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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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公开(公告)号：US08721406B2
公开(公告)日：2014-05-13
申请号：US13001353
申请日：2009-06-23
IPC分类号： B64D13/00
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56
摘要： An air duct for supplying ambient air in an aircraft includes an air inlet, a flow duct portion and a feed device that is devised to feed ambient air through the air inlet and the flow duct portion. A flow control flap closes the air inlet in a first position, releases a first flow cross-section of the air inlet in a second position and releases a larger second flow cross-section of the air inlet in a third position. The flow control flap is designed to not increase drag significantly in the second position while still enabling flow through the flow duct portion, while increasing drag to increase air fow through the flow duct portion in the third position.
摘要翻译： 用于在飞行器中供应环境空气的空气管道包括空气入口，流动管道部分和进给装置，其被设计成通过空气入口和流动管道部分供给环境空气。 流动控制翼将空气入口封闭在第一位置，将空气入口的第一流动横截面释放在第二位置，并在第三位置释放空气入口的较大的第二流动横截面。 流量控制挡板被设计成在第二位置中不会显着地增加阻力，同时仍然允许流过流道部分，同时增加阻力以增加通过第三位置中的流动管道部分的气流。
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5.发明申请Cooling Of An Electronic Device In An Aircraft By Case-By-Case Single-Phase Or Two-Phase Cooling 审中-公开飞机中电子设备的冷却通过单相或双相冷却公开(公告)号：US20120000630A1
公开(公告)日：2012-01-05
申请号：US12995220
申请日：2009-05-13
CPC分类号： B64D13/00 , B64D2013/0614 , B64D2013/0674 , F28D15/0266 , H05K7/20354
摘要： Cooling of an electronic device in an aircraft by case-by-case single-phase or two-phase coolingThere is proposed a method for cooling an electronic device in an aircraft (11), comprising the following steps:circulating a coolant in a cooling circuit,cooling the electronic device (2) by means of the coolant, andin an aircraft outer-shell heat exchanger, emitting the heat taken up by the coolant. The coolant evaporates, at least partially, during the cooling of the electronic device (2), and condenses in the aircraft outer-shell heat exchanger (7). The coolant circulates in the coolant circuit by natural convection.
摘要翻译： 通过逐个单相或两相冷却来冷却飞机中的电子设备提出了一种用于冷却飞行器（11）中的电子设备的方法，包括以下步骤：将冷却剂循环在冷却 电路，通过冷却剂冷却电子设备（2），并在飞机外壳热交换器中发射由冷却剂吸收的热量。 在冷却电子设备（2）期间，冷却剂至少部分地蒸发，并且在飞机外壳热交换器（7）中冷凝。 冷却剂通过自然对流在冷却剂回路中循环。
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公开(公告)号：US20110151764A1
公开(公告)日：2011-06-23
申请号：US13001353
申请日：2009-06-23
IPC分类号： B64D13/00
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56
摘要： The invention relates to an air duct (10) for supplying ambient air in an aircraft, comprising an air inlet (12), a flow duct portion (16) extending downstream of the air inlet (12) and a feed device (22) that is devised to feed ambient air through the air inlet (12) and the flow duct portion (16). A flow control flap (24) closes the air inlet (12) in a first position, releases a first flow cross-section of the air inlet (12) in a second position and releases a second flow cross-section of the air inlet (12), which is larger than the first flow cross-section, in a third position. The flow control flap (24) is so designed and disposed that a first surface portion (28) of the flow control flap (24), in the second position of the flow control flap (24), is aligned in the region of the air inlet (12) substantially parallel to an aircraft outer skin portion (18) is surrounding the air inlet (12), and that the first surface portion (28) of the flow control flap (24), in the third position of the flow control flap (14), is aligned in the region of the air inlet (12) at an angle to the aircraft outer skin portion (18) surrounding the air inlet (12).
摘要翻译： 本发明涉及一种用于在飞行器中提供环境空气的空气管道（10），包括空气入口（12），在空气入口（12）的下游延伸的流动管道部分（16）和进料装置（22） 被设计成通过空气入口（12）和流动管道部分（16）供给环境空气。 流动控制翼片（24）在第一位置关闭空气入口（12），将空气入口（12）的第一流动横截面释放在第二位置，并释放空气入口的第二流动横截面 12），其大于第一流动横截面，在第三位置。 流动控制翼片（24）被设计和设置成使得在流动控制翼片（24）的第二位置处的流量控制翼片（24）的第一表面部分（28）在空气的区域中对准 基本上平行于飞行器外皮部分（18）的入口（12）围绕空气入口（12），并且流量控制翼片（24）的第一表面部分（28）处于流量控制 翼片（14）在空气入口（12）的区域中与围绕空气入口（12）的飞行器外皮部分（18）成一定角度排列。
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公开(公告)号：US09045229B2
公开(公告)日：2015-06-02
申请号：US13189039
申请日：2011-07-22
申请人： Sebastian Roering
发明人： Sebastian Roering
IPC分类号： A47B96/04 , A47B95/00 , A47B96/00 , A61G11/00 , F16J15/46 , B64D11/00 , B64D13/00 , B64C1/14 , E06B7/23 , F25D19/00 , B64D11/04 , B64D13/06
CPC分类号： B64D11/0007 , B64D11/04 , B64D2013/0629 , E06B7/2318 , F16J15/46 , F25D19/003
摘要： A sealing system (38) for use in an aircraft facility to be sealed from the environment comprises a closing element (40) which can be connected to a housing (42) of the aircraft facility in order to seal an opening (44) formed in the housing (42) of the aircraft facility. Furthermore, the sealing system (38) comprises a receiving device (46), and a sealing element (48) received in the receiving device (46). A transfer device (54) is adapted to transfer the sealing element (48) between an inactive state, in which the sealing element (48) is shaped and/or positioned such that it cannot be brought into sealing contact with a sealing surface (64), and an active state, in which the sealing element (48) is shaped and/or positioned such that it can be brought into sealing contact with the sealing surface (64).
摘要翻译： 一种用于飞机设备中以便与环境密封的密封系统（38）包括关闭元件（40），其能够连接到飞行器设备的壳体（42），以便密封形成在其中的开口（44） 飞机设备的壳体（42）。 此外，密封系统（38）包括接收装置（46）和容纳在接收装置（46）中的密封元件（48）。 传送装置（54）适于将密封元件（48）转移到其中密封元件（48）被成形和/或定位成不能与密封表面（64）密封接触的非活动状态 ）和活动状态，其中密封元件（48）成形和/或定位成使得其能够与密封表面（64）密封接触。
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公开(公告)号：US20130074530A1
公开(公告)日：2013-03-28
申请号：US13428050
申请日：2012-03-23
CPC分类号： F25B41/00 , F25B1/00 , F25B23/006 , F25B2600/13 , Y02B30/745
摘要： A cooling system for cooling food on board an aircraft includes a cooling circuit adapted to supply cooling energy to at least one cooling station, a refrigerant circulating in the cooling circuit selected such that it is convertible at least partially from the liquid to the gaseous state of aggregation on releasing its cooling energy to the at least one cooling station and subsequently convertible back at least partially to the liquid state of aggregation again by an appropriate pressure and temperature control in the cooling circuit, and a refrigerant container including a receiving space arranged in an interior space of the refrigerant container which receives the refrigerant circulating in the cooling circuit, the receiving space of the refrigerant container connected to the cooling circuit by a flow line for discharging the refrigerant from the receiving space and by a return line for returning the refrigerant into the receiving space.
摘要翻译： 一种用于冷却飞机上的食物的冷却系统，包括适于向至少一个冷却站供应冷却能量的冷却回路，选择冷却回路中循环的制冷剂，使其至少部分地从液体转变为气态 在至少一个冷却站释放其冷却能量并且随后通过冷却回路中的适当的压力和温度控制再次可转换回到聚集的液体状态的聚集;以及制冷剂容器，其包括布置在 接收在冷却回路中循环的制冷剂的制冷剂容器的内部空间，通过用于从制冷剂从容纳空间排出的流路的冷却回路连接的制冷剂容器的容纳空间和用于使制冷剂返回的返回管 接收空间。
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公开(公告)号：US20120025679A1
公开(公告)日：2012-02-02
申请号：US13189039
申请日：2011-07-22
申请人： Sebastian Roering
发明人： Sebastian Roering
CPC分类号： B64D11/0007 , B64D11/04 , B64D2013/0629 , E06B7/2318 , F16J15/46 , F25D19/003
摘要： A sealing system (38) for use in an aircraft facility to be sealed from the environment comprises a closing element (40) which can be connected to a housing (42) of the aircraft facility in order to seal an opening (44) formed in the housing (42) of the aircraft facility. Furthermore, the sealing system (38) comprises a receiving device (46), and a sealing element (48) received in the receiving device (46). A transfer device (54) is adapted to transfer the sealing element (48) between an inactive state, in which the sealing element (48) is shaped and/or positioned such that it cannot be brought into sealing contact with a sealing surface (64), and an active state, in which the sealing element (48) is shaped and/or positioned such that it can be brought into sealing contact with the sealing surface (64).
摘要翻译： 一种用于飞机设备中以便与环境密封的密封系统（38）包括关闭元件（40），其能够连接到飞行器设备的壳体（42），以便密封形成在其中的开口（44） 飞机设备的壳体（42）。 此外，密封系统（38）包括接收装置（46）和容纳在接收装置（46）中的密封元件（48）。 传送装置（54）适于将密封元件（48）转移到其中密封元件（48）被成形和/或定位成不能与密封表面（64）密封接触的非活动状态 ）和活动状态，其中密封元件（48）成形和/或定位成使得其能够与密封表面（64）密封接触。
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10.发明授权Aircraft signal computer system having a plurality of modular signal computer units 有权具有多个模块化信号计算机单元的飞行器信号计算机系统公开(公告)号：US08508934B2
公开(公告)日：2013-08-13
申请号：US13059528
申请日：2009-08-13
申请人： Sebastian Roering
发明人： Sebastian Roering
IPC分类号： H05K7/20
CPC分类号： H05K7/20645 , G06F1/20 , G06F2200/201
摘要： An aircraft signal computer system includes a plurality of modular signal computer units and a liquid cooling device for cooling the modular signal computer units. The liquid cooling device includes a coolant line, which is connectable to a central liquid cooling system of an aircraft in order to supply a liquid coolant medium at a desired low temperature to the liquid cooling device. The coolant line of the liquid cooling device is in thermal surface contact with the modular signal computer units in order to dissipate heat from the modular signal computer units. A heat-emitting component of the modular signal computer units may be in thermal contact with a coolant bath or an internal heat conductor for removing heat energy.
摘要翻译： 飞行器信号计算机系统包括多个模块化信号计算机单元和用于冷却模块化信号计算机单元的液体冷却装置。 液体冷却装置包括冷却剂管线，冷却剂管线可连接到飞行器的中央液体冷却系统，以便将液体冷却剂介质以期望的低温供应到液体冷却装置。 液体冷却装置的冷却剂管线与模块化信号计算机单元热表面接触以便散发来自模块化信号计算机单元的热量。 模块化信号计算机单元的发热部件可以与冷却剂浴或用于去除热能的内部热导体热接触。
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