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1. 发明授权

US08480028B2 Optimized defrosting regulation of parallel arranged fresh air outlets of air conditioners 有权
标题翻译：优化空调平行布置的新鲜空气出口的除霜调节
公开(公告)号：US08480028B2
公开(公告)日：2013-07-09
申请号：US13460505
申请日：2012-04-30
申请人： Juergen Kelnhofer , Dariusz Krakowski , Jose-Javier Francisco-Palomares
发明人： Juergen Kelnhofer , Dariusz Krakowski , Jose-Javier Francisco-Palomares
IPC分类号： B64D11/00
CPC分类号： B64D13/06 , B64D2013/064 , Y10T137/0324
摘要： An arrangement is provided for de-icing pipeline connections of an aircraft, which are connected to all fresh air outlets of an air conditioner, whose construction includes, but is not limited to the functions of multiple turbines and heat exchangers, having a first pipeline, which is connected to a first turbine, and a second pipeline, which is connected to a second turbine, the two pipelines, which are each connected downstream from the two turbines and to which process air is fed at the turbine outlets, being connected at the pipe ends and being continued using a third pipeline. The arrangement is characterized in that a first hot air source is fed hot fresh air from a bleed air system of the aircraft and is connected at its outlet to a fourth pipeline, into which temperature-reduced fresh air is fed from the hot air source. The fourth pipeline is connected at its pipe end to two further valve-regulated pipelines, of which a fifth or a sixth pipeline is connected to the first or the second pipeline, and through which temperature-reduced fresh air is transported and fed valve-regulated to the first and/or second pipeline.
摘要翻译：提供了一种用于除冰空气调节器的所有新鲜空气出口连接的飞行器的管道连接的装置，其结构包括但不限于具有第一管道的多个涡轮机和热交换器的功能，连接到第一涡轮机的第二管道和连接到第二涡轮机的第二管道，两个管道各自连接在两个涡轮机的下游，并且在涡轮机出口处被供给到处理空气，其连接在管道末端并继续使用第三个管道。该装置的特征在于，第一热空气源从飞行器的放气系统供给热的新鲜空气，并在其出口处连接到第四管道，从热空气源供给减温的新鲜空气。第四条管道在其管端连接到两个另外的阀门调节管道，其中第五或第六管道连接到第一或第二管道，通过该管道将减温的新鲜空气输送并进行阀门调节到第一和/或第二管道。

2. 发明授权

US09321535B2 System and process for cooling an aircraft zone using an aircraft-external air assembly 有权
标题翻译：使用飞机 - 外部空气组件冷却飞机区域的系统和过程
公开(公告)号：US09321535B2
公开(公告)日：2016-04-26
申请号：US13203386
申请日：2010-02-18
申请人： Dariusz Krakowski , Stefan Gumm , Juergen Kelnhofer
发明人： Dariusz Krakowski , Stefan Gumm , Juergen Kelnhofer
IPC分类号： B64D13/06 , B64D13/00 , B64F1/36
CPC分类号： B64D13/00 , B64F1/364 , Y02T50/44 , Y02T50/56
摘要： A system for cooling an aircraft zone includes a mixing chamber which is connected to an air-conditioning assembly for making cool air available and/or to a recirculated-air conveying device for supplying recirculated air into the mixing chamber. The system further includes an aircraft-side air-distribution system which includes at least one line connecting the mixing chamber to the aircraft zone to be cooled and also at least one line that is connectable to an aircraft-external air-generating assembly in order to route air made available by the aircraft-external air-generating assembly into the aircraft-side air-distribution system.
摘要翻译：用于冷却飞机区域的系统包括混合室，该混合室连接到用于制造可用冷空气的空调组件和/或连接到用于将再循环空气供应到混合室中的再循环空气输送装置。该系统还包括飞行器侧空气分配系统，其包括将混合室连接到要冷却的飞行器区域的至少一条线路，还包括可连接到飞行器 - 外部发电组件的至少一条线路，以便将飞机外部发电组件提供的航空空气送入飞行器侧空气分配系统。

3. 发明授权

US09090350B2 System for cooling an aircraft zone, to be connected to an aircraft-external air unit 有权
标题翻译：用于冷却飞机区域的系统，连接到飞机 - 外部空气单元
公开(公告)号：US09090350B2
公开(公告)日：2015-07-28
申请号：US13002825
申请日：2009-07-07
申请人： Juergen Kelnhofer , Dariusz Krakowski
发明人： Juergen Kelnhofer , Dariusz Krakowski
IPC分类号： B64D13/06 , B64D13/00 , B64F1/36
CPC分类号： B64D13/00 , B64F1/364 , Y02T50/44 , Y02T50/56 , Y02T50/82
摘要： A system for cooling an aircraft region includes an air-conditioning unit for providing cool air, a circulating air conveying device, and a mixing chamber which is connected to the air conditioning unit via an air distribution line and to which circulating air can be fed by the circulating air conveying device. An inlet line which is connected to an aircraft-side connection for an aircraft-external air unit opens into the air distribution line connecting the air conditioning unit to the mixing chamber. Therefore, air flows from the aircraft-external air unit and air flow from the air-conditioning unit are simultaneously provided to the mixing unit and then to the aircraft region.
摘要翻译：用于冷却航空器区域的系统包括用于提供冷空气的空调单元，循环空气输送装置和混合室，其经由空气分配管线连接到空调单元，循环空气可以通过循环空气输送装置。连接到用于飞行器 - 外部空气单元的飞行器侧连接的入口管线通向将空调单元连接到混合室的空气分配管线。因此，从飞机 - 外部空气单元流出的空气和来自空调单元的空气流同时被提供给混合单元，然后提供给飞行器区域。

4. 发明申请

US20110177771A1 System For Cooling An Aircraft Zone, To Be Connected To An Aircraft-External Air Unit 有权
标题翻译：用于冷却飞机区域的系统，连接到飞机 - 外部空气单元
公开(公告)号：US20110177771A1
公开(公告)日：2011-07-21
申请号：US13002825
申请日：2009-07-07
申请人： Juergen Kelnhofer , Dariusz Krakowski
发明人： Juergen Kelnhofer , Dariusz Krakowski
IPC分类号： B64D13/06
CPC分类号： B64D13/00 , B64F1/364 , Y02T50/44 , Y02T50/56 , Y02T50/82
摘要： A system (10) for cooling an aircraft region comprises an air-conditioning unit (12a, 12b) for providing cool air, a circulating air conveying device (20a, 20b), and a mixing chamber (18) which is connected to the air conditioning unit (12a, 12b) via an air distribution line (16a, 16b) and to which circulating air can be fed by the circulating air conveying device (20a, 20b). An inlet line (28a, 28b) which is connected to an aircraft-side connection (24a, 24b, 24c, 24d) for an aircraft-external air unit (26a, 26b, 26c, 26d) opens into the air distribution line (16a, 16b) connecting the air conditioning unit (12a, 12b) to the mixing chamber (18).
摘要翻译：用于冷却航空器区域的系统（10）包括用于提供冷空气的空调单元（12a，12b），循环空气输送装置（20a，20b）和连接到空气的混合室（18）经由空气分配管线（16a，16b）经由循环空气输送装置（20a，20b）供给循环空气的空调单元（12a，12b）。连接到飞机 - 外部空气单元（26a，26b，26c，26d）的飞行器侧连接部（24a，24b，24c，24d）的入口管线（28a，28b）通向空气分配管线，16b）将空调单元（12a，12b）连接到混合室（18）。

5. 发明申请

US20120064816A1 System and process for cooling an aircraft zone using an aircraft-external air assembly 有权
标题翻译：使用飞机 - 外部空气组件冷却飞机区域的系统和过程
公开(公告)号：US20120064816A1
公开(公告)日：2012-03-15
申请号：US13203386
申请日：2010-02-18
申请人： Dariusz Krakowski , Stefan Gumm , Juergen Kelnhofer
发明人： Dariusz Krakowski , Stefan Gumm , Juergen Kelnhofer
IPC分类号： B64D13/06
CPC分类号： B64D13/00 , B64F1/364 , Y02T50/44 , Y02T50/56
摘要： A system for cooling an aircraft zone includes a mixing chamber (18) which is connected to an air-conditioning assembly (12a, 12b) for making cool air available and/or to a recirculated-air conveying device (20a, 20b) for supplying recirculated air into the mixing chamber (18). The system (10) further includes an aircraft-side air-distribution system (23) which includes at least one line (32) connecting the mixing chamber (18) to the aircraft zone to be cooled and also at least one line (28a, 28b) that is connectable to an aircraft-external air-generating assembly (26a, 26b, 26c, 26d) in order to route air made available by the aircraft-external air-generating assembly (26a, 26b, 26c, 26d) into the aircraft-side air-distribution system (23). The system (10) further includes a detection device (34) for detecting a parameter indicating an operating state in the aircraft-side air-distribution system (23) and/or in the mixing chamber (18) and also a control unit (42) which is set up to receive and evaluate signals made available by the detection device (34) and, when the system (10) is connected to the aircraft-external air-generating assembly (26a, 26b, 26c, 26d), to control the operation of the aircraft-external air-generating assembly (26a, 26b, 26c, 26d) in a manner depending on the signals made available by the detection device (34).
摘要翻译：用于冷却飞机区域的系统包括混合室（18），其连接到用于制造冷空气的空调组件（12a，12b）和/或连接到用于供应的再循环空气输送装置（20a，20b）再循环的空气进入混合室（18）。该系统（10）还包括飞行器侧空气分配系统（23），其包括将混合室（18）连接到要冷却的飞行器区域的至少一条线路（32），还包括至少一条线路（28a， 28b），其可连接到飞行器 - 外部产生组件（26a，26b，26c，26d），以便将由飞行器 - 外部产生组件（26a，26b，26c，26d）可用的空气路由到飞机侧配气系统（23）。该系统（10）还包括检测装置（34），用于检测指示飞行器侧空气分配系统（23）和/或混合室（18）中的操作状态的参数以及控制单元（42）），其被设置为接收和评估由检测装置（34）可用的信号，并且当系统（10）连接到飞行器 - 外部产生组件（26a，26b，26c，26d）时，以控制以与取决于检测装置（34）可用的信号的方式对飞机 - 外部产生组件（26a，26b，26c，26d）进行操作。

6. 发明申请

US20110247432A1 Aircraft Conduit Monitoring System And Method 有权
标题翻译：飞机管道监控系统及方法
公开(公告)号：US20110247432A1
公开(公告)日：2011-10-13
申请号：US12999752
申请日：2009-06-17
申请人： Juergen Kelnhofer , Dariusz Krakowski
发明人： Juergen Kelnhofer , Dariusz Krakowski
IPC分类号： G01F1/80 , B64D13/00 , B64D15/02
CPC分类号： B64D15/02 , B64D13/00 , G01M3/2815 , Y02T50/44
摘要： The invention relates to an aircraft conduit monitoring system comprising a conduit that conducts gas from a source to a point of application. A flow sensing device and a pressure sensing device are provided within the conduit. At least one set value of a gas mass flow rate and at least one set value of a pressure are sensed in a learning mode of operation. Said set values are compared with sensed actual values in the normal mode of operation. A gas volume flow rate can also be sensed and processed instead of a gas mass flow rate.
摘要翻译：本发明涉及一种飞机管道监测系统，其包括将气体从源极传导到施加点的导管。在导管内提供流量检测装置和压力感测装置。在学习操作模式中感测至少一个气体质量流量的设定值和至少一个压力设定值。将所述设定值与正常操作模式下的感测实际值进行比较。也可以感测和处理气体体积流量而不是气体质量流量。

7. 发明授权

US09221543B2 Compressor/turbine arrangement, air conditioning unit and method for operating a compressor/turbine arrangement 有权
标题翻译：压缩机/涡轮机布置，空调单元以及用于操作压缩机/涡轮机装置的方法
公开(公告)号：US09221543B2
公开(公告)日：2015-12-29
申请号：US13639624
申请日：2011-04-05
申请人： Juergen Kelnhofer
发明人： Juergen Kelnhofer
IPC分类号： B60H1/32 , F25D17/02 , F25D9/00 , F25D17/04 , B64D13/08 , F25B11/00 , B64D13/06 , B60H1/00
CPC分类号： B64D13/08 , B60H1/00021 , B60H1/00028 , B60H2001/00092 , B60H2001/0015 , B64D13/06 , B64D2013/0688 , F25B11/00 , Y02T50/44
摘要： The invention relates to a compressor/turbine arrangement for use in an air conditioning unit of an aircraft air conditioning system comprising a process air supply line which is designed to supply process air generated by a process air source to a compressor. A detection device is designed to detect a characteristic signal for the temperature of the process air flowing through the process air supply line. A turbine is designed to drive the compressor. A cooling device is disposed in a process air line connecting the compressor to the turbine and is designed to cool the process air coming out of the compressor and flowing through the process air line in the direction of the turbine. Downstream of the cooling device a connecting line branches off from the process air line and opens into the process air supply line. A control device is designed to control a process air flow through the connecting line in dependence on the signal detected by the detection device.
摘要翻译：本发明涉及一种用于飞机空调系统的空调单元中的压缩机/涡轮机装置，其包括工艺空气供应管线，其被设计成将由处理空气源产生的过程空气提供给压缩机。检测装置被设计为检测流过过程空气供应管线的处理空气的温度的特征信号。涡轮机设计用于驱动压缩机。冷却装置设置在将压缩机连接到涡轮机的处理空气管线中，并被设计成冷却从压缩机出来的工艺空气并沿着涡轮机的方向流过工艺空气管线。在冷却装置的下游，连接线从处理空气管线分支并且打开到过程空气供应管线。控制装置被设计成根据由检测装置检测到的信号来控制通过连接线的处理空气流。

8. 发明申请

US20130067945A1 COMPRESSOR/TURBINE ARRANGEMENT, AIR CONDITIONING UNIT AND METHOD FOR OPERATING A COMPRESSOR/TURBINE ARRANGEMENT 有权
标题翻译：压缩机/涡轮机布置，空调单元和压缩机/涡轮机装置的运行方法
公开(公告)号：US20130067945A1
公开(公告)日：2013-03-21
申请号：US13639624
申请日：2011-04-05
申请人： Juergen Kelnhofer
发明人： Juergen Kelnhofer
IPC分类号： B64D13/08
CPC分类号： B64D13/08 , B60H1/00021 , B60H1/00028 , B60H2001/00092 , B60H2001/0015 , B64D13/06 , B64D2013/0688 , F25B11/00 , Y02T50/44
摘要： The invention relates to a compressor/turbine arrangement for use in an air conditioning unit of an aircraft air conditioning system comprising a process air supply line which is designed to supply process air generated by a process air source to a compressor. A detection device is designed to detect a characteristic signal for the temperature of the process air flowing through the process air supply line. A turbine is designed to drive the compressor. A cooling device is disposed in a process air line connecting the compressor to the turbine and is designed to cool the process air coming out of the compressor and flowing through the process air line in the direction of the turbine. Downstream of the cooling device a connecting line branches off from the process air line and opens into the process air supply line. A control device is designed to control a process air flow through the connecting line in dependence on the signal detected by the detection device.
摘要翻译：本发明涉及一种用于飞机空调系统的空调单元中的压缩机/涡轮机装置，其包括工艺空气供应管线，其被设计成将由处理空气源产生的过程空气提供给压缩机。检测装置被设计为检测流过过程空气供应管线的处理空气的温度的特征信号。涡轮机设计用于驱动压缩机。冷却装置设置在将压缩机连接到涡轮机的处理空气管线中，并被设计成冷却从压缩机出来的工艺空气并沿着涡轮机的方向流过工艺空气管线。在冷却装置的下游，连接线从处理空气管线分支并且打开到过程空气供应管线。控制装置被设计成根据由检测装置检测到的信号来控制通过连接线的处理空气流。

9. 发明申请

US20090095004A1 SYSTEM FOR PRODUCING AIR 有权
标题翻译：生产空气的系统
公开(公告)号：US20090095004A1
公开(公告)日：2009-04-16
申请号：US11573531
申请日：2005-08-10
申请人： Juergen Kelnhofer , Thomas Scherer
发明人： Juergen Kelnhofer , Thomas Scherer
IPC分类号： B60H1/32 , F25B39/02 , B64D13/08
CPC分类号： B64D13/02 , B64D13/06 , B64D2013/0677 , F28D2021/0021 , Y02T50/44
摘要： A system for the provision of process air comprises a first cooling system (2) with a first heat exchanger, which is arranged in a channel (3) that serves as a cooling sink, and a cooling system (8), integrated in the first cooling system (2), wherein said cooling system (8) comprises a heat exchanger (9) which is integrated in the channel (3) either upstream or downstream of the first heat exchanger.
摘要翻译：一种用于提供处理空气的系统包括具有第一热交换器的第一冷却系统（2），其布置在用作冷却槽的通道（3）中，以及冷却系统（8），其集成在第一冷却系统（2），其中所述冷却系统（8）包括在第一热交换器的上游或下游集成在通道（3）中的热交换器（9）。

10. 发明授权

US09284057B2 System for cooling a heat exchanger on board an aircraft 有权
标题翻译：用于冷却飞机上的热交换器的系统
公开(公告)号：US09284057B2
公开(公告)日：2016-03-15
申请号：US13125728
申请日：2009-10-26
申请人： Juergen Kelnhofer
发明人： Juergen Kelnhofer
IPC分类号： B64D13/08 , B64D13/06
CPC分类号： B64D13/06 , B64D13/08 , B64D2013/0618 , Y02T50/44 , Y02T50/56
摘要： A system for cooling a heat exchanger on board an aircraft includes an engine bleed air line connected to an engine of the aircraft and adapted to supply engine bleed air to the heat exchanger. The system further includes a process air line branching off from the engine bleed air line such that the engine bleed air is supplied to the process air line and connecting to an input side of a turbine. The system also includes a cooling air line connected to an output side of the turbine such that cooling air produced by an expansion of the engine bleed air supplied to the turbine is supplied to the cooling air line and then to the heat exchanger. The heat exchanger is adapted to transfer cooling energy from the cooling air to the engine bleed air supplied to the heat exchanger from the engine bleed air line.
摘要翻译：用于冷却飞机上的热交换器的系统包括连接到飞行器的发动机并适于向发热体提供引擎排放空气的发动机排放空气管线。该系统还包括从发动机排气管线分支的工艺空气管线，使得发动机排放空气被供应到处理空气管线并连接到涡轮机的输入侧。该系统还包括连接到涡轮的输出侧的冷却空气管线，使得通过供应到涡轮机的发动机放气的膨胀产生的冷却空气被供应到冷却空气管路，然后被供应到热交换器。热交换器适于将冷却能量从冷却空气传递到从发动机排气管线供应到热交换器的发动机排放空气。

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