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1.发明申请Method for isolating a cabin wall of an aircraft or for cooling or heating of cabin air and a cabin wall suitable therefore 有权用于隔离飞行器舱壁或用于冷却或加热舱室空气和因此适合的舱壁的方法公开(公告)号：US20090189018A1
公开(公告)日：2009-07-30
申请号：US12317251
申请日：2008-12-19
申请人： Jan Dittmar , Marc Hoelling , Rainer Mueller
发明人： Jan Dittmar , Marc Hoelling , Rainer Mueller
CPC分类号： B64C1/066 , B64C1/40 , B64D13/08 , B64D2013/0662 , B64D2013/0688 , Y02T50/56
摘要： The present invention relates to a method for insulating an aircraft cabin 6 and for the cooling or heating of cabin air in an aircraft, respectively with the method comprising the steps of: introducing aircraft cabin air into an aircraft cabin wall 6; guiding this aircraft cabin air along a section of this aircraft cabin wall 6; and leading this aircraft cabin air away from the aircraft cabin wall 6.
摘要翻译： 本发明涉及一种隔离飞机机舱6并用于飞机内舱室空气冷却或加热的方法，方法包括以下步骤：将飞机机舱空气引入飞机机舱壁6; 引导这架飞机机舱沿着这架飞机舱壁6的一段空气; 并将该飞机机舱的空气引导离开飞机机舱壁6。
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2.发明授权Method for isolating a cabin wall of an aircraft or for cooling or heating of cabin air and a cabin wall suitable therefore 有权用于隔离飞行器舱壁或用于冷却或加热舱室空气和因此适合的舱壁的方法公开(公告)号：US08157209B2
公开(公告)日：2012-04-17
申请号：US12317251
申请日：2008-12-19
申请人： Jan Dittmar , Marc Hoelling , Rainer Mueller
发明人： Jan Dittmar , Marc Hoelling , Rainer Mueller
IPC分类号： B64C1/00
CPC分类号： B64C1/066 , B64C1/40 , B64D13/08 , B64D2013/0662 , B64D2013/0688 , Y02T50/56
摘要： The present invention relates to a method for insulating an aircraft cabin 6 and for the cooling or heating of cabin air in an aircraft, respectively with the method comprising the steps of: introducing aircraft cabin air into an aircraft cabin wall 6; guiding this aircraft cabin air along a section of this aircraft cabin wall 6; and leading this aircraft cabin air away from the aircraft cabin wall 6.
摘要翻译： 本发明涉及一种隔离飞机机舱6并用于飞机内舱室空气冷却或加热的方法，方法包括以下步骤：将飞机机舱空气引入飞机机舱壁6; 引导这架飞机机舱沿着这架飞机舱壁6的一段空气; 并将该飞机机舱的空气引导离开飞机机舱壁6。
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公开(公告)号：US20120279680A1
公开(公告)日：2012-11-08
申请号：US13434396
申请日：2012-03-29
申请人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
发明人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
IPC分类号： F28F27/00
摘要： A system for controlling a cooling system comprises an operating state detection unit adapted to detect operating signals characteristic of the operating state of the cooling system and/or the operating state of a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system and a database in which priority data dependent on the operating state and characteristic of the priority to be given to the cooling energy consumers in terms of the cooling energy to be supplied in various operating states of the cooling system and/or of the cooling energy consumers, is stored for a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system.
摘要翻译： 一种用于控制冷却系统的系统，包括操作状态检测单元，其适于检测冷却系统的运行状态的特性的运行信号和/或多个冷却能量消耗器的运行状态，以供冷却系统的冷却能量 以及数据库，其中根据要在冷却系统和/或冷却能量消耗器的各种操作状态下供应的冷却能量，依赖于给予冷却能量消耗器的优先级的操作状态和特性的优先级数据 被储存用于多个冷却能量消耗器以由冷却系统供应冷却能量。
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公开(公告)号：US09617007B2
公开(公告)日：2017-04-11
申请号：US13434396
申请日：2012-03-29
申请人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
发明人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
摘要： A system for controlling a cooling system comprises an operating state detection unit adapted to detect operating signals characteristic of the operating state of the cooling system and/or the operating state of a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system and a database in which priority data dependent on the operating state and characteristic of the priority to be given to the cooling energy consumers in terms of the cooling energy to be supplied in various operating states of the cooling system and/or of the cooling energy consumers, is stored for a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system.
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公开(公告)号：US09315272B2
公开(公告)日：2016-04-19
申请号：US13432733
申请日：2012-03-28
申请人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
发明人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
摘要： A system for cooling and/or heating aircraft devices to be cooled and/or heated includes a first individual cooling and/or heating system associated with a first aircraft device to be cooled and/or heated, a second individual cooling and/or heating system associated with a second aircraft device to be cooled and/or heated, a cooling and/or heating energy supply apparatus adapted to supply cooling and/or heating energy generated by the first and/or the second individual cooling and/or heating system to the first and/or the second aircraft device to be cooled and/or heated, a control device adapted to receive and process signals characteristic of the cooling and/or heating requirements of the first and/or the second aircraft device to be cooled and/or heated and of the load condition of the first and/or the second individual cooling and/or heating system.
摘要翻译： 用于冷却和/或加热待冷却和/或加热的飞行器装置的系统包括与要冷却和/或加热的第一飞行器装置相关联的第一单独冷却和/或加热系统，第二单独冷却和/或加热系统 与要冷却和/或加热的第二飞行器装置相关联的冷却和/或加热能量供应装置，其适于将由第一和/或第二单独冷却和/或加热系统产生的冷却和/或加热能量提供给 第一和/或待冷却和/或加热的第二飞行器装置，适于接收和处理特征于待冷却的第一和/或第二飞行器装置的冷却和/或加热要求的信号的控制装置和/或 加热和第一和/或第二单独冷却和/或加热系统的负载状态。
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6.发明申请公开(公告)号：US20110126562A1
公开(公告)日：2011-06-02
申请号：US12812831
申请日：2009-01-12
申请人： Jan Dittmar , Christian Schumacher
发明人： Jan Dittmar , Christian Schumacher
CPC分类号： B64D13/06 , B64D11/0626 , B64D2013/0662 , B64D2013/0674 , Y02T50/44 , Y02T50/46 , Y02T50/56
摘要： An air conditioning system for an aircraft for the individual air conditioning of regions of a cabin of an aircraft includes a central air conditioning device, which provides a pressurized and temperature-controlled central air flow. A part of the central air flow is supplied to a first cabin region. Another part of the central air flow is heated in a heating device or cooled in a cooling device and supplied to another cabin region. Water evaporates in the cooling device, in order to cool the air flow to be supplied to the cabin region.
摘要翻译： 用于飞行器机舱区域的各个空调的飞机的空调系统包括中央空调装置，其提供加压和温度控制的中央空气流。 中央空气流的一部分被供应到第一舱区域。 中央空气流的另一部分在加热装置中加热或在冷却装置中冷却并供应到另一个舱区。 水在冷却装置中蒸发，以便冷却要供应到舱区的空气流。
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7.发明授权Individual temperature-control of aircraft cabin regions by heating and evaporative cooling 有权通过加热和蒸发冷却对飞机机舱区域进行个别温度控制公开(公告)号：US09540111B2
公开(公告)日：2017-01-10
申请号：US12812831
申请日：2009-01-12
申请人： Jan Dittmar , Christian Schumacher
发明人： Jan Dittmar , Christian Schumacher
CPC分类号： B64D13/06 , B64D11/0626 , B64D2013/0662 , B64D2013/0674 , Y02T50/44 , Y02T50/46 , Y02T50/56
摘要： An air conditioning system for an aircraft for the individual air conditioning of regions of a cabin of an aircraft includes a central air conditioning device, which provides a pressurized and temperature-controlled central air flow. A part of the central air flow is supplied to a first cabin region. Another part of the central air flow is heated in a heating device or cooled in a cooling device and supplied to another cabin region. Water evaporates in the cooling device, in order to cool the air flow to be supplied to the cabin region.
摘要翻译： 用于飞行器机舱区域的各个空调的飞机的空调系统包括中央空调装置，其提供加压和温度控制的中央空气流。 中央空气流的一部分被供应到第一舱区域。 中央空气流的另一部分在加热装置中加热或在冷却装置中冷却并供应到另一个舱区。 水在冷却装置中蒸发，以便冷却要供应到舱区的空气流。
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8.发明申请METHOD FOR CONTROLLING THERMAL EFFLUENTS GENERATED BY AN AIRCRAFT AND COOLING DEVICE FOR AN AIRCRAFT IMPLEMENTING SAID METHOD 有权用于控制飞机生产的热效应的方法和用于实施方法的飞机的冷却装置公开(公告)号：US20100288244A1
公开(公告)日：2010-11-18
申请号：US12742937
申请日：2008-11-12
申请人： Guillaume Bulin , Jan Dittmar
发明人： Guillaume Bulin , Jan Dittmar
IPC分类号： F02G5/00
CPC分类号： B64D37/34 , B64D33/10 , B64D2013/0614 , B64D2013/0659 , F02C7/224 , Y02T50/54 , Y02T50/671
摘要： A process for management of thermal effluents of an aircraft that includes an airframe (110) and at least one propulsion system (112), whereby the at least one propulsion system (112) includes a gas turbine engine (116) that is supplied with fuel via a fuel supply circuit (122) that extends from a reservoir (124) that is arranged at the airframe (110), whereby the airframe (110) includes at least one source of thermal effluents (134), wherein the process includes at least partially dissipating—at the level of at least one propulsion system (112)—the thermal effluents that are generated at the airframe (110) by using as coolant the fuel that is used for supplying the gas turbine engine (116).
摘要翻译： 一种用于管理包括机体（110）和至少一个推进系统（112）的飞机的热排出物的过程，由此所述至少一个推进系统（112）包括燃气涡轮发动机（116），所述燃气涡轮发动机（116）被供应燃料 通过从布置在机身（110）处的储存器（124）延伸的燃料供应回路（122），由此机身（110）包括至少一个热源流出源（134），其中该过程至少包括 通过使用用于供应燃气涡轮发动机（116）的燃料作为冷却剂，在至少一个推进系统（112）的水平面部分地消散在机身（110）处产生的热流出物。
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公开(公告)号：US08572996B2
公开(公告)日：2013-11-05
申请号：US12744165
申请日：2008-11-26
申请人： Jan Dittmar , Nicolas Antoine , Uwe Buchholz
发明人： Jan Dittmar , Nicolas Antoine , Uwe Buchholz
IPC分类号： F25B27/00
CPC分类号： B64D13/06 , B64D2013/0607 , B64D2013/0611 , B64D2013/0618 , B64D2013/0644 , B64D2013/0696 , B64D2221/00 , Y02T50/44 , Y02T50/56
摘要： An energy supply system for operating at least one air conditioning system of an aircraft, comprises at least one air line network and at least one electric line network. The air line network is connected to the air conditioning system and at least one bleed air connection for routing bleed air to the air conditioning system. The electric line network is connected to the air conditioning system and at least one electrical energy source for routing electrical energy to the air conditioning system. The air conditioning system has an electrically operable cooling device. By means of the energy supply system according to the invention the energy withdrawn from the power units is better adapted to the energy necessary for operating the air conditioning system and other systems—such as, for example, wing de-icing—and therefore reduces the excess fuel consumption of the aircraft.
摘要翻译： 一种用于操作飞行器的至少一个空调系统的能量供应系统，包括至少一个空气管线网络和至少一个电力线路网络。 空气管网连接到空调系统和至少一个放气连接，用于将排气引导到空调系统。 电线网络连接到空调系统和至少一个用于将电能路由到空调系统的电能源。 空调系统具有电动可操作的冷却装置。 通过根据本发明的能量供应系统，从动力单元撤出的能量更好地适应于操作空调系统和其它系统所需的能量，例如机翼除冰 - 因此减少了 燃油消耗过多的飞机。
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10.发明授权Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said method 有权用于控制飞行器和用于执行所述方法的飞行器的冷却装置产生的热排出物的方法公开(公告)号：US08677755B2
公开(公告)日：2014-03-25
申请号：US12742937
申请日：2008-11-12
申请人： Guillaume Bulin , Jan Dittmar
发明人： Guillaume Bulin , Jan Dittmar
IPC分类号： F02C7/224
CPC分类号： B64D37/34 , B64D33/10 , B64D2013/0614 , B64D2013/0659 , F02C7/224 , Y02T50/54 , Y02T50/671
摘要： A process for management of thermal effluents of an aircraft that includes an airframe (110) and at least one propulsion system (112), whereby the at least one propulsion system (112) includes a gas turbine engine (116) that is supplied with fuel via a fuel supply circuit (122) that extends from a reservoir (124) that is arranged at the airframe (110), whereby the airframe (110) includes at least one source of thermal effluents (134), wherein the process includes at least partially dissipating—at the level of at least one propulsion system (112)—the thermal effluents that are generated at the airframe (110) by using as coolant the fuel that is used for supplying the gas turbine engine (116).
摘要翻译： 一种用于管理包括机体（110）和至少一个推进系统（112）的飞机的热排出物的过程，由此所述至少一个推进系统（112）包括燃气涡轮发动机（116），所述燃气涡轮发动机（116）被供应燃料 通过从布置在机身（110）处的储存器（124）延伸的燃料供应回路（122），由此机身（110）包括至少一个热源流出源（134），其中该过程至少包括 通过使用用于供应燃气涡轮发动机（116）的燃料作为冷却剂，在至少一个推进系统（112）的水平面部分地消散在机身（110）处产生的热流出物。
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