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1.发明授权Craft and method of coupling a propulsion system to a regenerative fuel cell system 有权将推进系统耦合到再生燃料电池系统的工艺和方法公开(公告)号：US08282045B2
公开(公告)日：2012-10-09
申请号：US12711955
申请日：2010-02-24
申请人： Isabelle Nann , Antoine Iffly , Martin Lang
发明人： Isabelle Nann , Antoine Iffly , Martin Lang
CPC分类号： B64G1/402 , B64G1/1007 , B64G1/423
摘要： The invention relates to a craft comprising an energy storage system of the RFCS (regenerative fuel cell system) type and a system for pressurizing the propellants used for propulsion. The craft also comprises a plurality of means (31 to 38) for coupling the tanks of the fuel cell to the propellant-pressurizing tanks of the propulsion system of the craft when the tanks of the propellant-pressurizing system are no longer used.The invention also relates to the method of coupling the tanks of the propellant-pressurizing means to the energy storage system.The invention applies particularly to telecommunication satellites and more generally to spacecraft.
摘要翻译： 本发明涉及一种包括RFCS（再生燃料电池系统）类型的能量存储系统和用于对用于推进的推进剂进行加压的系统的工艺。 该工艺还包括多个装置（31至38），用于当不再使用推进剂加压系统的罐时，将燃料电池的罐连接到工艺的推进系统的推进剂加压罐。 本发明还涉及将推进剂加压装置的罐联接到储能系统的方法。 本发明特别适用于电信卫星，更一般地应用于航天器。
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2.发明申请Craft and Method of Coupling a Propulsion System to a Regenerative Fuel Cell System 有权将推进系统耦合到再生燃料电池系统的工艺和方法公开(公告)号：US20100213319A1
公开(公告)日：2010-08-26
申请号：US12711955
申请日：2010-02-24
申请人： Isabelle Nann , Antoine Iffly , Martin Lang
发明人： Isabelle Nann , Antoine Iffly , Martin Lang
IPC分类号： B64G1/40
CPC分类号： B64G1/402 , B64G1/1007 , B64G1/423
摘要： The invention relates to a craft comprising an energy storage system of the RFCS (regenerative fuel cell system) type and a system for pressurizing the propellants used for propulsion. The craft also comprises a plurality of means (31 to 38) for coupling the tanks of the fuel cell to the propellant-pressurizing tanks of the propulsion system of the craft when the tanks of the propellant-pressurizing system are no longer used.The invention also relates to the method of coupling the tanks of the propellant-pressurizing means to the energy storage system.The invention applies particularly to telecommunication satellites and more generally to spacecraft.
摘要翻译： 本发明涉及一种包括RFCS（再生燃料电池系统）类型的能量存储系统和用于对用于推进的推进剂进行加压的系统的工艺。 该工艺还包括多个装置（31至38），用于当不再使用推进剂加压系统的罐时，将燃料电池的罐连接到工艺的推进系统的推进剂加压罐。 本发明还涉及将推进剂加压装置的罐联接到储能系统的方法。 本发明特别适用于电信卫星，更一般地应用于航天器。
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公开(公告)号：US08616271B2
公开(公告)日：2013-12-31
申请号：US12037186
申请日：2008-02-26
申请人： Julien Hugon , Thierry Dargent , Isabelle Nann , Paul De Larminat
发明人： Julien Hugon , Thierry Dargent , Isabelle Nann , Paul De Larminat
摘要： The invention relates to a thermal control device intended to dissipate the heat generated by a payload on a spacecraft, comprising a number of surfaces and including means for circulating a refrigerant. An evaporation zone (Z1) comprises means for circulating the refrigerant, a compression zone (Z2), a condensation zone (Z3) comprising at least one radiating panel, linked to a part of the means for circulating the refrigerant, including several branches and comprising means to allow or inhibit the circulation of the refrigerant within these branches so as to vary the area of the heat exchange surface in the condensation zone, a pressure reduction zone (Z4) comprising means for circulating the refrigerant. Such a device is particularly well adapted to thermal problems encountered in telecommunications satellites.
摘要翻译： 本发明涉及一种热控制装置，其旨在消散由有效载荷在航天器上产生的热量，包括多个表面并且包括用于循环制冷剂的装置。 蒸发区（Z1）包括用于使制冷剂循环的装置，压缩区（Z2），包括至少一个散热板的冷凝区（Z3），其连接到用于循环制冷剂的装置的一部分，包括多个分支，并且包括 允许或禁止在这些分支中的制冷剂的循环以便改变冷凝区中的热交换表面的面积的装置，包括使制冷剂循环的装置的减压区（Z4）。 这种装置特别适用于电信卫星遇到的热问题。
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公开(公告)号：US20100223942A1
公开(公告)日：2010-09-09
申请号：US12718748
申请日：2010-03-05
申请人： Anne-Sophie Merino , Julien Hugon , Valérie Canton , Patrick Hugonnot , Thierry Dargent , Isabelle Nann
发明人： Anne-Sophie Merino , Julien Hugon , Valérie Canton , Patrick Hugonnot , Thierry Dargent , Isabelle Nann
CPC分类号： B64G1/1007 , B64G1/50 , B64G1/503 , B64G1/506 , F28D15/00 , F28D15/0266 , F28D15/0275
摘要： The invention relates to a thermal management device intended to collect the heat dissipated by a group of dissipative equipment of a spacecraft in an evaporation zone before discharging this heat to cold space via a condensation zone, situated in the region of the radiators. The evaporation zone and the condensation zone each consist of at least one heat-exchange part comprising a network of a plurality of compact heat-exchange elements distributed over their respective heat-exchange surface and connected in series and/or in parallel by the tubes of the thermal fluid circulation means.A device such as this is particularly intended for telecommunications satellites.
摘要翻译： 本发明涉及一种热管理装置，其用于在通过位于散热器的区域中的冷凝区将该热量排放到冷空气之前收集由蒸发区中的一组飞行器的耗散设备消散的热量。 蒸发区和冷凝区各自包括至少一个热交换部分，该热交换部分包括分布在它们各自的热交换表面上的多个紧凑的热交换元件的网络，并且由管的串联和/或并联连接 热流体循环装置。 诸如此类的设备特别适用于通信卫星。
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公开(公告)号：US20080217483A1
公开(公告)日：2008-09-11
申请号：US12037186
申请日：2008-02-26
申请人： Julien HUGON , Thierry Dargent , Isabelle Nann , Paul De Larminat
发明人： Julien HUGON , Thierry Dargent , Isabelle Nann , Paul De Larminat
摘要： The invention relates to a thermal control device intended to dissipate the heat generated by a payload on a spacecraft, comprising a number of surfaces and including means for circulating a refrigerant. An evaporation zone (Z1) comprises means for circulating the refrigerant, a compression zone (Z2), a condensation zone (Z3) comprising at lEast one radiating panel, linked to a part of the means for circulating the refrigerant, including several branches and comprising means to allow or inhibit the circulation of the refrigerant within these branches so as to vary the area of the heat exchange surface in the condensation zone, a pressure reduction zone (Z4) comprising means for circulating the refrigerant. Such a device is particularly well adapted to thermal problems encountered in telecommunications satellites.
摘要翻译： 本发明涉及一种热控制装置，其旨在消散由有效载荷在航天器上产生的热量，包括多个表面并且包括用于循环制冷剂的装置。 蒸发区（Z 1> 1）包括用于循环制冷剂，压缩区（Z 2/2），冷凝区（Z 3 3））的装置， 包括在第一个辐射面板上，连接到用于循环制冷剂的装置的一部分，包括多个分支，并且包括允许或抑制制冷剂在这些分支内的循环的装置，以便改变在这些分支中的热交换表面的面积 冷凝区，包括用于循环制冷剂的装置的减压区（Z 4 S 4）。 这种装置特别适用于电信卫星遇到的热问题。
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