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公开(公告)号：US12027716B2
公开(公告)日：2024-07-02
申请号：US17524448
申请日：2021-11-11
发明人： Philippe Pene , Thomas Scherer
IPC分类号： H01M50/00 , A62C3/16 , A62C37/11 , H01M10/613 , H01M10/6556 , H01M10/6557 , H01M10/6568 , H01M10/6569 , H01M50/22
CPC分类号： H01M50/22 , A62C3/16 , A62C37/11 , H01M10/613 , H01M10/6556 , H01M10/6557 , H01M10/6568 , H01M10/6569
摘要： An electric generator including a number of electric accumulators and at least one heat-sink device using a phase-change material configured to pick up the excessive thermal energy produced by one of the electric accumulators and change phase in order to absorb a large quantity of thermal energy in the form of latent heat.
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公开(公告)号：US12054281B2
公开(公告)日：2024-08-06
申请号：US17982567
申请日：2022-11-08
发明人： Thomas Josset , Didier Poirier , Holger Bammann , Thomas Scherer
IPC分类号： B64D41/00 , B60L58/33 , B64D13/06 , H01M8/04007 , H01M8/04029 , H01M8/04111 , H01M8/04664 , H01M8/04746
CPC分类号： B64D41/00 , B60L58/33 , B64D13/06 , H01M8/04029 , H01M8/04074 , H01M8/04111 , H01M8/04664 , H01M8/04753 , H01M8/04776 , B60L2200/10 , B64D2013/0611 , B64D2041/005 , H01M2250/20
摘要： An auxiliary power unit for an aircraft. It includes an air compressor coupled to an air-drawing device for drawing in air from outside the aircraft, the compressor supplying compressed air to a manifold. The manifold is configured to supply air to an environmental control system and a start-up module of at least one propulsion system of the aircraft running on hydrogen. The manifold is also configured to supply air to a fuel cell stack arranged to provide an electric generation function configured to power non-propulsive systems of the aircraft, the fuel cell stack also being supplied with hydrogen from a tank supplying hydrogen to the at least one propulsion system of the aircraft.
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公开(公告)号：US11952134B2
公开(公告)日：2024-04-09
申请号：US17737134
申请日：2022-05-05
发明人： Jorge Carretero Benignos , Benedikt Bammer , Olivier Verseux , Maria Del Sagrario Juanas Fernandez , Jorge Molano Rembiasz , Thomas Scherer , Alexander Solntsev
摘要： An electric propulsion unit of an aircraft including a nacelle housing an electric power system, an electric motor and a cooling system for the electric power system; the nacelle including a central fairing, a front fairing which extends from the central fairing to a front end and a rear fairing which extends from the central fairing to a rear end. The front fairing includes a protrude positioned in a lower part of the front fairing, the protrude having a front face in a transverse plane, a main air inlet of the cooling system being positioned on the front face.
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公开(公告)号：US10457400B2
公开(公告)日：2019-10-29
申请号：US14310381
申请日：2014-06-20
发明人： Dietrich Lampe , Thomas Scherer
摘要： A mixing device that is particularly suitable for use in an aircraft air-conditioning system comprising a cold air supply line adapted to supply cold air to the mixing device. A first recirculation air supply line is adapted to supply recirculation air to the mixing device. A mixing chamber is connected to the cold air supply line and the first recirculation air supply line and is adapted to supply the cold air supplied to the mixing device via the cold air supply line with the recirculation air supplied to the mixing device via the first recirculation air supply line. The first recirculation air supply line has a heat transfer portion which is thermoconductively connected to an area of a wall delimiting the mixing chamber that is at risk of icing.
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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
发明人： Michael Markwart , Jens Lohmar , Dariusz Krakowski , Martin Schmid , Torsten Stengel , Jens Elmers , Thomas Scherer
CPC分类号： B64D13/00 , B64D2013/0688
摘要： 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.
摘要翻译： 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：US20140302765A1
公开(公告)日：2014-10-09
申请号：US14310381
申请日：2014-06-20
发明人： Dietrich Lampe , Thomas Scherer
IPC分类号： B64D13/08
CPC分类号： B64D13/08 , B64D13/06 , B64D2013/0666 , B64D2013/0688 , Y02T50/56
摘要： A mixing device that is particularly suitable for use in an aircraft air-conditioning system comprising a cold air supply line adapted to supply cold air to the mixing device. A first recirculation air supply line is adapted to supply recirculation air to the mixing device. A mixing chamber is connected to the cold air supply line and the first recirculation air supply line and is adapted to supply the cold air supplied to the mixing device via the cold air supply line with the recirculation air supplied to the mixing device via the first recirculation air supply line. The first recirculation air supply line has a heat transfer portion which is thermoconductively connected to an area of a wall delimiting the mixing chamber that is at risk of icing.
摘要翻译： 一种特别适用于飞机空调系统的混合装置，包括适于向混合装置供应冷空气的冷气供应管线。 第一再循环空气供应管线适于向混合装置供应再循环空气。 混合室连接到冷气供应管线和第一再循环空气供应管线，并且适于经由冷气供应管路供应到混合装置的冷空气，再循环空气通过第一再循环供给到混合装置 供气线。 第一再循环空气供应管线具有热传导部分，其传热连接到限定混合室的壁的区域，该混合室处于结冰的风险。
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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
发明人： Michael Markwart , Jens Lohmar , Dariusz Krakowski , Martin Schmid , Torsten Stengel , Jens Elmers , Thomas Scherer
IPC分类号： B64D13/08
CPC分类号： B64D13/00 , B64D2013/0688
摘要： 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.
摘要翻译： 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：US09869477B2
公开(公告)日：2018-01-16
申请号：US14296593
申请日：2014-06-05
发明人： Dietrich Lampe , Thomas Scherer , Jens Lohmar , Michael Markwart , Martin Schmid
CPC分类号： F24F3/12 , B64D13/00 , B64D2013/0655 , Y02T50/56
摘要： A mixer assembly for an air-conditioning system comprising a recirculation air line, connectable to a vehicle region to be air-conditioned, to remove recirculation air from the region, and an air-conditioning air line, connectable to an air-conditioning unit to remove conditioned air from the air-conditioning unit. A first mixing region, for mixing the recirculation air with the conditioned air, is connected to the two air lines. A second mixing region, for mixing the first mixing region air with recirculation air, is connected to the recirculation air line and the first mixing region. Also, a first supply line is connected to the first mixing region to supply air from the first mixing region to a first partial region of the vehicle region, and a second supply line is connected to the second mixing region to supply air from the second mixing region to a second partial region of the vehicle region.
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公开(公告)号：US20140287672A1
公开(公告)日：2014-09-25
申请号：US14296593
申请日：2014-06-05
发明人： Dietrich Lampe , Thomas Scherer , Jens Lohmar , Michael Markwart , Martin Schmid
IPC分类号： F24F3/12
CPC分类号： F24F3/12 , B64D13/00 , B64D2013/0655 , Y02T50/56
摘要： A mixer assembly for an air-conditioning system comprising a recirculation air line, connectable to a vehicle region to be air-conditioned, to remove recirculation air from the region, and an air-conditioning air line, connectable to an air-conditioning unit to remove conditioned air from the air-conditioning unit. A first mixing region, for mixing the recirculation air with the conditioned air, is connected to the two air lines. A second mixing region, for mixing the first mixing region air with recirculation air, is connected to the recirculation air line and the first mixing region. Also, a first supply line is connected to the first mixing region to supply air from the first mixing region to a first partial region of the vehicle region, and a second supply line is connected to the second mixing region to supply air from the second mixing region to a second partial region of the vehicle region.
摘要翻译： 一种用于空调系统的混合器组件，包括可连接到待空调的车辆区域的循环空气管线，以从该区域移除再循环空气，以及可连接到空调单元的空调空气管路 从空调机组中取出调节空气。 用于将再循环空气与调节空气混合的第一混合区域连接到两条空气管线。 用于将第一混合区域空气与再循环空气混合的第二混合区域连接到再循环空气管线和第一混合区域。 此外，第一供给管线连接到第一混合区域以将空气从第一混合区域供应到车辆区域的第一部分区域，并且第二供应管线连接到第二混合区域以从第二混合区域供应空气 区域到车辆区域的第二部分区域。
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公开(公告)号：US20190161196A1
公开(公告)日：2019-05-30
申请号：US16165154
申请日：2018-10-19
发明人： Thomas Heuer , Patrick Bäumle , Thomas Scherer
IPC分类号： B64D13/08
摘要： An air-conditioning system for an aircraft has a fresh air line, a recirculation device, an air-mixing device, an air distribution system with multiple cabin air outlets, and a control unit. The control unit is designed to determine or to receive flight-specific parameters characterizing the flight state of the aircraft, and to determine or to receive environment-specific parameters which characterize an air quality in the environment of the aircraft. A first operating state of the air-conditioning system is brought about in the case of a predefined limit value of at least one environment-specific parameter being exceeded, and a second operating state of said system is brought about during a second flight state, which is outside the first flight state. In the second operating state, the fresh air line is fluidically connected to the air-mixing device, and in the first operating state, the fresh air line is separated from the air-mixing device.
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