： Dirk Metzler
发明人： Dirk Metzler
IPC分类号： H01M8/04 , B64D33/00
CPC分类号： H01M8/04291 , B64D2041/005 , H01M8/04022 , H01M8/04029 , H01M8/04164 , H01M2250/20 , Y02T90/32 , Y02T90/36
摘要： The present invention relates to a system for water reclamation from an exhaust gas flow of a fuel cell of an aircraft comprising a fuel cell for the energy supply of the aircraft, comprising an expansion unit in which the fuel cell exhaust gas is expanded and comprising a condenser for the condensation of water in the fuel cell exhaust gas, with the condenser being flowed through by the fuel cell exhaust gas on its hot side and by a cooling medium on its cold side. Provision is accordingly made for the hot side of the condenser to be connected upstream of the expansion unit and for the dehumidified fuel cell exhaust gas expanded in the expansion unit to serve as the cooling medium. The invention furthermore relates to an aircraft comprising a system in accordance with the invention for water reclamation from an exhaust gas flow of a fuel cell of an aircraft.
摘要翻译：本发明涉及一种用于从飞行器的燃料电池的废气流中回收水的系统，该系统包括用于飞行器的能量供应的燃料电池，其包括膨胀单元，在该膨胀单元中，燃料电池废气膨胀并且包括用于冷凝燃料电池废气中的水的冷凝器，其中冷凝器由燃料电池排气在其热侧流过，并通过其冷侧的冷却介质流过。因此，为了使冷凝器的热侧连接在膨胀单元的上游，并且在膨胀单元中膨胀的除湿燃料电池废气用作冷却介质。本发明还涉及一种飞行器，其包括根据本发明的用于从飞机的燃料电池的废气流进行水回收的系统。

6. 发明申请

US20070026268A1 Aircraft having a fuel cell 失效
标题翻译：具有燃料电池的飞机
公开(公告)号：US20070026268A1
公开(公告)日：2007-02-01
申请号：US11376823
申请日：2006-03-16
申请人： Dirk Metzler , Ralf Brugger
发明人： Dirk Metzler , Ralf Brugger
IPC分类号： H01M8/04 , B64D33/00
CPC分类号： H01M8/04029 , B64D2041/002 , B64D2041/005 , H01M8/04089 , Y02T90/36
摘要： The invention relates to an aircraft, in particular to an airplane, having at least one fuel cell, having at least one supply line which connects the fuel cell to a fuel supply, having at least one outlet line by means of which fuel supplied by the supply line and not consumed in the fuel cell is drained off and having means for the influencing of the fuel flow through the fuel cell as well as having means for the influencing of the fuel flow through the fuel cell, with the means for the influencing of the fuel flow having a pressure regulator located in the at least one supply line and a restrictor member located in the at least one outlet line, with the pressure regulator regulating the pressure of the fuel supply to the operating pressure of the fuel cell and with the restrictor member reducing the flow of the fuel flowing through the outlet line.
摘要翻译：本发明涉及一种具有至少一个燃料电池的飞机，特别是飞机，具有至少一个将燃料电池连接到燃料供应的供应管线，该至少一个供应管线具有至少一个出口管线，通过该出口管路由燃料电池中未消耗的供应管线被排出并且具有用于影响通过燃料电池的燃料流动的装置以及具有影响通过燃料电池的燃料流动的装置，具有影响燃料电池的装置所述燃料流具有位于所述至少一个供应管线中的压力调节器和位于所述至少一个出口管线中的限流器构件，所述压力调节器将所述燃料供应器的压力调节到所述燃料电池的操作压力，限制器构件减少流过出口管线的燃料的流动。

7. 发明授权

US07799477B2 Aircraft having a fuel cell 失效
标题翻译：具有燃料电池的飞机
公开(公告)号：US07799477B2
公开(公告)日：2010-09-21
申请号：US11376823
申请日：2006-03-16
申请人： Dirk Metzler , Ralf Brugger
发明人： Dirk Metzler , Ralf Brugger
IPC分类号： H01M8/06 , H01M8/04
CPC分类号： H01M8/04029 , B64D2041/002 , B64D2041/005 , H01M8/04089 , Y02T90/36
摘要： The invention relates to an aircraft, in particular to an airplane, having at least one fuel cell, having at least one supply line which connects the fuel cell to a fuel supply, having at least one outlet line by means of which fuel supplied by the supply line and not consumed in the fuel cell is drained off and having means for the influencing of the fuel flow through the fuel cell as well as having means for the influencing of the fuel flow through the fuel cell, with the means for the influencing of the fuel flow having a pressure regulator located in the at least one supply line and a restrictor member located in the at least one outlet line, with the pressure regulator regulating the pressure of the fuel supply to the operating pressure of the fuel cell and with the restrictor member reducing the flow of the fuel flowing through the outlet line.
摘要翻译：本发明涉及一种具有至少一个燃料电池的飞机，特别是飞机，具有至少一个将燃料电池连接到燃料供应的供应管线，该至少一个供应管线具有至少一个出口管线，通过该出口管路由燃料电池中未消耗的供应管线被排出并且具有用于影响通过燃料电池的燃料流动的装置以及具有影响通过燃料电池的燃料流动的装置，具有影响燃料电池的装置所述燃料流具有位于所述至少一个供应管线中的压力调节器和位于所述至少一个出口管线中的限流器构件，所述压力调节器将所述燃料供应器的压力调节到所述燃料电池的操作压力，限制器构件减少流过出口管线的燃料的流动。

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