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1. 发明授权

US08403258B2 Power regulating device for an aircraft 有权
标题翻译：飞机动力调节装置
公开(公告)号：US08403258B2
公开(公告)日：2013-03-26
申请号：US12563000
申请日：2009-09-18
申请人： Martin Arendt , Lars Frahm , Andreas Westenberger
发明人： Martin Arendt , Lars Frahm , Andreas Westenberger
IPC分类号： B64D27/00
CPC分类号： H01M8/04805 , H01M8/04082 , H01M8/04365 , H01M8/0444 , H01M8/04619 , H01M8/04626 , H01M8/2495 , H01M16/003 , H01M2250/20 , H01M2250/40 , H02J1/10 , H02J1/14 , H02J4/00 , H02J2001/004 , Y02E60/56 , Y02T90/32
摘要： A power regulator and a process regulator, or a power regulating device for regulating hybrid energy sources are provided for an aircraft. The power regulator and process regulator is equipped such that the requirement of a required means of a consumer is measurable. In this arrangement the power regulating device is equipped such that a first operating characteristic of a first energy source and a second operating characteristic of a second energy source are determinable. By means of the first energy source a first requirement share can be generated, and by means of the second energy source a second requirement share of the required means can be generated. The power regulating device can regulate the first energy source and the second energy source such that depending on the first operating characteristic and on the second operating characteristic the first requirement share and the second requirement share of the required means can be provided to the consumer.
摘要翻译：为飞机提供了功率调节器和过程调节器或用于调节混合能源的功率调节装置。功率调节器和过程调节器配备使得消费者需要的手段的要求是可测量的。在这种布置中，功率调节装置被配备成使得第一能量源的第一操作特性和第二能量源的第二操作特性是可确定的。通过第一能量源可以产生第一要求份额，并且借助于第二能量源可以产生所需装置的第二要求份额。功率调节装置可以调节第一能量源和第二能源，使得根据第一操作特性和第二操作特性，可以向消费者提供所需装置的第一需求份额和第二需求份额。

2. 发明申请

US20110174006A1 ZONE TEMPERATURE CONTROL ON BOARD AN AIRPLANE BY MEANS OF FUEL CELL WASTE HEAT 审中-公开
标题翻译：燃料电池废气处理机组的飞行员区域温度控制
公开(公告)号：US20110174006A1
公开(公告)日：2011-07-21
申请号：US13060829
申请日：2009-08-12
申请人： Martin Arendt , Till Marquardt , Andreas Westenberger , Lars Frahm
发明人： Martin Arendt , Till Marquardt , Andreas Westenberger , Lars Frahm
IPC分类号： F25B27/00 , B64D13/06 , B64D13/02
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , B64D2041/005 , Y02T50/56 , Y02T90/36
摘要： The invention relates to an air conditioning system for a transportation means, having multiple zones to be air-conditioned, which may be variably air-conditioned by means of processed supply air in combination with individual trim air conduits, wherein the air conditioning system further has at least one heat exchanger for heating supply air by means of the exhaust heat of a fuel cell, and for discharging the supply air into a trim air distributor supplying the trim air conduits.
摘要翻译：本发明涉及一种用于运输装置的空调系统，具有多个要进行空调的区域，其可以通过与各个装饰空气管道结合的经处理的供给空气进行可变空调，其中空调系统还具有至少一个热交换器，用于通过燃料电池的排热加热供应空气，并且用于将供应空气排放到供应修剪空气管道的修剪空气分配器中。

3. 发明申请

US20100071371A1 POWER REGULATING DEVICE FOR AN AIRCRAFT 有权
标题翻译：用于飞机的动力调节装置
公开(公告)号：US20100071371A1
公开(公告)日：2010-03-25
申请号：US12563000
申请日：2009-09-18
申请人： Martin ARENDT , Lars FRAHM , Andreas WESTENBERGER
发明人： Martin ARENDT , Lars FRAHM , Andreas WESTENBERGER
IPC分类号： F01B21/04
CPC分类号： H01M8/04805 , H01M8/04082 , H01M8/04365 , H01M8/0444 , H01M8/04619 , H01M8/04626 , H01M8/2495 , H01M16/003 , H01M2250/20 , H01M2250/40 , H02J1/10 , H02J1/14 , H02J4/00 , H02J2001/004 , Y02E60/56 , Y02T90/32
摘要： A power regulator and a process regulator, or a power regulating device for regulating hybrid energy sources are provided for an aircraft. The power regulator and process regulator is equipped such that the requirement of a required means of a consumer is measurable. In this arrangement the power regulating device is equipped such that a first operating characteristic of a first energy source and a second operating characteristic of a second energy source are determinable. By means of the first energy source a first requirement share can be generated, and by means of the second energy source a second requirement share of the required means can be generated. The power regulating device can regulate the first energy source and the second energy source such that depending on the first operating characteristic and on the second operating characteristic the first requirement share and the second requirement share of the required means can be provided to the consumer.
摘要翻译：为飞机提供了功率调节器和过程调节器或用于调节混合能源的功率调节装置。功率调节器和过程调节器配备使得消费者需要的手段的要求是可测量的。在这种布置中，功率调节装置被配备成使得第一能量源的第一操作特性和第二能量源的第二操作特性是可确定的。通过第一能量源可以产生第一要求份额，并且借助于第二能量源可以产生所需装置的第二要求份额。功率调节装置可以调节第一能量源和第二能源，使得根据第一操作特性和第二操作特性，可以向消费者提供所需装置的第一需求份额和第二需求份额。

4. 发明申请

US20090014593A1 Cooling system on the basis of suction of a boundary layer 有权
标题翻译：基于吸附边界层的冷却系统
公开(公告)号：US20090014593A1
公开(公告)日：2009-01-15
申请号：US12148953
申请日：2008-04-23
申请人： Andreas Westenberger , Martin Arendt , Till Marquardt , Lars Frahm , Geza Schrauf
发明人： Andreas Westenberger , Martin Arendt , Till Marquardt , Lars Frahm , Geza Schrauf
IPC分类号： B64C21/06 , F28D15/00
CPC分类号： B64C21/08 , B64D2013/0622 , Y02T50/166 , Y02T50/56
摘要： A cooling system on board an aircraft includes a device for removing by suction a boundary layer, and a heat exchanger through which flows the boundary layer air that has been removed by suction. Cooling by way of a ram air channel can be reduced or entirely stopped, depending on the flight phase, such that the air drag of the aircraft and thus the fuel consumption can be reduced.
摘要翻译：飞机上的冷却系统包括用于通过抽吸除去边界层的装置和通过抽吸除去的边界层空气流过的热交换器。取决于飞行阶段，通过冲压空气通道的冷却可以减少或完全停止，从而可以减少飞行器的空气阻力并因此降低燃料消耗。

5. 发明授权

US08191834B2 Cooling system on the basis of suction of a boundary layer 有权
标题翻译：基于吸附边界层的冷却系统
公开(公告)号：US08191834B2
公开(公告)日：2012-06-05
申请号：US12148953
申请日：2008-04-23
申请人： Andreas Westenberger , Martin Arendt , Till Marquardt , Lars Frahm , Geza Schrauf
发明人： Andreas Westenberger , Martin Arendt , Till Marquardt , Lars Frahm , Geza Schrauf
IPC分类号： B64C21/06
CPC分类号： B64C21/08 , B64D2013/0622 , Y02T50/166 , Y02T50/56
摘要： A cooling system on board an aircraft includes a device for removing by suction a boundary layer, and a heat exchanger through which flows the boundary layer air that has been removed by suction. Cooling by way of a ram air channel can be reduced or entirely stopped, depending on the flight phase, such that the air drag of the aircraft and thus the fuel consumption can be reduced.
摘要翻译：飞机上的冷却系统包括用于通过抽吸除去边界层的装置和通过抽吸除去的边界层空气流过的热交换器。取决于飞行阶段，通过冲压空气通道的冷却可以减少或完全停止，从而可以减少飞行器的空气阻力并因此降低燃料消耗。

6. 发明授权

US08623566B2 Aircraft fuel cell system 有权
标题翻译：飞机燃料电池系统
公开(公告)号：US08623566B2
公开(公告)日：2014-01-07
申请号：US12865007
申请日：2009-01-28
申请人： Andreas Westenberger , Martin Arendt , Lars Frahm , Till Marquardt
发明人： Andreas Westenberger , Martin Arendt , Lars Frahm , Till Marquardt
IPC分类号： H01M8/04 , B64D41/00
CPC分类号： H01M8/04014 , B64D41/00 , B64D2041/005 , H01M8/04089 , H01M8/04111 , H01M8/249 , H01M2008/1095 , H01M2250/20 , Y02T50/53 , Y02T90/32 , Y02T90/36
摘要： An aircraft fuel cell system includes a fuel cell which has an oxidant inlet for supplying an oxygen-containing medium to the fuel cell. An oxidant supply line has a first end which is connected to the oxidant inlet of the fuel cell. A second end of the oxidant supply line is connectable to a used air outlet of a cabin of the aircraft. A heat exchanger is located in the oxidant supply line and thermally couples the oxygen-containing medium flowing through the oxidant supply line and a second medium flowing through an air conditioning process air line of an air conditioning unit, the heat exchanger being located downstream of a cabin air compressor in the air conditioning process air line.
摘要翻译：飞机燃料电池系统包括具有用于向燃料电池供应含氧介质的氧化剂入口的燃料电池。氧化剂供应管线具有连接到燃料电池的氧化剂入口的第一端。氧化剂供应管线的第二端可连接到飞行器舱室的废气出口。热交换器位于氧化剂供应管线中并且热连接流过氧化剂供应管线的含氧介质和流过空调单元的空气调节处理空气管线的第二介质，该热交换器位于客舱空气压缩机在空调过程空气管路。

7. 发明申请

US20110045370A1 Aircraft Fuel Cell System 有权
标题翻译：飞机燃料电池系统
公开(公告)号：US20110045370A1
公开(公告)日：2011-02-24
申请号：US12865007
申请日：2009-01-28
申请人： Andreas Westenberger , Martin Arendt , Lars Frahm , Till Quardt
发明人： Andreas Westenberger , Martin Arendt , Lars Frahm , Till Quardt
IPC分类号： H01M8/04 , B64D41/00
CPC分类号： H01M8/04014 , B64D41/00 , B64D2041/005 , H01M8/04089 , H01M8/04111 , H01M8/249 , H01M2008/1095 , H01M2250/20 , Y02T50/53 , Y02T90/32 , Y02T90/36
摘要： An aircraft fuel cell system (10) includes a fuel cell (12a, 12b, 12c, 12d) which has an oxidant inlet (14a, 14b, 14c, 14d) for supplying an oxygen-containing medium to the fuel cell (12a, 12b, 12c, 12d). An oxidant supply line (16) has a first end which is connected to the oxidant inlet (14a, 14b, 14c, 14d) of the fuel cell (12a, 12b, 12c, 12d). A second end of the oxidant supply line (16) is connectable to a used air outlet (18) of a cabin (20) of the aircraft.
摘要翻译：飞机燃料电池系统（10）包括燃料电池（12a，12b，12c，12d），其具有用于向燃料电池（12a，12b）供应含氧介质的氧化剂入口（14a，14b，14c，14d），12c，12d）。氧化剂供应管线（16）具有连接到燃料电池（12a，12b，12c，12d）的氧化剂入口（14a，14b，14c，14d）的第一端。氧化剂供应管线（16）的第二端可连接到飞机的舱室（20）的用过的空气出口（18）。

8. 发明申请

US20070144460A1 HYBRID SYSTEM OF FUEL CELL AND COMBUSTION ENGINE 审中-公开
标题翻译：燃料电池和燃烧发动机混合系统
公开(公告)号：US20070144460A1
公开(公告)日：2007-06-28
申请号：US11613275
申请日：2006-12-20
申请人： Julika BLEIL , Martin ARENDT , Lars FRAHM , Andreas WESTENBERGER
发明人： Julika BLEIL , Martin ARENDT , Lars FRAHM , Andreas WESTENBERGER
IPC分类号： F02B43/08
CPC分类号： B60K6/32 , B60K6/24 , H01M8/04164 , H01M8/0662 , H01M2250/20 , H01M2250/407 , Y02E60/563 , Y02T10/6295 , Y02T90/32 , Y02T90/34
摘要： A hybrid system contains a fuel cell and a combustion engine, whereby a nitrogen-enriched discharge air of the fuel cell is used for a combustion process in a combustion chamber of the combustion engine.
摘要翻译：混合动力系统包括燃料电池和内燃机，由此燃料电池的富氮排放空气用于内燃机的燃烧室中的燃烧过程。

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