专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 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）。

2. 发明授权

US06415621B2 Aircraft air conditioning system providing auxiliary ventilation 有权
标题翻译：飞机空调系统提供辅助通风
公开(公告)号：US06415621B2
公开(公告)日：2002-07-09
申请号：US09795230
申请日：2001-02-27
申请人： Uwe Buchholz , Juergen Kelnhofer , Thomas Scherer
发明人： Uwe Buchholz , Juergen Kelnhofer , Thomas Scherer
IPC分类号： F25D900
CPC分类号： B64D13/06 , F05B2220/50 , F25B9/004 , Y02T50/56
摘要： An air conditioning system for an aircraft includes a first rotatable shaft with a first compressor, a first turbine, a cooling air fan, and an auxiliary compressor connected for rotation therewith, and preferably further includes a second rotatable shaft with a second compressor and a second turbine connected for rotation therewith. A compression, cooling, and expansion cycle driven by at least the first compressor and the first turbine provides a principle flow of air conditioning air. The auxiliary compressor draws in outside air and provides a redundant auxiliary ventilation air flow, which is supplied into the installation space in which the air conditioning unit is installed, or another space in the aircraft that requires a reliable constant ventilation and cooling whenever the air conditioning unit is operational. The auxiliary ventilation air may be connected to a common air distribution network with other air conditioning units.
摘要翻译：一种用于飞机的空调系统包括具有第一压缩机的第一可旋转轴，第一涡轮机，冷却空气风扇和连接用于与其一起旋转的辅助压缩机，并且优选地还包括具有第二压缩机的第二可旋转轴和第二压缩机涡轮连接以便与其一起旋转。由至少第一压缩机和第一涡轮机驱动的压缩，冷却和膨胀循环提供空调空气的主要流动。辅助压缩机吸入外部空气，并且提供冗余的辅助通风空气流，其被供应到安装有空调单元的安装空间中，或者在飞机中的另一空间需要可靠的恒定的通风和冷却，每当空调单位运作。辅助通风空气可以与其他空调单元连接到公共空气分配网络。

3. 发明授权

US07922118B2 System for producing process air 有权
标题翻译：生产工艺空气的系统
公开(公告)号：US07922118B2
公开(公告)日：2011-04-12
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： B64D11/00
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）。

4. 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。

5. 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。

6. 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。

7. 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。

8. 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）。

9. 发明申请

US20110111683A1 System For Ventilation Of An Aircraft Area 有权
标题翻译：飞机区通风系统
公开(公告)号：US20110111683A1
公开(公告)日：2011-05-12
申请号：US12995281
申请日：2009-05-06
申请人： Juergen Kelnhofer
发明人： Juergen Kelnhofer
IPC分类号： B61D27/00
CPC分类号： B64D13/00 , B64D13/006 , Y02T50/44 , Y02T50/56
摘要： A system (10) for ventilation of an aircraft area (32, 34) comprises a ram-air duct (12) with an air inlet (14), a first ram-air duct branch (16) and a second ram-air duct branch (18) allowing for being flowed parallel to the first ram-air duct branch (16). A supply line (26) connected to the ram-air duct (12) is adapted to supply air flowing through the ram-air duct (12) to the aircraft area (32, 34) to be ventilated. In the first ram-air duct branch (16) a conveying device (24) is arranged. In the second ram-air duct branch (18) a heat exchanger (36) of an aircraft system to be supplied with cooling energy is arranged.
摘要翻译：用于飞机区域（32,34）的通风的系统（10）包括具有空气入口（14）的冲压空气管道（12），第一冲压空气管道分支（16）和第二压缩空气导管分支（18）允许平行于第一压缩空气管道分支（16）流动。连接到冲压空气管道（12）的供应管线（26）适于将流过冲压空气管道（12）的空气供应到飞机区域（32,34）以通风。在第一压缩空气管道分支（16）中布置有输送装置（24）。在第二压缩空气管道分支（18）中布置有要供应冷却能量的飞行器系统的热交换器（36）。

10. 发明申请

US20100101251A1 Method And System For Controlling An Aircraft Air Conditioning System With Optimised Fuel Consumption 有权
标题翻译：控制具有优化燃料消耗的飞机空调系统的方法和系统
公开(公告)号：US20100101251A1
公开(公告)日：2010-04-29
申请号：US12582850
申请日：2009-10-21
申请人： Juergen Kelnhofer
发明人： Juergen Kelnhofer
IPC分类号： B60H1/32
CPC分类号： B64D13/06 , B64D2013/0618 , B64D2013/0688 , Y02T50/56
摘要： In a method for controlling an aircraft air conditioning system (10) a correlation is established between a plurality of values of a process air mass flow supplyable to an air conditioning unit (12) of the aircraft air conditioning system (10) and the fuel consumption of the aircraft. A correlation is also established between a plurality of values of an ambient air mass flow which is used to cool the process air mass flow supplyable to the air conditioning unit (12) of the aircraft air conditioning system (10) and the fuel consumption of the aircraft. The process air mass flow and the ambient air mass flow are controlled in dependence on a predetermined cooling capacity of the aircraft air conditioning system (10) such that the fuel consumption of the aircraft is minimised.
摘要翻译：在一种用于控制飞行器空调系统（10）的方法中，建立了可供给飞机空调系统（10）的空调单元（12）的过程空气质量流的多个值与燃料消耗之间的相关性的飞机。在用于冷却可供给飞机空调系统（10）的空调单元（12）的过程空气质量流量的多个环境空气质量流的值与燃料消耗量之间也存在相关性飞机。根据飞机空调系统（10）的预定冷却能力来控制过程空气质量流量和环境空气质量流量，使得飞机的燃料消耗最小化。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式