-
1.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。
-
2.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。
-
公开(公告)号：US20090277445A1
公开(公告)日：2009-11-12
申请号：US12279286
申请日：2007-02-13
申请人： Michael Markwart
发明人： Michael Markwart
IPC分类号： A61M16/00
CPC分类号： B64D13/00 , B64D2013/0614 , B64D2013/0677 , B64D2013/0688 , Y02T50/44 , Y02T50/56
摘要： A system for improving the air quality in a pressure cabin of an aircraft comprises a recirculation air circuit by means of which a portion of the cabin air, referred to as recirculation air, is withdrawn from the pressure cabin, filtered and then recirculated into the pressure cabin. To increase the oxygen partial pressure of the air fed back into the pressure cabin, the quantity of recirculation air is passed wholly or partially through a nitrogen generator (52) which generates nitrogen and an oxygen-containing waste gas from the recirculation air supplied. The oxygen-containing waste gas of the nitrogen generator (52), together with any remaining quantity of recirculation air untreated by the nitrogen generator (52), is recirculated into the pressure cabin. The nitrogen generator (52), to which only recirculation air is supplied, utilises a pressure gradient existing in flight between the pressure cabin and the outside of the aircraft for nitrogen generation.
摘要翻译： 用于改善飞机的压力舱中的空气质量的系统包括再循环空气回路，借助于该再循环空气回路，将一部分称为再循环空气的客舱空气从压力舱中取出，过滤并再循环进入压力 舱。 为了增加反馈到压力舱中的空气的氧气分压，再循环空气的量完全或部分地通过氮气发生器（52），氮气发生器（52）从供应的再循环空气产生氮气和含氧废气。 氮气发生器（52）的含氧废气以及未经氮气发生器（52）处理的剩余量的再循环空气再循环进入压力舱。 只有再循环空气供应的氮气发生器（52）利用存在于压力舱和飞机外部的飞行中的压力梯度来产生氮气。
-
4.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。
-
5.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。
-
公开(公告)号：US08074927B2
公开(公告)日：2011-12-13
申请号：US12279286
申请日：2007-02-13
申请人： Michael Markwart
发明人： Michael Markwart
IPC分类号： A61M16/00
CPC分类号： B64D13/00 , B64D2013/0614 , B64D2013/0677 , B64D2013/0688 , Y02T50/44 , Y02T50/56
摘要： A system for improving the air quality in a pressure cabin of an aircraft includes a recirculation air circuit in which a portion of the cabin air, referred to as recirculation air, is withdrawn from the pressure cabin, filtered and then recirculated into the pressure cabin. To increase the oxygen partial pressure of the air fed back into the pressure cabin, the quantity of recirculation air is passed wholly or partially through a nitrogen generator which generates nitrogen and an oxygen-containing waste gas from the recirculation air supplied. The oxygen-containing waste gas of the nitrogen generator, together with any remaining quantity of recirculation air untreated by the nitrogen generator, is recirculated into the pressure cabin. The nitrogen generator, to which only recirculation air is supplied, utilizes a pressure gradient existing in flight between the pressure cabin and the outside of the aircraft for nitrogen generation.
摘要翻译： 用于改善飞机的压力舱中的空气质量的系统包括一个再循环空气回路，其中将一部分称为再循环空气的客舱空气从压力舱中取出，过滤并再循环进入压力舱。 为了增加反馈到压力舱中的空气的氧气分压，再循环空气的量完全或部分地通过产生氮气的氮气发生器和来自供应的再循环空气的含氧废气。 氮气发生器的含氧废气以及未经氮气发生器处理的剩余量的再循环空气再循环进入压力舱。 仅供给再循环空气的氮气发生器利用在压力舱和飞机外部的飞行中存在的压力梯度来产生氮气。
-
7.发明申请公开(公告)号：US20110192565A1
公开(公告)日：2011-08-11
申请号：US13083904
申请日：2011-04-11
IPC分类号： B64D13/08
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。
-
公开(公告)号：US20100173576A1
公开(公告)日：2010-07-08
申请号：US12646224
申请日：2009-12-23
CPC分类号： B64D13/08 , B64D2013/0666 , Y02T50/56
摘要： An aircraft air-conditioning system (10) comprises an air-conditioning unit (12) that is connected by a main fresh-air line (16) to a mixer (18) in order to supply the mixer (18) with fresh air at a desired low temperature. A fresh-air branch line (20) that is connected upstream of the mixer (18) to the main fresh-air line (16) has a flow cross section that is smaller than a flow cross section of the main fresh-air line (16). In a region of connection of the main fresh-air line (16) to the fresh-air branch line (20) the main fresh-air line (16) and the fresh-air branch line (20) are so formed that a main fresh air flow flowing through the main fresh-air line (16) is deflected, while a fresh air branch flow flowing through the fresh-air branch line (20) experiences substantially no deflection,
摘要翻译： 飞机空调系统（10）包括空调单元（12），该空调单元（12）通过主要新鲜空气管路（16）连接到混合器（18），以便向混合器（18）提供新鲜空气 所需的低温。 将连接在混合器18上游的主空气管路（20）与主空气管路（16）连接的流路横截面小于主空气管路的流路截面（ 16）。 在主空气管路（16）与新鲜空气支路（20）连接的区域中，主空气管路（16）和新鲜空气支管路（20）形成为主 流过主新鲜空气管路（16）的新鲜空气流被偏转，而流过新鲜空气支路（20）的新鲜空气分支流体基本上没有弯曲，
-
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。
-
10.发明授权System and method for air conditioning at least one partial region of an airplane 有权用于空调飞机的至少一个部分区域的系统和方法公开(公告)号：US09227730B2
公开(公告)日：2016-01-05
申请号：US12738482
申请日：2008-10-17
申请人： Michael Markwart , Peggy Bendfeldt , Ingo Gores , Uwe Buchholz , Christina Koepp
发明人： Michael Markwart , Peggy Bendfeldt , Ingo Gores , Uwe Buchholz , Christina Koepp
CPC分类号： B64D13/06 , B64D13/00 , B64D2013/0625 , B64D2013/0662 , B64D2013/0688 , Y02T50/44 , Y02T50/56
摘要： A system for air conditioning at least one partial region of an aircraft comprises an air providing device for providing air to be supplied to a region of the aircraft to be ventilated at a desired temperature and pressure. A supply air duct is connected at a first end to the air providing device. A second end of the supply air duct is connected to an air inlet which opens near the floor into the aircraft region to be ventilated. A control device is set up to ensure that the air provided by the air providing device enters the aircraft region to be ventilated via the air inlet at such a speed that the air is distributed near the floor in the aircraft region to be ventilated and rises at heat sources present in the aircraft region to be ventilated, and that the air provided by the air providing device enters the aircraft region to be ventilated via the air inlet at such a temperature that a desired ambient temperature is set in the aircraft region to be ventilated.
摘要翻译： 用于空调飞行器的至少一个部分区域的系统包括空气提供装置，用于在期望的温度和压力下提供要供应到要通风的飞行器的区域的空气。 供气管道在第一端连接到空气供应装置。 供气管道的第二端连接到在地板附近打开进入通风的飞机区域的空气入口。 设置控制装置以确保由空气提供装置提供的空气通过空气入口进入飞机区域以使得空气分布在飞机区域附近的地板上被通风并在 存在于飞机区域中要通风的热源，并且由空气提供装置提供的空气通过空气入口进入飞机区域，以使飞机区域中设置期望的环境温度以通风 。
-
-
-
-
-
-
-
-
-
搜索结果
25 条记录 (耗时 0.012 秒)
