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公开(公告)号：US20230366771A1
公开(公告)日：2023-11-16
申请号：US18144479
申请日：2023-05-08
Applicant: AIRBUS SAS , Airbus Operations GmbH , University of Ioannina-Special Account for Research Funds
Inventor： Alois Friedberger , Dariusz Krakowski , Alkiviadis S. Paipetis , George Karalis
Abstract: A fluid transport device includes a conduit unit having a wall for separating an inside from an outside of the conduit unit. The device also includes an energy supply unit coupled to the conduit unit and configured to provide electrical energy based on a temperature gradient between the inside and the outside of the conduit unit. The device also includes a monitoring unit configured to monitor a state of the conduit unit and to generate data representative for the state of the conduit unit. The energy supply unit supplies the electrical energy to the monitoring unit, thereby enabling the monitoring unit to monitor the state of the conduit unit. A method for manufacturing a fluid transport device is also described.
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公开(公告)号：US10507926B2
公开(公告)日：2019-12-17
申请号：US14990803
申请日：2016-01-08
Applicant: Airbus Operations GmbH
Inventor： Dariusz Krakowski , Stephan Risse
Abstract: A conveying device for conveying a fluid stream comprising a mechanical unit, including a movable conveying element, and an electrical unit comprising a housing as well as electronic elements arranged in the housing. The mechanical unit and the electrical unit are detachably connected to one another.
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公开(公告)号：US20130139891A1
公开(公告)日：2013-06-06
申请号：US13692672
申请日：2012-12-03
Applicant: AIRBUS OPERATIONS GMBH
Inventor： Jurgen Kelnhofer , Dariusz Krakowski
IPC: F16L53/00
CPC classification number: F16L53/30 , B64D13/06 , B64D2013/0611 , F02C6/06 , F05D2220/50 , F05D2270/306 , Y02T50/56 , Y10T137/0318 , Y10T137/6416
Abstract: A method for controlling the operation of an auxiliary power unit supplying an aircraft air conditioning system with compressed process air includes determining a heating or cooling requirement of an aircraft region to be air-conditioned, determining a desired value of at least one process air flow parameter in dependence on the determined heating or cooling requirement of the aircraft region to be air-conditioned, controlling the operation of the auxiliary power unit in dependence on the determined process air flow parameter desired value, acquiring an actual value of the at least one process air flow parameter, comparing the process air flow parameter actual value with the process air flow parameter desired value and controlling the operation of the auxiliary power unit in dependence on the result of the comparison of the process air flow parameter actual value with the process air flow parameter desired value.
Abstract translation: 用于控制向压缩处理空气供应飞行器空调系统的辅助动力单元的操作的方法包括确定要进行空调的飞行器区域的加热或冷却要求，确定至少一个处理空气流参数的期望值 根据所确定的要进行空调的飞行器区域的加热或冷却要求，根据确定的过程空气流量参数期望值来控制辅助动力单元的运行，获取至少一个处理空气的实际值 流程参数，将过程空气流量参数实际值与过程空气流量参数期望值进行比较，并根据过程空气流量参数实际值与过程空气流量参数的比较结果控制辅助动力单元的运行 所需值。
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公开(公告)号：US20170066536A1
公开(公告)日：2017-03-09
申请号：US15254067
申请日：2016-09-01
Applicant: Airbus Operations GmbH , Airbus SAS
Inventor： Nicolas Houis , Dariusz Krakowski , Tim Giese
CPC classification number: B64D13/08 , B64D13/06 , B64D2013/0688 , F25B13/00 , Y02T50/56
Abstract: An aircraft air conditioning system comprising an air conditioning unit adapted and configured to be supplied with compressed process air and to generate cold fresh air, a mixer adapted and configured to mix the cold fresh air from the air conditioning unit with recirculation air recirculated from an aircraft region to be air conditioned, an air outlet adapted and configured to direct mixed air from the mixer into the aircraft region, a first sensor adapted and configured to detect an actual temperature in the aircraft region, a second sensor adapted and configured to detect a temperature of the mixed air directed into the aircraft region, and a control unit adapted and configured to control an operation of the air conditioning unit in dependence on a difference between the temperature of the mixed air directed into the aircraft region and the actual temperature in the aircraft region.
Abstract translation: 一种飞机空调系统，包括空调单元，该空调单元适于并被配置为供应压缩的处理空气并产生冷的新鲜空气;混合器，适于并构造成将来自空调单元的冷新鲜空气与从飞行器再循环的再循环空气混合 要进行空调的区域，适于并且被配置为将来自混合器的混合空气引导到飞行器区域中的空气出口，适于并配置成检测飞机区域中的实际温度的第一传感器，适于并构造成检测温度的第二传感器 被引导到飞行器区域的混合空气的控制单元，以及控制单元，其被配置成根据引导到飞机区域的混合空气的温度与飞行器中的实际温度之间的差异来控制空调单元的操作 地区。
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5.发明申请CONVEYING DEVICE AND AIRCRAFT SYSTEM WITH A CONVEYING DEVICE OF SUCH A TYPE 审中-公开具有这种类型的输送装置的输送装置和飞行器系统公开(公告)号：US20160200440A1
公开(公告)日：2016-07-14
申请号：US14990803
申请日：2016-01-08
Applicant: Airbus Operations, GmbH
Inventor： Dariusz Krakowski , Stephan Risse
CPC classification number: B64D13/06 , B64D2013/0644 , F04D13/06 , F04D25/068 , F04D29/644
Abstract: A conveying device for conveying a fluid stream comprising a mechanical unit, including a movable conveying element, and an electrical unit comprising a housing as well as electronic elements arranged in the housing. The mechanical unit and the electrical unit are detachably connected to one another.
Abstract translation: 一种用于输送流体流的输送装置，包括包括可移动输送元件的机械单元，以及包括壳体的电气单元以及布置在壳体中的电子元件。 机械单元和电气单元可拆卸地彼此连接。
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Patent Agency Ranking
公开(公告)号：US09689597B2
公开(公告)日：2017-06-27
申请号：US14573059
申请日：2014-12-17
Applicant: Airbus Operations GmbH
Inventor： Jürgen Kelnhofer , Dariusz Krakowski
CPC classification number: F25B49/02 , B64D13/06 , B64D2013/0655 , Y02T50/56
Abstract: An aircraft air conditioning system comprises a plurality of temperature zones and at least one door. Comprises an air-conditioning unit configured to condition and provide air to at least one of the plurality of temperature zones, temperature zone sensors each associated with a temperature zone for measuring the temperature therein, and a control unit. The control unit receives information representing the closing state of a cabin door, and is coupled to the temperature zone sensors and configured to control the temperature of the conditioned air provided to at least one of the plurality of temperature zones in two operation modes. In a first mode, when doors are closed, the temperature control depends on the measured temperatures in the temperature zones. In the second mode, it depends on a set-temperature, independent of the measured temperature in a temperature zone affected by an open door.
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公开(公告)号：US09394055B2
公开(公告)日：2016-07-19
申请号：US13646231
申请日：2012-10-05
Applicant: AIRBUS OPERATIONS GMBH
Inventor： Michael Markwart , Jens Lohmar , Dariusz Krakowski , Martin Schmid , Torsten Stengel , Jens Elmers , Thomas Scherer
CPC classification number: B64D13/00 , B64D2013/0688
Abstract: A mixer for an aircraft air conditioning system has first and second fresh air lines and first and second recirculation air lines. A first premixer is connected to the first fresh air line and the first recirculation air line, to mix the fresh air with the recirculation air thereof. A second premixer is connected to the second fresh air line and the second recirculation air line, to mix the fresh air with the recirculation air thereof. A main mixer is connected by a first premixed air line to the first premixer and by a second premixed air line to the second premixer. The main mixer is adapted to be supplied through the first premixed air line and the second premixed air line exclusively with premixed air from the first and/or the second premixer.
Abstract translation: 用于飞机空调系统的混合器具有第一和第二新鲜空气管线和第一和第二再循环空气管线。 第一预混合器连接到第一新鲜空气管线和第一再循环空气管线，以将新鲜空气与其再循环空气混合。 第二预混合器连接到第二新鲜空气管线和第二再循环空气管线，以将新鲜空气与其再循环空气混合。 主混合器通过第一预混合空气管线连接到第一预混合器，并且通过第二预混合空气管线连接到第二预混合器。 主混合器适于通过第一预混合空气管线和第二预混合空气管线专门提供来自第一和/或第二预混合器的预混合空气。
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8.发明申请公开(公告)号：US20150329210A1
公开(公告)日：2015-11-19
申请号：US14715846
申请日：2015-05-19
Applicant: Airbus Operations GmbH , Airbus Operations S.L.
Inventor： Holger Bammann , Frank Klimpel , Dariusz Krakowski , Anton Mendez-Diaz
CPC classification number: B64D13/06 , B60H1/00435 , B60H1/3211 , B64D2013/0611 , B64D2013/0618 , B64D2013/0688 , Y02T50/56
Abstract: An aircraft air conditioning system comprises a process air line configured to supply compressed process air provided by a process air source to an air conditioning unit of the aircraft air conditioning system and a trim air line branching off from the process air line upstream of the air conditioning unit and being configured such that trim air flows through the trim air line, the trim air having been branched off from the compressed process air flowing through the process air line. A compressor is arranged in the trim air line and is configured to compress the trim air flowing through the trim air line. A turbine of the aircraft air conditioning system is configured to drive the compressor. A cabin exhaust air line is configured to supply cabin exhaust air discharged from an aircraft cabin to the turbine for driving the turbine.
Abstract translation: 飞机空调系统包括处理空气管线，其被配置为将由处理空气源提供的压缩过程空气供应到飞行器空调系统的空调单元和从空调的上游的处理空气管线分支的调整空气管线 单元并且被配置为使得修剪空气流过修剪空气管线，修剪空气已经从流过处理空气管线的压缩过程空气分支。 压缩机布置在装饰空气管线中并且构造成压缩流过修剪空气管线的修剪空气。 飞机空调系统的涡轮机构造成驱动压缩机。 客舱排气管线被配置为将从飞机机舱排出的客舱排气供应到用于驱动涡轮机的涡轮机。
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公开(公告)号：US20130035027A1
公开(公告)日：2013-02-07
申请号：US13646231
申请日：2012-10-05
Applicant: AIRBUS OPERATIONS GMBH
Inventor： Michael Markwart , Jens Lohmar , Dariusz Krakowski , Martin Schmid , Torsten Stengel , Jens Elmers , Thomas Scherer
IPC: B64D13/08
CPC classification number: B64D13/00 , B64D2013/0688
Abstract: A mixer for an aircraft air conditioning system has first and second fresh air lines and first and second recirculation air lines. A first premixer is connected to the first fresh air line and the first recirculation air line, to mix the fresh air with the recirculation air thereof. A second premixer is connected to the second fresh air line and the second recirculation air line, to mix the fresh air with the recirculation air thereof. A main mixer is connected by a first premixed air line to the first premixer and by a second premixed air line to the second premixer. The main mixer is adapted to be supplied through the first premixed air line and the second premixed air line exclusively with premixed air from the first and/or the second premixer.
Abstract translation: 用于飞机空调系统的混合器具有第一和第二新鲜空气管线和第一和第二再循环空气管线。 第一预混合器连接到第一新鲜空气管线和第一再循环空气管线，以将新鲜空气与其再循环空气混合。 第二预混合器连接到第二新鲜空气管线和第二再循环空气管线，以将新鲜空气与其再循环空气混合。 主混合器通过第一预混合空气管线连接到第一预混合器，并且通过第二预混合空气管线连接到第二预混合器。 主混合器适于通过第一预混合空气管线和第二预混合空气管线专门提供来自第一和/或第二预混合器的预混合空气。
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公开(公告)号：US09976684B2
公开(公告)日：2018-05-22
申请号：US13692672
申请日：2012-12-03
Applicant: AIRBUS OPERATIONS GMBH
Inventor： Jurgen Kelnhofer , Dariusz Krakowski
CPC classification number: F16L53/30 , B64D13/06 , B64D2013/0611 , F02C6/06 , F05D2220/50 , F05D2270/306 , Y02T50/56 , Y10T137/0318 , Y10T137/6416
Abstract: A method for controlling the operation of an auxiliary power unit supplying an aircraft air conditioning system with compressed process air includes determining a heating or cooling requirement of an aircraft region to be air-conditioned, determining a desired value of at least one process air flow parameter in dependence on the determined heating or cooling requirement of the aircraft region to be air-conditioned, controlling the operation of the auxiliary power unit in dependence on the determined process air flow parameter desired value, acquiring an actual value of the at least one process air flow parameter, comparing the process air flow parameter actual value with the process air flow parameter desired value and controlling the operation of the auxiliary power unit in dependence on the result of the comparison of the process air flow parameter actual value with the process air flow parameter desired value.
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