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1. 发明申请

WO2008031510A1 AIR SUPPLY SYSTEM OF AN AIRCRAFT AND METHOD FOR MIXING TWO AIR STREAMS IN AN AIR SUPPLY SYSTEM 审中-公开
标题翻译：空气供应系统和空气供应系统中混合两个空气流的方法
公开(公告)号：WO2008031510A1
公开(公告)日：2008-03-20
申请号：PCT/EP2007/007636
申请日：2007-08-31
申请人： AIRBUS DEUTSCHLAND GMBH , BARKOWSKY, Jan
发明人： BARKOWSKY, Jan
IPC分类号： B64D13/00
CPC分类号： B64D13/06 , B64D2013/0618 , B64D2013/064 , B64D2013/0648 , B64D2013/0688 , Y02T50/44 , Y02T50/56
摘要： The invention relates to an air supply system of an aircraft, in particular of a passenger aircraft, which comprises a fresh air system, through which fresh air can be supplied to an aircraft cabin, a circulating air system, which is coupled to the fresh air system and through which used cabin air can be supplied to the fresh air system, a cooling air system for cooling an air conditioning system of the aircraft disposed in the fresh air system, and a ventilation system coupled to the cooling air system for ventilating an installation space of the air conditioning system. The air supply system includes a device for fluidically coupling the cooling air system and the ventilation system. The device is disposed and configured inside the fuselage of the aircraft such that the air in one system can be driven through the air flow in the other system. The invention also relates to a method for mixing two air streams in an air supply system of this kind of an aircraft.
摘要翻译：本发明涉及飞机，特别是客机的空气供应系统，其包括新鲜空气系统，新鲜空气可以通过该空气系统供应到飞机机舱;循环空气系统，其连接到新鲜空气系统，并且通过其将二手车空气供应到新鲜空气系统，用于冷却设置在新鲜空气系统中的飞行器的空调系统的冷却空气系统，以及耦合到冷却空气系统以将设备通风的通风系统空调系统的空间。空气供应系统包括用于流体耦合冷却空气系统和通风系统的装置。该设备被布置和配置在飞行器的机身内部，使得一个系统中的空气可以被驱动通过另一个系统中的空气流。本发明还涉及一种在这种飞行器的空气供应系统中混合两种气流的方法。

2. 发明申请

WO2012045864A1 MAIN ENGINE START BY MEANS OF AN AIRCRAFT AIR CONDITIONING SYSTEM 审中-公开
标题翻译：主要发动机由飞机空调系统开始
公开(公告)号：WO2012045864A1
公开(公告)日：2012-04-12
申请号：PCT/EP2011/067563
申请日：2011-10-07
申请人： AIRBUS OPERATIONS GMBH , BARKOWSKY, Jan , DITTMAR, Jan
发明人： BARKOWSKY, Jan , DITTMAR, Jan
IPC分类号： B64D41/00
CPC分类号： F02C7/26 , B64D13/06 , B64D2013/0696
摘要： An air conditioning system in an aircraft comprises at least one air cycle air-conditioning pack with a compressor comprising a bleed air outlet and with a compressed-air line connected to the bleed air connection, which compressed-air line is connectable to a starter turbine for a main engine. With the use of air from a compressor of an air conditioning pack it is not necessary to switch off the air conditioning pack; bleed air removal from the auxiliary power units becomes obsolete; and, since there is no unnecessary discharge of compressed air from a bleed air system, noise pollution on the ground is reduced.
摘要翻译：飞行器中的空调系统包括至少一个空气循环空调组件，其具有压缩机，该空气压缩机包括排放出气口和连接到排气连接的压缩空气管路，该压缩空气管线可连接到起动涡轮机一个主机。利用来自空调包装机的压缩机的空气，不需要关闭空调包装; 从辅助动力装置排出的排气变得过时了; 并且，由于没有从排气系统排出不必要的压缩空气，因此降低了对地面的噪声污染。

3. 发明申请

WO2012045832A1 AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM WITH CONDITIONED HEAT SINK 审中-公开
标题翻译：具有调节散热器的飞机环境控制系统
公开(公告)号：WO2012045832A1
公开(公告)日：2012-04-12
申请号：PCT/EP2011/067494
申请日：2011-10-06
申请人： AIRBUS OPERATIONS GMBH , BARKOWSKY, Jan
发明人： BARKOWSKY, Jan
IPC分类号： B64D13/06 , B64D13/08
CPC分类号： B64D13/00 , B64D13/06 , B64D2013/0614 , B64D2013/0674 , Y02T50/44 , Y02T50/56
摘要： An air conditioning system (2) for an aircraft comprises at least one air conditioning pack (4) which for the purpose of heat dissipation can be connected to at least one cooling air inlet (42) of the aircraft and is designed to cool air and to introduce it at a cabin (6) pressure into a passenger cabin of the aircraft. A separately operable cooling device (16) is designed to cool the ambient air flowing into the cooling air inlet.
摘要翻译：用于飞行器的空调系统（2）包括至少一个用于散热的空调包（4），其可以连接到飞行器的至少一个冷却空气入口（42），并被设计成冷却空气和将其在舱室（6）压力下引入飞机的客舱。设计分开可操作的冷却装置（16）以冷却流入冷却空气入口的周围空气。

4. 发明申请

WO2012113541A1 COOLING AIR INLET AND METHOD FOR OPERATING A COOLING AIR INLET 审中-公开
标题翻译：冷却空气入口和操作冷却空气入口的方法
公开(公告)号：WO2012113541A1
公开(公告)日：2012-08-30
申请号：PCT/EP2012/000758
申请日：2012-02-21
申请人： AIRBUS OPERATIONS GMBH , BARKOWSKY, Jan , DITTMAR, Jan , KELNHOFER, Juergen
发明人： BARKOWSKY, Jan , DITTMAR, Jan , KELNHOFER, Juergen
IPC分类号： F01D17/10 , F02K3/115
CPC分类号： F02C7/00 , B64D2013/0618 , F01D17/105 , F02K3/115 , F05B2260/20 , F05D2260/20 , Y02T50/56 , Y02T50/676
摘要： A cooling air inlet (32) which is particularly suitable for use in an engine bleed air system (10) of an aircraft air conditioning system comprises a cooling air inlet opening (32) which opens into an inlet portion (38) of a cooling air line (28). A cooling air inlet valve (40) which is positionable in a first open position or a second open position is arranged in the inlet portion (38) of the cooling air line (28). The cooling air inlet valve (40) is adapted to effect the build-up of a first cooling air admission pressure (p 1 ) in the inlet portion (38) of the cooling air line (28) in its first open position and the build-up of a second cooling air admission pressure (p 2 ) in the inlet portion (38) of the cooling air line (28) in its second open position. The second cooling air admission pressure (p 2 ) is greater than the first cooling air inlet pressure (p 1 ).
摘要翻译：特别适用于飞机空调系统的发动机排放空气系统（10）的冷却空气入口（32）包括通向冷却空气入口部分（38）的冷却空气入口（32）线（28）。可冷却空气管路（28）的入口部（38）中设置有能够在第一打开位置或第二打开位置定位的冷却空气导入阀（40）。冷却空气入口阀（40）适于在冷却空气管线（28）的第一打开位置的入口部分（38）中累积第一冷却空气进入压力（p1）在冷却空气管线（28）的入口部分（38）中处于其第二打开位置的第二冷却空气入口压力（p2）。第二冷却空气入口压力（p2）大于第一冷却空气入口压力（p1）。

5. 发明申请

WO2011147977A2 AIR CONDITIONING SYSTEM WITH HYBRID OPERATION FOR AN AIRCRAFT 审中-公开
标题翻译：用于飞机混合操作的空调系统
公开(公告)号：WO2011147977A2
公开(公告)日：2011-12-01
申请号：PCT/EP2011/058759
申请日：2011-05-27
申请人： AIRBUS OPERATIONS GMBH , DITTMAR, Jan , BARKOWSKY, Jan , MEVENKAMP, Christoph
发明人： DITTMAR, Jan , BARKOWSKY, Jan , MEVENKAMP, Christoph
CPC分类号： B60H1/00 , B64D13/00 , B64D13/06 , B64D2013/0618 , B64D2013/064 , B64D2013/0644 , Y02T50/44 , Y02T50/56
摘要： A system (32) for air conditioning an aircraft cabin comprises at least one cooling circuit (40, 42), at least one compressed-air line (33) and at least one compressor (36) for compressing air. The cooling circuit (40, 42) is connected to the compressor (36) by way of the compressed-air line (33), wherein the compressor (36) is drivable independently of bleed air. This makes it possible to tap engine bleed air at a lower pressure than usual, because an arising difference from a required operating pressure can be compensated for by the compressor (36). The air conditioning system (32) can thus be operated by means of a hybrid energy supply.
摘要翻译：用于空调飞机机舱的系统（32）包括至少一个冷却回路（40,42），至少一个压缩空气管路（33）和用于压缩空气的至少一个压缩机（36）。冷却回路（40,42）通过压缩空气管路（33）连接到压缩机（36），其中压缩机（36）独立于排放空气被驱动。这使得可以以比通常更低的压力来抽取发动机排放空气，因为与压缩机（36）可以补偿所需操作压力的差异。因此，空调系统（32）可以通过混合能量供应来操作。

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