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1. 发明申请

WO2009007094A3 AIR CONDITIONING SYSTEM FOR AIRCRAFT CABINS 审中-公开
标题翻译：飞机客舱空调系统
公开(公告)号：WO2009007094A3
公开(公告)日：2009-06-25
申请号：PCT/EP2008005564
申请日：2008-07-08
申请人： AIRBUS GMBH , CREMERS JOERG , DERLIEN HENRIK , KRICKE KLAUS-DIETER , WILKE KATJA-MARIA
发明人： CREMERS JOERG , DERLIEN HENRIK , KRICKE KLAUS-DIETER , WILKE KATJA-MARIA
IPC分类号： B64D13/06 , B64D41/00
CPC分类号： B64D13/06 , B64D2013/0611 , B64D2013/0618 , B64D2013/0648 , B64D2013/0662 , B64D2013/0688 , Y02T50/44 , Y02T50/56
摘要： The present invention relates to an air conditioning system (10) for an aircraft cabin (12) with at least one air inlet (14) for supplying air to the cabin (12), at least one air outlet (16) for discharging air from the cabin (12) and at least one compressed-air source (52, 54, 56), which is adapted to provide pressurised fresh air for supplying to the cabin (12) via the at least one air inlet (14). The air conditioning system (10) further comprises a heat exchanger (42) supplied with ram air from a ram air inlet (92) for cooling air from the compressed-air source (52, 54, 56), wherein the heat exchanger (42) is disposed upstream of the air inlet (14) of the cabin (12). It is intended that the air conditioning system (10) comprises a cabin air heat exchanger (100) which is designed to be supplied with air discharged from the cabin (12), wherein the cabin air heat exchanger (100) is disposed downstream of the at least one air outlet (16) and upstream of a point (N) at which fresh air is mixed with air from the cabin (12).
摘要翻译：本发明涉及一种用于飞机机舱（12）的空调系统（10），其具有用于向机舱（12）供应空气的至少一个空气入口（14），用于从空气出口所述舱室（12）和至少一个压缩空气源（52,54,56），所述压缩空气源适于提供加压的新鲜空气以经由所述至少一个空气入口（14）供应到所述舱室（12）。空调系统（10）还包括从冲压空气入口（92）供给冲压空气的热交换器（42），用于冷却来自压缩空气源（52,54,56）的空气，其中热交换器（42 ）设置在驾驶室（12）的进气口（14）的上游。意图在于，空调系统（10）包括设计成供应有从车厢（12）排出的空气的车厢空气热交换器（100），其中车厢空气热交换器（100）设置在至少一个空气出口（16）和新鲜空气与来自机舱（12）的空气混合的点（N）的上游。

2. 发明申请

WO2009007094A4 AIR CONDITIONING SYSTEM FOR AIRCRAFT CABINS 审中-公开
标题翻译：航空客舱空调系统
公开(公告)号：WO2009007094A4
公开(公告)日：2009-09-11
申请号：PCT/EP2008005564
申请日：2008-07-08
申请人： AIRBUS OPERATIONS GMBH , CREMERS JOERG , DERLIEN HENRIK , KRICKE KLAUS-DIETER , WILKE KATJA-MARIA
发明人： CREMERS JOERG , DERLIEN HENRIK , KRICKE KLAUS-DIETER , WILKE KATJA-MARIA
IPC分类号： B64D13/06 , B64D41/00
CPC分类号： B64D13/06 , B64D2013/0611 , B64D2013/0618 , B64D2013/0648 , B64D2013/0662 , B64D2013/0688 , Y02T50/44 , Y02T50/56
摘要： The present invention relates to an air conditioning system (10) for an aircraft cabin (12) with at least one air inlet (14) for supplying air to the cabin (12), at least one air outlet (16) for discharging air from the cabin (12) and at least one compressed-air source (52, 54, 56), which is adapted to provide pressurised fresh air for supplying to the cabin (12) via the at least one air inlet (14). The air conditioning system (10) further comprises a heat exchanger (42) supplied with ram air from a ram air inlet (92) for cooling air from the compressed-air source (52, 54, 56), wherein the heat exchanger (42) is disposed upstream of the air inlet (14) of the cabin (12). It is intended that the air conditioning system (10) comprises a cabin air heat exchanger (100) which is designed to be supplied with air discharged from the cabin (12), wherein the cabin air heat exchanger (100) is disposed downstream of the at least one air outlet (16) and upstream of a point (N) at which fresh air is mixed with air from the cabin (12).
摘要翻译：本发明涉及一种用于飞机机舱（12）的空调系统（10），所述空调系统具有至少一个用于向所述机舱（12）供应空气的空气入口（14），至少一个空气出口（16），用于从所述舱室（12）和至少一个压缩空气源（52,54,56），其适于提供加压的新鲜空气，用于经由所述至少一个空气入口（14）供应到所述舱室（12）。空调系统（10）还包括一个从冲压空气入口（92）供应冲压空气的热交换器（42），用于冷却来自压缩空气源（52,54,56）的空气，其中热交换器）设置在机舱（12）的进气口（14）的上游。目的是空调系统（10）包括舱室空气热交换器（100），其被设计成供应从舱（12）排出的空气，其中客舱空气热交换器（100）设置在客舱空气热交换器至少一个空气出口（16）和点（N）的上游，新鲜空气与来自舱室（12）的空气混合。

3. 发明申请

WO2009141400A4 INERTING SYSTEM FOR AN AIRCRAFT 审中-公开
标题翻译：飞机的增音系统
公开(公告)号：WO2009141400A4
公开(公告)日：2010-07-15
申请号：PCT/EP2009056180
申请日：2009-05-20
申请人： AIRBUS OPERATIONS GMBH , CREMERS JOERG , KRICKE KLAUS-DIETER , SCHUMACHER CHRISTIAN
发明人： CREMERS JOERG , KRICKE KLAUS-DIETER , SCHUMACHER CHRISTIAN
IPC分类号： B64D13/00 , B64D37/32
CPC分类号： B64D13/06 , B64D37/32 , B64D2013/0677 , Y02T50/44 , Y02T50/56
摘要： The invention relates to an inerting system for an aircraft, comprising at least one air separation module provided with at least one air inlet, a first air outlet and a second air outlet. Said air separation module is designed in such a manner that an incoming air flow is divided into a first air flow and a second air flow. The first airflow is enriched with oxygen in relation to the incoming air flow and is removed by the first air outlet and the second air flow is enriched with nitrogen in relation to the incoming air flow and is removed by the second air outlet. The claimed inerting system is characterised in relation to known inerting systems in that the air inlet can be connected to an air removal point in an air preparation system and that the inerting system is designed to guide the first air flow into a cabin that is to be climatised.
摘要翻译：本发明涉及一种惰性化系统用于飞行器具有至少一个空气入口，一个第一空气输出端和第二空气出口的至少一个空气分离模块。空气分离模块被配置为将输入空气流分成第一空气流和第二空气流，其特征在于，朝向所述输入空气流的第一空气流富含氧气，并在所述第一空气出口被排出，并且所述从与富氮空气的输入流和第二空气出口的第二空气流已经出院。根据本发明的惰化系统是从已知的惰化系统区分的特征在于，所述空气输入可以在空气调节系统与包括惰化系统的空气出口连接适于引导所述第一空气流中的机舱待调节。

4. 发明申请

WO2009141400A3 INERTING SYSTEM FOR AN AIRCRAFT 审中-公开
标题翻译：惰FOR A平面
公开(公告)号：WO2009141400A3
公开(公告)日：2010-04-29
申请号：PCT/EP2009056180
申请日：2009-05-20
申请人： AIRBUS OPERATIONS GMBH , CREMERS JOERG , KRICKE KLAUS-DIETER , SCHUMACHER CHRISTIAN
发明人： CREMERS JOERG , KRICKE KLAUS-DIETER , SCHUMACHER CHRISTIAN
IPC分类号： B64D13/00 , B64D37/32
CPC分类号： B64D13/06 , B64D37/32 , B64D2013/0677 , Y02T50/44 , Y02T50/56
摘要： The invention relates to an inerting system for an aircraft, comprising at least one air separation module provided with at least one air inlet, a first air outlet and a second air outlet. Said air separation module is designed in such a manner that an incoming air flow is divided into a first air flow and a second air flow. The first airflow is enriched with oxygen in relation to the incoming air flow and is removed by the first air outlet and the second air flow is enriched with nitrogen in relation to the incoming air flow and is removed by the second air outlet. The claimed inerting system is characterised in relation to known inerting systems in that the air inlet can be connected to an air removal point in an air preparation system and that the inerting system is designed to guide the first air flow into a cabin that is to be climatised.
摘要翻译：本发明涉及一种惰性化系统用于飞行器具有至少一个空气入口，一个第一空气输出端和第二空气出口的至少一个空气分离模块。空气分离模块被配置为将输入空气流分成第一空气流和第二空气流，其特征在于，朝向所述输入空气流的第一空气流富含氧气，并在所述第一空气出口被排出，并且所述从与富氮空气的输入流和第二空气出口的第二空气流排出。根据本发明的惰化系统是从已知的惰化系统区分的特征在于，所述空气输入可以在空气调节系统与包括惰化系统的空气出口连接适于引导所述第一空气流中的机舱待调节。

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