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1. 发明授权

US08132737B2 Aircraft air-conditioning system for an aircraft cabin having a plurality of zones 有权
标题翻译：具有多个区域的飞机机舱的飞机空调系统
公开(公告)号：US08132737B2
公开(公告)日：2012-03-13
申请号：US12014330
申请日：2008-01-15
申请人： Johannes Eichholz , Torsten Schwan
发明人： Johannes Eichholz , Torsten Schwan
IPC分类号： F24D19/10 , F24F11/00 , G05D23/275
CPC分类号： B64D13/00 , B64D2013/0625
摘要： An air-conditioning system and associated method for air-conditioning an aircraft cabin including a first zone and a second zone of variable length and at least one intermediate zone is provided. The intermediate zone is selectively associated with the first zone or the second zone. Air at a first set temperature is supplied to the first zone, and air at a second set temperature is supplied to the second zone. Likewise, air at a third set temperature is supplied to the intermediate zone. A regulating device regulates the third set temperature such that if the intermediate zone is associated with the first zone, the third set temperature corresponds substantially to the first set temperature; but if the intermediate zone is associated with the second zone, the third set temperature.
摘要翻译：提供一种空调系统和相关联的方法，用于对包括第一区域和可变长度的第二区域以及至少一个中间区域的飞机机舱进行空调。中间区域选择性地与第一区域或第二区域相关联。将第一设定温度的空气供给到第一区域，将第二设定温度的空气供给到第二区域。同样地，将第三设定温度的空气供给到中间区域。调节装置调节第三设定温度，使得如果中间区域与第一区域相关联，则第三设定温度基本上对应于第一设定温度; 但是如果中间区域与第二区域相关联，则为第三设定温度。

2. 发明授权

US08336609B2 Method for controlling the feed air temperature of a passenger aircraft 有权
标题翻译：控制客机进给空气温度的方法
公开(公告)号：US08336609B2
公开(公告)日：2012-12-25
申请号：US10580944
申请日：2004-12-30
申请人： Torsten Schwan , Michael Markwart
发明人： Torsten Schwan , Michael Markwart
IPC分类号： B60H1/00 , G05D23/00
CPC分类号： B64D13/00 , B64D2013/0655
摘要： A passenger aircraft includes a cabin subdivided into a plurality of cabin zones supplied with feed air from respective supply lines, a plurality of temperature sensors, and an electronic control unit coupled to the plurality of temperature sensors. The plurality of temperature sensors measures a plurality of individual ambient temperature values associated with different locations in at least one of the plurality of cabin zones. The electronic control unit derives a derived ambient temperature value for the at least one cabin zone from the plurality of individual ambient temperature values. The electronic control unit then controls a temperature of the feed air supplied to the at least one cabin zone based on the difference between the derived ambient temperature value and a room temperature target value for the at least one cabin zone.
摘要翻译：客机包括被分为多个舱区的舱室，其中多个舱区域供应有来自各供应管线的进料空气，多个温度传感器和耦合到多个温度传感器的电子控制单元。多个温度传感器测量与多个舱区中的至少一个中的不同位置相关联的多个独立环境温度值。电子控制单元从多个单独的环境温度值中导出至少一个客舱区域的导出的环境温度值。电子控制单元然后基于导出的环境温度值和至少一个客舱区域的室温目标值之间的差来控制供应到至少一个客舱区域的进料空气的温度。

3. 发明申请

US20080168786A1 Flexible Aircraft Air-Conditioning System For A Flexible Aircraft Cabin 有权
标题翻译：柔性飞机机舱柔性飞机空调系统
公开(公告)号：US20080168786A1
公开(公告)日：2008-07-17
申请号：US12014330
申请日：2008-01-15
申请人： Johannes Eichholz , Torsten Schwan
发明人： Johannes Eichholz , Torsten Schwan
IPC分类号： F25B41/00
CPC分类号： B64D13/00 , B64D2013/0625
摘要： Flexible aircraft air-conditioning system for a flexible aircraft cabin The invention relates to a method and a device for air-conditioning an aircraft cabin, which comprises a first zone and a second zone of variable length and at least one intermediate zone. The at least one intermediate zone may be associated with the lo first zone or the second zone. Air at a first set temperature is supplied to the first zone (6a) via a first supply line (10a). Air at a second set temperature is supplied to the second zone (6b) via a second supply line (10b). In at least one intermediate zone (6c) air is supplied via an intermediate zone supply line (10c) associated therewith. If the at least one intermediate zone (6c) is associated with the first zone is (6a), the set temperature of the air supplied to the intermediate zone (6c) corresponds substantially to the set temperature of the air supplied to the first zone (6a). If the at least one intermediate zone (6c) is associated with the second zone (6b), the set temperature of the air supplied to the intermediate zone (6c) corresponds substantially to the set temperature of the air supplied to the second zone (6b).
摘要翻译：用于柔性飞机机舱的柔性飞机空调系统技术领域本发明涉及一种用于空调飞机机舱的方法和装置，其包括第一区域和可变长度的第二区域以及至少一个中间区域。该至少一个中间区域可以与第一区域或第二区域相关联。第一设定温度的空气通过第一供应管线（10a）供应到第一区域（6a）。第二设定温度的空气通过第二供应管线（10b）供应到第二区域（6b）。在至少一个中间区域（6c）中，通过与其相关联的中间区域供应管线（10c）供应空气。如果至少一个中间区域（6c）与第一区域相关联（6a），则供应到中间区域（6c）的空气的设定温度基本上对应于供应给第一区（6a）。如果至少一个中间区域（6c）与第二区域（6b）相关联，则供应到中间区域（6c）的空气的设定温度基本上对应于供应到第二区域（6a）的空气的设定温度区域（6b）。

4. 发明申请

US20070144726A1 Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft 有权
标题翻译：用于控制喷射到客机的客舱区域中的进料空气的温度的方法
公开(公告)号：US20070144726A1
公开(公告)日：2007-06-28
申请号：US10582595
申请日：2004-12-30
申请人： Thomas Scherer , Michael Markwart , Torsten Schwan
发明人： Thomas Scherer , Michael Markwart , Torsten Schwan
IPC分类号： F24D19/10 , B60H1/00
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y10S62/05
摘要： With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controlled feed air, the temperature of the injected feed air is controlled for each cabin zone, dependent upon the deviation of an injection temperature actual value for the feed air injected into the cabin zone in question, measured by sensors, in relation to an injection temperature optimum value. If there is no, or at least no usable reading of the ambient temperature of this cabin zone for a cabin zone, an optimum value for the injection temperature of this cabin zone can be established in accordance with a variation, whereby it is determined upon the basis of the injection temperature optimum values and/or the injection temperature actual values of other cabin zones, whereby the measurement by sensors of the cabin temperature works reliably. In accordance with another variation, the injection temperature optimum value of a cabin zone can be established without measuring ambient temperature by sensors or without reliably measuring ambient temperature from the temperature measured for the external surrounds of the aircraft.
摘要翻译：使用一种用于控制喷射到客机的客舱区域中的进料空气的温度的方法，其将舱室分成几个舱区，分别提供特别温度控制的进料空气，喷射进料的温度根据喷射温度最佳值，根据传感器测量的注入到所述舱室区域的进料空气的喷射温度实际值的偏差，对每个舱室进行空气控制。如果对于客舱区域没有或至少没有可用的该舱室区域的环境温度读数，则可以根据变化确定该舱区域的喷射温度的最佳值，由此根据喷射温度最佳值和/或其他舱区的喷射温度实际值的基础，由此由客舱温度的传感器进行的测量可靠地工作。根据另一个变化，可以建立客舱区域的喷射温度最佳值，而不需要通过传感器测量环境温度，或者不会从对飞行器的外部环境测量的温度可靠地测量环境温度。

5. 发明申请

US20100267323A1 Method For Controlling The Temperature Of Feed Air Injected Into The Cabin Zone Of A Passenger Aircraft 有权
标题翻译：用于控制进入客机客舱区域的进料空气温度的方法
公开(公告)号：US20100267323A1
公开(公告)日：2010-10-21
申请号：US12824898
申请日：2010-06-28
申请人： Thomas Scherer , Michael Markwart , Torsten Schwan
发明人： Thomas Scherer , Michael Markwart , Torsten Schwan
IPC分类号： B64D13/08 , B64D13/00
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y10S62/05
摘要： With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controlled feed air, the temperature of the injected feed air is controlled for each cabin zone, dependent upon the deviation of an injection temperature actual value for the feed air injected into the cabin zone in question, measured by sensors, in relation to an injection temperature optimum value. If there is no, or at least no usable reading of the ambient temperature of this cabin zone for a cabin zone, an optimum value for the injection temperature of this cabin zone can be established in accordance with a variation, whereby it is determined upon the basis of the injection temperature optimum values and/or the injection temperature actual values of other cabin zones, whereby the measurement by sensors of the cabin temperature works reliably. In accordance with another variation, the injection temperature optimum value of a cabin zone can be established without measuring ambient temperature by sensors or without reliably measuring ambient temperature from the temperature measured for the external surrounds of the aircraft.
摘要翻译：使用一种用于控制喷射到客机的客舱区域中的进料空气的温度的方法，其将舱室分成几个舱区，分别提供特别温度控制的进料空气，喷射进料的温度根据喷射温度最佳值，根据传感器测量的注入到所述舱室区域的进料空气的喷射温度实际值的偏差，对每个舱室进行空气控制。如果对于客舱区域没有或至少没有可用的该舱室区域的环境温度读数，则可以根据变化确定该舱区域的喷射温度的最佳值，由此根据喷射温度最佳值和/或其他舱区的喷射温度实际值的基础，由此由客舱温度的传感器进行的测量可靠地工作。根据另一个变化，可以建立客舱区域的喷射温度最佳值，而不需要通过传感器测量环境温度，或者不会从对飞行器的外部环境测量的温度可靠地测量环境温度。

6. 发明授权

US07775447B2 Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft 有权
标题翻译：用于控制喷射到客机的客舱区域中的进料空气的温度的方法
公开(公告)号：US07775447B2
公开(公告)日：2010-08-17
申请号：US10582595
申请日：2004-12-30
申请人： Thomas Scherer , Michael Markwart , Torsten Schwan
发明人： Thomas Scherer , Michael Markwart , Torsten Schwan
IPC分类号： F24F11/00 , B60H1/00 , F24F3/00
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y10S62/05
摘要： With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controlled feed air, the temperature of the injected feed air is controlled for each cabin zone, dependent upon the deviation of an injection temperature actual value for the feed air injected into the cabin zone in question, measured by sensors, in relation to an injection temperature optimum value. If there is no, or at least no usable reading of the ambient temperature of this cabin zone for a cabin zone, an optimum value for the injection temperature of this cabin zone can be established in accordance with a variation, whereby it is determined upon the basis of the injection temperature optimum values and/or the injection temperature actual values of other cabin zones, whereby the measurement by sensors of the cabin temperature works reliably. In accordance with another variation, the injection temperature optimum value of a cabin zone can be established without measuring ambient temperature by sensors or without reliably measuring ambient temperature from the temperature measured for the external surrounds of the aircraft.
摘要翻译：使用一种用于控制喷射到客机的客舱区域中的进料空气的温度的方法，其将舱室分成几个舱区，分别提供特别温度控制的进料空气，喷射进料的温度根据喷射温度最佳值，根据传感器测量的注入到所述舱室区域的进料空气的喷射温度实际值的偏差，对每个舱室进行空气控制。如果对于客舱区域没有或至少没有可用的该舱室区域的环境温度读数，则可以根据变化确定该舱区域的喷射温度的最佳值，由此根据喷射温度最佳值和/或其他舱区的喷射温度实际值的基础，由此由客舱温度的传感器进行的测量可靠地工作。根据另一个变化，可以建立客舱区域的喷射温度最佳值，而不需要通过传感器测量环境温度，或者不会从对飞行器的外部环境测量的温度可靠地测量环境温度。

7. 发明申请

US20070130970A1 Method for controlling the feed air temperature of a passenger aircraft 有权
标题翻译：控制客机进给空气温度的方法
公开(公告)号：US20070130970A1
公开(公告)日：2007-06-14
申请号：US10580944
申请日：2004-12-30
申请人： Torsten Schwan , Michael Markwart
发明人： Torsten Schwan , Michael Markwart
IPC分类号： F25D17/00 , F25B41/00
CPC分类号： B64D13/00 , B64D2013/0655
摘要： With a method for controlling the temperature of feed air supplied to a cabin area of a passenger aircraft (10), a measurement value for the ambient temperature in the cabin area is determined by means of a temperature sensor system (24). The temperature of the feed air is controlled, dependent upon a deviation of the ambient temperature measurement value in relation to an ambient temperature optimum value. In accordance with the invention, the ambient temperature measurement value is deduced from a number of individual temperature values for different points in the cabin area. In accordance with an example, the temperature sensor system used to establish individual temperature values for a cabin zone includes a number of discreet temperature sensors (24) positioned in this cabin zone, each of which provides an individual temperature value. Preferably, the temperature sensors (24) are distributed evenly over the whole length of the cabin zone in question.
摘要翻译：利用用于控制供应到客机（10）的客舱区域的供给空气的温度的方法，通过温度传感器系统（24）确定客舱区域中的环境温度的测量值。取决于环境温度测量值相对于环境温度最佳值的偏差来控制进料空气的温度。根据本发明，从客舱区域中的不同点的多个单独的温度值推导出环境温度测量值。根据一个例子，用于为舱区建立单独的温度值的温度传感器系统包括定位在该舱室区域中的多个谨慎的温度传感器（24），每个温度传感器提供单独的温度值。优选地，温度传感器（24）在所讨论的舱区的整个长度上均匀分布。

8. 发明授权

US08490884B2 Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft 有权
标题翻译：用于控制喷射到客机的客舱区域中的进料空气的温度的方法
公开(公告)号：US08490884B2
公开(公告)日：2013-07-23
申请号：US12824898
申请日：2010-06-28
申请人： Thomas Scherer , Michael Markwart , Torsten Schwan
发明人： Thomas Scherer , Michael Markwart , Torsten Schwan
IPC分类号： B60H1/00 , F24F3/00
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y10S62/05
摘要： Method for controlling the temperature of feed air injected into at least one cabin zone of a passenger aircraft, the temperature of injected feed air being controlled for each cabin zone dependent on the deviation of the injection temperature actual value of the feed air from an injection temperature target value, the injection temperature target value being established using an external ambient temperature actual value and not using a temperature sensor in the at least one cabin zone.
摘要翻译：用于控制喷射到客机的至少一个客舱区域中的进料空气的温度的方法，取决于进料空气的喷射温度实际值与喷射温度的偏差来控制每个舱区域的喷射进料空气的温度目标值，使用外部环境温度实际值建立喷射温度目标值，并且在至少一个舱区中不使用温度传感器。

9. 发明授权

US07802732B2 Device and process for temperature regulation of sections of the interior of an aircraft 有权
标题翻译：飞机内部部分温度调节的装置和过程
公开(公告)号：US07802732B2
公开(公告)日：2010-09-28
申请号：US10582570
申请日：2004-12-30
申请人： Thomas Scherer , Torsten Schwan , Georg Mühlthaler , Jan Dittmar
发明人： Thomas Scherer , Torsten Schwan , Georg Mühlthaler , Jan Dittmar
IPC分类号： F24F11/00 , F24F7/00 , F24F3/00 , F24D19/10
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y02T50/44
摘要： A device for temperature regulation of sections of the interior of an aircraft includes a controlled mixer valve for the mixing of engine bleed air and air that is cooler than the engine bleed air in order to obtain pre-tempered mixed air flowing out of the mixer valve; a distribution line connected to the outlet of the mixer valve which is connected to the respective sections by at least two supply lines; individual heating units assigned to the respective sections; sensors assigned to the individual sections for the respective actual temperatures; transmitters for the respective nominal temperatures; and a regulator unit which controls the mixer valve dependent upon the respective nominal temperatures and the respective actual temperatures in the individual areas.
摘要翻译：用于飞行器内部的部分温度调节的装置包括用于混合发动机排出空气和比发动机放气更冷的空气的受控混合器阀，以获得从混合器阀流出的预调温混合空气 ; 连接到混合器阀的出口的分配线，其通过至少两条供应管线连接到各个部分; 分配给各个部分的各个加热单元; 分配给相应实际温度的各个部分的传感器; 发射机相应的标称温度; 以及调节器单元，其根据相应的标称温度和各个区域中的相应实际温度来控制混合器阀。

10. 发明申请

US20070119584A1 Device and process for temperature regulation of sections of the interior of an aircraft 有权
标题翻译：飞机内部部分温度调节的装置和过程
公开(公告)号：US20070119584A1
公开(公告)日：2007-05-31
申请号：US10582570
申请日：2004-12-30
申请人： Thomas Scherer , Torsten Schwan , Georg Muhlthaler
发明人： Thomas Scherer , Torsten Schwan , Georg Muhlthaler
IPC分类号： F24D19/10 , B60H1/00 , F24F3/00
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y02T50/44
摘要： A process for temperature regulation of sections of the interior of an aircraft with the following steps: recording of the respective actual temperatures and the respective nominal temperatures in the individual sections; mixing of engine bleed air and air which is cooler than the engine bleed air in order to obtain pre-tempered mixed air at a temperature which essentially corresponds to the lowest of the nominal temperatures recorded; distribution of the pre-tempered mixed air to all sections; and post-tempering of the mixed air distributed to the sections with higher nominal temperature corresponding to the differences between the respective nominal temperatures and the respective actual temperatures can be carried out in a device with a controlled mixer valve for the mixing of engine bleed air and air that is cooler than the engine bleed air in order to obtain pre-tempered mixed air flowing out of the mixer valve; to a distribution line connected to the outlet of the mixer valve which is connected to the respective sections by means of at least two supply lines; individual heating units assigned to the respective sections; sensors assigned to the individual sections for the respective actual temperatures and transmitters for the respective nominal temperatures; a regulator unit which controls the mixer valve dependent upon the respective nominal temperatures and the respective actual temperatures in the individual areas in such a way that the pre-tempered mixed air is of a temperature which essentially corresponds to the lowest of the nominal temperatures for all sections, and which controls the heating units assigned to the other sections corresponding to the differences between the respective nominal temperatures and the respective actual temperatures.
摘要翻译：一种用于对飞行器内部的部分进行温度调节的过程，具有以下步骤：在各个部分中记录相应的实际温度和相应的标称温度; 混合发动机排出空气和比发动机放气更冷的空气，以获得基本上对应于记录的最低标称温度的温度的预调温混合空气; 将预调混合空气分配到所有区段; 并且分配到具有相应于相应标称温度和相应实际温度之间的差异的具有较高标称温度的部分的混合空气的后回火可以在具有受控混合器阀的装置中进行，用于混合发动机排放空气和比发动机冷却的空气排出空气，以获得从混合器阀流出的预调温混合空气; 连接到通过至少两条供应管线连接到各个部分的混合器阀的出口的分配线路; 分配给各个部分的各个加热单元; 分配给相应实际温度的各个部分的传感器和相应标称温度的发射器; 调节器单元，其根据相应的标称温度和各个区域中的相应实际温度来控制混合器阀，使得预调温混合空气的温度基本上对应于所有的最低标称温度并且其控制分配给对应于相应标称温度和相应实际温度之间的差异的其它部分的加热单元。

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