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1.发明授权公开(公告)号：US07980928B2
公开(公告)日：2011-07-19
申请号：US11311535
申请日：2005-12-19
CPC分类号： B64D13/06 , B64D2013/0648 , Y02T50/56
摘要： The present application describes an arrangement and a method for utilizing the heat of waste air for heating the bilge area of aircraft, wherein the bilge area is connected to a heat transfer unit via a first air supply pipe, through which a bilge air flow drawn in from the bilge area flows into the heat transfer unit, wherein the heat transfer unit comprises a second air supply pipe, through which a waste air heat flow to be cooled that is created at another location in the aircraft flows into the heat transfer unit in order to heat the drawn-in bilge air flow, wherein the heat transfer unit comprises a first air discharge pipe, through which the cooled waste air heat flow is discharged, and a second air discharge pipe with a bilge inlet section, and wherein at least a portion of the heated bilge flow is returned to the bilge area via the air discharge pipe and the bilge inlet section.
摘要翻译： 本申请描述了一种用于利用废气的热量来加热飞机舱底区域的布置和方法，其中舱底区域经由第一空气供应管连接到传热单元，通过该第一空气供应管， 从舱底区域流入传热单元，其中传热单元包括第二空气供应管，通过该第二空气供应管，在飞机中的另一位置处产生的待冷却的废气热流按顺序流入传热单元 加热吸入舱底空气流，其中传热单元包括排出冷却的废气热流的第一排气管和具有舱底入口段的第二排气管，并且其中至少一个 加热的舱底流的一部分经由排气管和舱底入口部返回到舱底区域。
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2.发明申请公开(公告)号：US20060138280A1
公开(公告)日：2006-06-29
申请号：US11311535
申请日：2005-12-19
IPC分类号： B64C1/00
CPC分类号： B64D13/06 , B64D2013/0648 , Y02T50/56
摘要： The present application describes an arrangement and a method for utilizing the heat of waste air for heating the bilge area of aircraft, wherein the bilge area is connected to a heat transfer unit via a first air supply pipe, through which a bilge air flow drawn in from the bilge area flows into the heat transfer unit, wherein the heat transfer unit comprises a second air supply pipe, through which a waste air heat flow to be cooled that is created at another location in the aircraft flows into the heat transfer unit in order to heat the drawn-in bilge air flow, wherein the heat transfer unit comprises a first air discharge pipe, through which the cooled waste air heat flow is discharged, and a second air discharge pipe with a bilge inlet section, and wherein at least a portion of the heated bilge flow is returned to the bilge area via the air discharge pipe and the bilge inlet section.
摘要翻译： 本申请描述了一种用于利用废气的热量来加热飞机舱底区域的布置和方法，其中舱底区域经由第一空气供应管连接到传热单元，通过该第一空气供应管， 从舱底区域流入传热单元，其中传热单元包括第二空气供应管，通过该第二空气供应管，在飞机中的另一位置处产生的待冷却的废气热流按顺序流入传热单元 加热吸入舱底空气流，其中传热单元包括排出冷却的废气热流的第一排气管和具有舱底入口段的第二排气管，并且其中至少一个 加热的舱底流的一部分经由排气管和舱底入口部返回到舱底区域。
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3.发明授权公开(公告)号：US08137169B2
公开(公告)日：2012-03-20
申请号：US13083904
申请日：2011-04-11
CPC分类号： B64D13/06 , B64D2013/0648 , Y02T50/56
摘要： The present application describes an arrangement and a method for utilizing the heat of waste air for heating the bilge area of aircraft, wherein the bilge area is connected to a heat transfer unit via a first air supply pipe, through which a bilge air flow drawn in from the bilge area flows into the heat transfer unit, wherein the heat transfer unit comprises a second air supply pipe, through which a waste air heat flow to be cooled that is created at another location in the aircraft flows into the heat transfer unit in order to heat the drawn-in bilge air flow, wherein the heat transfer unit comprises a first air discharge pipe, through which the cooled waste air heat flow is discharged, and a second air discharge pipe with a bilge inlet section, and wherein at least a portion of the heated bilge flow is returned to the bilge area via the air discharge pipe and the bilge inlet section.
摘要翻译： 本申请描述了一种用于利用废气的热量来加热飞机舱底区域的布置和方法，其中舱底区域经由第一空气供应管连接到传热单元，通过该第一空气供应管， 从舱底区域流入传热单元，其中传热单元包括第二空气供应管，通过该第二空气供应管，在飞机中的另一位置处产生的待冷却的废气热流按顺序流入传热单元 加热吸入舱底空气流，其中传热单元包括排出冷却的废气热流的第一排气管和具有舱底入口段的第二排气管，并且其中至少一个 加热的舱底流的一部分经由排气管和舱底入口部返回到舱底区域。
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4.发明申请Method For Controlling The Temperature Of Feed Air Injected Into The Cabin Zone Of A Passenger Aircraft 有权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
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。
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5.发明授权Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft 有权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
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。
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6.发明授权Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft 有权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
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。
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7.发明授权公开(公告)号：US07878887B2
公开(公告)日：2011-02-01
申请号：US10581001
申请日：2004-12-30
申请人： Jens Elmers , Michael Markwart , Dietrich Lampe , Thomas Scherer
发明人： Jens Elmers , Michael Markwart , Dietrich Lampe , Thomas Scherer
摘要： A method and a line system for the air-conditioning of a cabin of an aircraft envisage that at sites remote from passengers air that is at a temperature lower than air at sites closer to passengers is introduced into the cabin.
摘要翻译： 用于飞机机舱空调的方法和线路系统设想在远离乘客的位置处，在靠近乘客的位置处于比空气低的空气的空气被引入到舱室中。
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8.发明授权
公开(公告)号：US5695396A
公开(公告)日：1997-12-09
申请号：US617487
申请日：1996-03-15
申请人： Michael Markwart , Klaus Petry , Thomas Scherer
发明人： Michael Markwart , Klaus Petry , Thomas Scherer
CPC分类号： B64D13/00 , B64D2013/003 , B64D2013/0651 , B64D2013/0688 , F24F2003/1646 , F24F2011/0024 , Y02B30/78 , Y02T50/56
摘要： An air supply system for an aircraft cabin reduces the concentration of contaminations of the air in the cabin by a flexibly controllable valve system that comprises pairs of valves which on the one hand are ganged to respective air openings. One valve of a pair is connected to a fresh air or mixed air supply line. The other valve of a pair is connected to a suction or exhaust duct. Thus, depending on which valve in a pair is open and which is closed, the respective air opening can function as an air outlet for supply of mixed or fresh air into the cabin or as a suction port. Such a system permits a flexible volume control of the supply of fresh air into selectable cabin sections as well as a flexible volume control for the removal of used air from respective cabin sections. Additionally, it is now possible to increase the size of the non-smoking section at the expense of the smoking section or vice versa simply by a respective valve control.
摘要翻译： 用于飞机机舱的空气供应系统通过柔性可控的阀门系统来减少舱内空气的污染物浓度，该系统包括成对的阀门，这些阀门一方面被组合到相应的空气开口。 一对一个阀连接到新鲜空气或混合空气供应管线。 一对的另一个阀连接到吸气或排气管道。 因此，取决于一对中的哪个阀打开并且其被关闭，相应的空气开口可以用作用于将混合或新鲜空气供应到客舱或作为吸入口的出气口。 这样的系统允许将新鲜空气供应到可选择的舱室部分中的灵活的体积控制以及用于从相应的舱室部分移除用过的空气的灵活的体积控制。 此外，现在可以通过相应的阀门控制来增加非吸烟部分的尺寸，而烟费部分的费用也是相反的。
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公开(公告)号：US20050230488A1
公开(公告)日：2005-10-20
申请号：US11020617
申请日：2004-12-23
申请人： Michael Markwart , Klaus Arnold , Frank Bracker , Jens Lohmar , Thomas Scherer , Torsten Schwan
发明人： Michael Markwart , Klaus Arnold , Frank Bracker , Jens Lohmar , Thomas Scherer , Torsten Schwan
CPC分类号： B64D13/08 , B60H1/00371 , B60H2001/00235 , B64D13/06
摘要： An air dispersion system has a main supply line, a plurality of air outlets, which are connected via respective air exhaust routes to the main supply line, and at least one heating element, which is associated with at least one of the air outlets and can temper the air in the exhaust route of this air outlet.
摘要翻译： 空气分散系统具有主供应管线，多个空气出口，其经由各自的排气路径连接到主供应管线，以及至少一个加热元件，其与至少一个空气出口和罐 调节该出风口的排气路径中的空气。
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10.发明授权
公开(公告)号：US5545084A
公开(公告)日：1996-08-13
申请号：US504906
申请日：1995-07-20
申请人： Heinz Fischer , Thomas Scherer , Michael Markwart , Klaus Petry
发明人： Heinz Fischer , Thomas Scherer , Michael Markwart , Klaus Petry
IPC分类号： B64D13/08
CPC分类号： B64D13/08 , B64D2013/0651 , B64D2013/0688 , Y02T50/56
摘要： A method and apparatus is provided for air conditioning two passenger decks in an aircraft, especially a high capacity aircraft. The engine tap air stream is provided for air conditioning the upper deck passenger cabin and the lower deck passenger cabin. The air stream is cooled in at least one air conditioning plant, mixed with recirculated air from the lower cabin in at least one premix chamber, and then mixed with recirculated air from the upper cabin in local mixing chambers. The finished air streams are directed to the upper deck and the lower deck passenger cabins. The upper deck exhaust air is essentially completely used as recirculation air being mixed with the conditioning air in the local mixing chambers. The lower deck exhaust air is partially used as recirculation air being mixed with the conditioning air in the premix chambers, and is partially exhausted overboard. The desired air temperature, quality, and quantity can thus be achieved independently in the two passenger cabins, in an energy efficient and space-saving manner.
摘要翻译： 提供一种用于空调飞机中的两个乘客甲板的方法和装置，特别是高容量飞机。 发动机水龙头气流用于空调上甲板客舱和下甲板客舱。 空气流在至少一个空调设备中冷却，在至少一个预混合室中与来自下部舱室的再循环空气混合，然后与来自上部舱室的再循环空气混合在局部混合室中。 成品气流被引导到上甲板和下甲板客舱。 上层排气基本上完全用作再循环空气与局部混合室中的调节空气混合。 下甲板废气被部分地用作再循环空气与预混室中的调节空气混合，并且部分地被耗尽在外面。 因此，能够以节能且节省空间的方式在两个客舱中独立地实现期望的空气温度，质量和数量。
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