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1.发明申请EVAPORATIVELY COOLED FUEL CELL SYSTEM AND METHOD FOR OPERATING AN EVAPORATIVELY COOLED FUEL CELL SYSTEM 失效蒸气冷却燃料电池系统和运行蒸发冷却燃料电池系统的方法公开(公告)号：US20130260273A1
公开(公告)日：2013-10-03
申请号：US13893913
申请日：2013-05-14
发明人： Tobias Scheibert
IPC分类号： H01M8/04
CPC分类号： H01M8/04059 , B64D15/02 , B64D2041/005 , H01M2250/20 , Y02T90/32 , Y02T90/36
摘要： A fuel cell system (10) comprises a fuel cell (14) and an evaporative cooling system (16), which is in thermal contact with the fuel cell (14), in order that heat generated by the fuel cell (14) during operation of the fuel cell (14) is absorbed through evaporation of a cooling medium and is removed from the fuel cell (14). The fuel cell system (10) further comprises a device (22) for sensing the pressure in the evaporative cooling system (16). A control unit (24) is adapted to control the operating temperature of the fuel cell (14) in dependence on signals that are supplied to the control unit (24) from the device (22) for sensing the pressure in the evaporative cooling system (16), in such a way that the cooling medium of the evaporative cooling system (16) is transferred from the liquid to the gaseous state of matter by the heat generated by the fuel cell (14) during operation of the fuel cell (14).
摘要翻译： 燃料电池系统（10）包括与燃料电池（14）热接触的燃料电池（14）和蒸发冷却系统（16），以便在操作期间由燃料电池（14）产生的热量 的燃料电池（14）通过冷却介质的蒸发而被吸收并从燃料电池（14）移除。 燃料电池系统（10）还包括用于感测蒸发冷却系统（16）中的压力的装置（22）。 控制单元（24）适于根据从设备（22）提供给控制单元（24）的信号来控制燃料电池（14）的操作温度，用于感测蒸发冷却系统中的压力（ 16），使得蒸发冷却系统（16）的冷却介质在燃料电池（14）的操作期间由燃料电池（14）产生的热量从液体转移到气态物质， 。
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2.发明申请ICING PROTECTION SYSTEM FOR AN AIRCRAFT AND METHOD FOR OPERATING AN ICING PROTECTION SYSTEM 有权用于航空器的保护系统和操作保护系统的方法公开(公告)号：US20130199218A1
公开(公告)日：2013-08-08
申请号：US13754027
申请日：2013-01-30
发明人： Tobias Scheibert
IPC分类号： F25D21/04
CPC分类号： F25B21/04 , B64D15/02 , B64D15/04 , B64D15/06 , B64D2041/005 , F25D21/04 , H01M8/04059 , Y02T90/36
摘要： An icing protection system comprises a fuel cell, an evaporative cooling system, a thermal deicing device, a control unit and a device for measuring the pressure in the evaporative cooling system. The evaporative cooling system is in thermal contact with the fuel cell and with the thermal deicing device in order to conduct heat from the fuel cell to the thermal deicing device. The control unit controls the electrical power demanded from the evaporatively cooled fuel cell in dependence on a deviation of the pressure measured by the pressure measuring device from a predetermined NOMINAL pressure. In this way, an energetically very efficient and very well controllable icing protection system is made available that can be operated without bleed air supplied by engines or electrical energy provided by engine generators.
摘要翻译： 结冰保护系统包括燃料电池，蒸发冷却系统，热除冰装置，控制单元和用于测量蒸发冷却系统中的压力的装置。 蒸发冷却系统与燃料电池和热除冰装置热接触，以将热量从燃料电池传导到热除冰装置。 控制单元根据由压力测量装置测量的压力与预定的NOMINAL压力的偏差来控制从蒸发冷却的燃料电池所需的电力。 以这种方式，可以获得能够非常有效且非常好地控制的结冰保护系统，其可以在发动机或由发动机发电机提供的电能提供的排放空气下运行。
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3.发明授权Icing protection system for an aircraft and method for operating an icing protection system 有权用于飞机的结冰保护系统和运行结冰保护系统的方法公开(公告)号：US09267715B2
公开(公告)日：2016-02-23
申请号：US13754027
申请日：2013-01-30
发明人： Tobias Scheibert
CPC分类号： F25B21/04 , B64D15/02 , B64D15/04 , B64D15/06 , B64D2041/005 , F25D21/04 , H01M8/04059 , Y02T90/36
摘要： An icing protection system comprises a fuel cell, an evaporative cooling system, a thermal deicing device, a control unit and a device for measuring the pressure in the evaporative cooling system. The evaporative cooling system is in thermal contact with the fuel cell and with the thermal deicing device in order to conduct heat from the fuel cell to the thermal deicing device. The control unit controls the electrical power demanded from the evaporatively cooled fuel cell in dependence on a deviation of the pressure measured by the pressure measuring device from a predetermined NOMINAL pressure. In this way, an energetically very efficient and very well controllable icing protection system is made available that can be operated without bleed air supplied by engines or electrical energy provided by engine generators.
摘要翻译： 结冰保护系统包括燃料电池，蒸发冷却系统，热除冰装置，控制单元和用于测量蒸发冷却系统中的压力的装置。 蒸发冷却系统与燃料电池和热除冰装置热接触，以将热量从燃料电池传导到热除冰装置。 控制单元根据由压力测量装置测量的压力与预定的NOMINAL压力的偏差来控制从蒸发冷却的燃料电池所需的电力。 以这种方式，可以获得能够非常有效且非常好地控制的结冰保护系统，其可以在发动机或由发动机发电机提供的电能提供的排放空气下运行。
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4.发明授权Evaporatively cooled fuel cell system and method for operating an evaporatively cooled fuel cell system 失效蒸发冷却的燃料电池系统和用于操作蒸发冷却的燃料电池系统的方法公开(公告)号：US08685581B2
公开(公告)日：2014-04-01
申请号：US13893913
申请日：2013-05-14
发明人： Tobias Scheibert
IPC分类号： H01M8/04
CPC分类号： H01M8/04059 , B64D15/02 , B64D2041/005 , H01M2250/20 , Y02T90/32 , Y02T90/36
摘要： A fuel cell system (10) comprises a fuel cell (14) and an evaporative cooling system (16), which is in thermal contact with the fuel cell (14), in order that heat generated by the fuel cell (14) during operation of the fuel cell (14) is absorbed through evaporation of a cooling medium and is removed from the fuel cell (14). The fuel cell system (10) further comprises a device (22) for sensing the pressure in the evaporative cooling system (16). A control unit (24) is adapted to control the operating temperature of the fuel cell (14) in dependence on signals that are supplied to the control unit (24) from the device (22) for sensing the pressure in the evaporative cooling system (16), in such a way that the cooling medium of the evaporative cooling system (16) is transferred from the liquid to the gaseous state of matter by the heat generated by the fuel cell (14) during operation of the fuel cell (14).
摘要翻译： 燃料电池系统（10）包括与燃料电池（14）热接触的燃料电池（14）和蒸发冷却系统（16），以便在操作期间由燃料电池（14）产生的热量 的燃料电池（14）通过冷却介质的蒸发而被吸收并从燃料电池（14）移除。 燃料电池系统（10）还包括用于感测蒸发冷却系统（16）中的压力的装置（22）。 控制单元（24）适于根据从设备（22）提供给控制单元（24）的信号来控制燃料电池（14）的操作温度，用于感测蒸发冷却系统中的压力（ 16），使得蒸发冷却系统（16）的冷却介质在燃料电池（14）的操作期间由燃料电池（14）产生的热量从液体转移到气态物质， 。
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