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。

公开(公告)号：US20130074530A1

公开(公告)日：2013-03-28

申请号：US13428050

申请日：2012-03-23

申请人： Markus Piesker ,  Ahmet Kayihan Kiryaman ,  Sebastian Roering

发明人： Markus Piesker ,  Ahmet Kayihan Kiryaman ,  Sebastian Roering

IPC分类号： F25B41/00 ,  F25B1/00

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。

公开(公告)号：US08721406B2

公开(公告)日：2014-05-13

申请号：US13001353

申请日：2009-06-23

申请人： Dirk Kastell ,  Sebastian Roering ,  Wilson Willy Casas Noriega

发明人： Dirk Kastell ,  Sebastian Roering ,  Wilson Willy Casas Noriega

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。

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

IPC分类号： E06B7/20 ,  A47F3/04

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。

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。

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

CPC分类号： B64D13/08 ,  B64D13/00 ,  B64D2013/0655 ,  F25B49/02 ,  Y02T50/44 ,  Y02T50/56

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。

公开(公告)号：US08713950B2

公开(公告)日：2014-05-06

申请号：US12718631

申请日：2010-03-05

申请人： Sebastian Roering

发明人： Sebastian Roering

IPC分类号： F25B7/00

CPC分类号： F25D17/02 ,  B64D13/06 ,  B64D2013/0674 ,  F25B45/00 ,  F25B2309/06 ,  Y02T50/44 ,  Y02T50/56

摘要： In a method of the application, cooling energy is produced by a refrigerating device. The cooling energy produced by the refrigerating device is supplied to at least one cooling station by a cooling circuit, circulating in which is a refrigerant, which upon release of its cooling energy to the at least one cooling station is converted from the liquid to the gaseous state and is then converted back to the liquid state by corresponding pressure- and temperature control in the cooling circuit. Upon transfer of the cooling system to its state of rest, a control value disposed in the cooling circuit is controlled in such a way that a desired operating pressure (ρβ) arises in the cooling circuit downstream of the control valve. Refrigerant cooled by the refrigerating device is received in a reservoir disposed upstream of the control valve in the cooling circuit.

摘要翻译： 在应用的方法中，冷却能量由制冷装置产生。 由制冷装置产生的冷却能量通过冷却回路供给到至少一个冷却站，该冷却回路循环成为制冷剂，在将冷却能量释放到至少一个冷却站的冷却能量从液体转化为气态 状态，然后通过冷却回路中相应的压力和温度控制转换回液态。 在将冷却系统转移到其休止状态时，设置在冷却回路中的控制值被控制为在控制阀下游的冷却回路中产生期望的操作压力（＆amp; rgr。）。 由制冷装置冷却的制冷剂被容纳在设置在冷却回路中的控制阀的上游的储存器中。

公开(公告)号：US20100251737A1

公开(公告)日：2010-10-07

申请号：US12718631

申请日：2010-03-05

申请人： Sebastian Roering

发明人： Sebastian Roering

IPC分类号： F25B1/00

CPC分类号： F25D17/02 ,  B64D13/06 ,  B64D2013/0674 ,  F25B45/00 ,  F25B2309/06 ,  Y02T50/44 ,  Y02T50/56

摘要： In a method of operating a cooling system (10) that is suitable in particular for cooling food on board an aircraft, cooling energy is produced by means of a refrigerating device (12). The cooling energy produced by the refrigerating device (12) is supplied to at least one cooling station (14) by means of a cooling circuit (16), circulating in which is a refrigerant, which upon release of its cooling energy to the at least one cooling station (14) is converted from the liquid to the gaseous state and is then converted back to the liquid state by means of corresponding pressure- and temperature control in the cooling circuit (16). Upon transfer of the cooling system (10) to its state of rest, a control valve (44) disposed in the cooling circuit (16) is controlled in such a way that a desired operating pressure (pB) arises in the cooling circuit (16) downstream of the control valve (44). Refrigerant cooled by the refrigerating device (12) is received in a reservoir (30) disposed upstream of the control valve (44) in the cooling circuit (16).

摘要翻译： 在特别适用于冷却飞机上的食物冷却的冷却系统（10）的操作方法中，通过制冷装置（12）产生冷却能。 由制冷装置（12）产生的冷却能量通过冷却回路（16）被供给至少一个冷却站（14），循环冷却装置（16），其中制冷剂是将其冷却能量释放到至少 一个冷却站（14）从液体转变为气态，然后通过冷却回路（16）中相应的压力和温度控制转换回液态。 在将冷却系统（10）转移到其休止状态时，设置在冷却回路（16）中的控制阀（44）被控制成使得在冷却回路（16）中产生期望的工作压力（pB） ）控制阀（44）的下游。 由制冷装置（12）冷却的制冷剂被容纳在设置在冷却回路（16）内的控制阀（44）上游的贮存器（30）中。

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

IPC分类号： G05B13/00 ,  B64D13/08 ,  B64D13/00 ,  B60H1/00 ,  F25B29/00 ,  F28F13/00 ,  B64D13/06

CPC分类号： B64D13/08 ,  B64D13/00 ,  B64D2013/0655 ,  F25B49/02 ,  Y02T50/44 ,  Y02T50/56

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.

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

IPC分类号： B64D13/08 ,  B64D13/00 ,  B64D13/06

CPC分类号： B64D13/08 ,  B64D13/00 ,  B64D2013/0655 ,  F25B49/02 ,  Y02T50/44 ,  Y02T50/56

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。