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1. 发明申请

WO2011147977A3 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：WO2011147977A3
公开(公告)日：2012-02-09
申请号：PCT/EP2011058759
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
IPC分类号： B64D13/06
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：一种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）和至少一个用于压缩空气的压缩机（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）可以补偿所需工作压力的差异。因此，空调系统（32）可以通过混合能量供应来操作。

2. 发明申请

WO2011147977A9 AIR CONDITIONING SYSTEM WITH HYBRID OPERATION FOR AN AIRCRAFT 审中-公开
标题翻译：航空器混合动力空调系统
公开(公告)号：WO2011147977A9
公开(公告)日：2012-03-22
申请号：PCT/EP2011058759
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
IPC分类号： B64D13/06
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线（33）和至少一个用于压缩空气的压缩机（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）可独立于引气而被驱动。这使得能够以比平常更低的压力分接发动机引气，因为与压缩机（36）相比可以补偿与所需运行压力的差别。空调系统（32）因此可以通过混合能量供应来操作。

3. 发明申请

WO2011038889A8 SYSTEM AND METHOD FOR COOLING AND/OR HEATING AIRCRAFT DEVICES 审中-公开
公开(公告)号：WO2011038889A8
公开(公告)日：2011-09-01
申请号：PCT/EP2010005913
申请日：2010-09-28
申请人： AIRBUS OPERATIONS GMBH , HOELLING MARC , ROTHAMMER WERNER , DITTMAR JAN , COLBERG CARSTEN , CASAS NORIEGA WILSON WILLY , ULUC OZAN , ROERING SEBASTIAN , WOLF HOLGER
发明人： HOELLING MARC , ROTHAMMER WERNER , DITTMAR JAN , COLBERG CARSTEN , CASAS NORIEGA WILSON WILLY , ULUC OZAN , ROERING SEBASTIAN , WOLF HOLGER
IPC分类号： B64D13/08
CPC分类号： B64D13/08 , B64D13/00 , B64D2013/0655 , F25B49/02 , Y02T50/44 , Y02T50/56
摘要： A system (10) for cooling and/or heating aircraft devices to be cooled and/or heated comprises a first individual cooling and/or heating system (20, 22) associated with a first aircraft device (12, 14) to be cooled and/or heated, and a second individual cooling and/or heating system (24, 26) associated with a second aircraft device (16, 18) to be cooled and/or heated. The system (10) further comprises a cooling and/or heating energy supply apparatus (28) which is designed to supply cooling and/or heating energy generated by the first and/or the second individual cooling and/or heating system (20, 22, 24, 26) to the first and/or the second aircraft device (12, 14, 16, 18) to be cooled and/or heated. A control device (30) is designed to receive and process signals characteristic of the cooling and/or heating requirements of the first and/or the second aircraft device (12, 14, 16, 18) to be cooled and/or heated and of the load condition of the first and/or the second individual cooling and/or heating system (20, 22, 24, 26). The control device (30) is further designed to control, on the basis of said signals, the operation of the first and/or the second individual cooling and/or heating system (20, 22, 24, 26) and/or the supply of cooling and/or heating energy generated by the first and/or the second individual cooling and/or heating system (20, 22, 24, 26) to the first and/or the second aircraft device (12, 14, 16, 18) to be cooled and/or heated.

4. 发明申请

WO2011038888A8 SYSTEM AND METHOD FOR CONTROLLING AN AIRCRAFT COOLING SYSTEM 审中-公开
标题翻译：系统和方法控制飞机冷却系统
公开(公告)号：WO2011038888A8
公开(公告)日：2011-09-01
申请号：PCT/EP2010005912
申请日：2010-09-28
申请人： AIRBUS OPERATIONS GMBH , HOELLING MARC , ROTHAMMER WERNER , DITTMAR JAN , COLBERG CARSTEN , CASAS NORIEGA WILSON WILLY , ULUC OZAN , ROERING SEBASTIAN , WOLF HOLGER
发明人： HOELLING MARC , ROTHAMMER WERNER , DITTMAR JAN , COLBERG CARSTEN , CASAS NORIEGA WILSON WILLY , ULUC OZAN , ROERING SEBASTIAN , WOLF HOLGER
IPC分类号： B64D13/08
CPC分类号： B64D13/08 , B64D13/00 , B64D2013/0655 , F25B49/02 , Y02T50/44 , Y02T50/56
摘要： A system (10) for controlling a cooling system (100) for use especially on board an aircraft comprises a operating state detection unit (30) that is designed to detect operating state signals characteristic of the operating state of the cooling system (100) and/or the operating state of a plurality of cooling energy consumers (16a-d, 18a-d, 20a-d) to be supplied with cooling energy by the cooling system (100). The control system (10) further comprises a database (38) in which priority data that is dependent on the operating state and is characteristic of the priority to be given to the cooling energy consumers (16a-d, 18a-d, 20a-d) in terms of the cooling energy to be supplied in various operating states of the cooling system (100) and/or of the cooling energy consumers (16a-d, 18a-d, 20a-d), is stored for a plurality of cooling energy consumers (16a-d, 18a-d, 20a-d) to be supplied with cooling energy by the cooling system (100). A control signal generation unit (40) of the control system (10) is designed to generate control signals that control the supply of cooling energy to the cooling energy consumers (16a-d, 18a-d, 20a-d) to be supplied with cooling energy by the cooling system (100) in accordance with the operating state signals detected by the operating state detection unit (30) and the priority data stored in the database (38).
摘要翻译：一种用于控制特定的系统（10），用于在船上使用航空器冷却系统（100）包括适于检测用于冷却系统的操作条件（100）和/或操作状态的操作状态信号的运转状态检测单元（30）与冷却能量冷却能量消耗（16A-D，18A-D，20A-D）是特性被供应的多个贯通的冷却系统（100）。此外，控制系统（10）包括在其中具有冷却能量冷却能量消耗（16A-D，18A-D，20A-D）被供给通过所述冷却系统（100）的多个数据的基础（38）的操作相关的条件优先级数据被存储时，用于冷却能量消耗（16A-D，18A-D，20A-D）在所述冷却系统（100）和/或冷却能量消耗（16A-D，18A-D，20A-D）特性在供应einzuräumende冷却能量优先的各种操作条件是。控制系统的控制信号产生单元（40）（10）适于通过所述冷却系统（100）来控制冷却功率到与冷却能量冷却能量消耗（16A-D，18A-D，20A-D）控制的控制信号作为操作状态检测单元的功能被提供（30）运行状态信号中检测并存储在数据库（38），以产生优先级数据。

5. 发明申请

WO2011038888A3 SYSTEM AND METHOD FOR CONTROLLING AN AIRCRAFT COOLING SYSTEM 审中-公开
标题翻译：用于控制飞机冷却系统的系统和方法
公开(公告)号：WO2011038888A3
公开(公告)日：2011-07-14
申请号：PCT/EP2010005912
申请日：2010-09-28
申请人： AIRBUS OPERATIONS GMBH , HOELLING MARC , ROTHAMMER WERNER , DITTMAR JAN , COLBERG CARSTEN , CASAS NORIEGA WILSON WILLY , ULUC OZAN , ROERING SEBASTIAN , WOLF HOLGER
发明人： HOELLING MARC , ROTHAMMER WERNER , DITTMAR JAN , COLBERG CARSTEN , CASAS NORIEGA WILSON WILLY , ULUC OZAN , ROERING SEBASTIAN , WOLF HOLGER
IPC分类号： B64D13/08
CPC分类号： B64D13/08 , B64D13/00 , B64D2013/0655 , F25B49/02 , Y02T50/44 , Y02T50/56
摘要： A system (10) for controlling a cooling system (100) for use especially on board an aircraft comprises a operating state detection unit (30) that is designed to detect operating state signals characteristic of the operating state of the cooling system (100) and/or the operating state of a plurality of cooling energy consumers (16a-d, 18a-d, 20a-d) to be supplied with cooling energy by the cooling system (100). The control system (10) further comprises a database (38) in which priority data that is dependent on the operating state and is characteristic of the priority to be given to the cooling energy consumers (16a-d, 18a-d, 20a-d) in terms of the cooling energy to be supplied in various operating states of the cooling system (100) and/or of the cooling energy consumers (16a-d, 18a-d, 20a-d), is stored for a plurality of cooling energy consumers (16a-d, 18a-d, 20a-d) to be supplied with cooling energy by the cooling system (100). A control signal generation unit (40) of the control system (10) is designed to generate control signals that control the supply of cooling energy to the cooling energy consumers (16a-d, 18a-d, 20a-d) to be supplied with cooling energy by the cooling system (100) in accordance with the operating state signals detected by the operating state detection unit (30) and the priority data stored in the database (38).
摘要翻译：一种用于控制特定的系统（10），用于在船上使用航空器冷却系统（100）包括适于检测用于冷却系统的操作条件（100）和/或操作状态的操作状态信号的运转状态检测单元（30）由冷却系统（100）供应冷却能量的多个冷却能量消耗装置（16a-d，18a-d，20a-d）是特征性的。此外，控制系统（10）包括在其中具有冷却能量冷却能量消耗（16A-d，图18a-d，20a至d）被供给通过所述冷却系统（100）的多个数据的基础（38）的操作相关的条件优先级数据被存储时，用于冷却能量消耗（16A-d，图18a-d，20a至d）中的冷却系统（100）和/或冷却能量消耗（16A-d，图18a-d，20a至d）特性在供应einzuräumende冷却能量优先的各种操作条件是。控制系统的控制信号产生单元（40）（10）适于通过所述冷却系统（100）来控制冷却功率到与冷却能量冷却能量消耗（16A-d，图18a-d，20a至d）控制的控制信号作为操作状态检测单元的功能被提供（30）生成检测到的操作状态信号和存储在数据库（38）中的优先级数据。

6. 发明申请

WO2011038889A3 SYSTEM AND METHOD FOR COOLING AND/OR HEATING AIRCRAFT DEVICES 审中-公开
标题翻译：用于冷却和/或加热飞机设备的系统和方法
公开(公告)号：WO2011038889A3
公开(公告)日：2011-07-14
申请号：PCT/EP2010005913
申请日：2010-09-28
申请人： AIRBUS OPERATIONS GMBH , HOELLING MARC , ROTHAMMER WERNER , DITTMAR JAN , COLBERG CARSTEN , CASAS NORIEGA WILSON WILLY , ULUC OZAN , ROERING SEBASTIAN , WOLF HOLGER
发明人： HOELLING MARC , ROTHAMMER WERNER , DITTMAR JAN , COLBERG CARSTEN , CASAS NORIEGA WILSON WILLY , ULUC OZAN , ROERING SEBASTIAN , WOLF HOLGER
IPC分类号： B64D13/08
CPC分类号： B64D13/08 , B64D13/00 , B64D2013/0655 , F25B49/02 , Y02T50/44 , Y02T50/56
摘要： A system (10) for cooling and/or heating aircraft devices to be cooled and/or heated comprises a first individual cooling and/or heating system (20, 22) associated with a first aircraft device (12, 14) to be cooled and/or heated, and a second individual cooling and/or heating system (24, 26) associated with a second aircraft device (16, 18) to be cooled and/or heated. The system (10) further comprises a cooling and/or heating energy supply apparatus (28) which is designed to supply cooling and/or heating energy generated by the first and/or the second individual cooling and/or heating system (20, 22, 24, 26) to the first and/or the second aircraft device (12, 14, 16, 18) to be cooled and/or heated. A control device (30) is designed to receive and process signals characteristic of the cooling and/or heating requirements of the first and/or the second aircraft device (12, 14, 16, 18) to be cooled and/or heated and of the load condition of the first and/or the second individual cooling and/or heating system (20, 22, 24, 26). The control device (30) is further designed to control, on the basis of said signals, the operation of the first and/or the second individual cooling and/or heating system (20, 22, 24, 26) and/or the supply of cooling and/or heating energy generated by the first and/or the second individual cooling and/or heating system (20, 22, 24, 26) to the first and/or the second aircraft device (12, 14, 16, 18) to be cooled and/or heated.
摘要翻译：一种用于冷却和/或加热系统（10）被冷却和/或加热的空气的车载设备包括具有Einzelkühl-和/或加热模块（20相关联的第一，第一被冷却和/或加热的空气的车辆设备（12，14）， 22）以及与独立冷却和/或加热系统（24,26）相关联的第二待冷却和/或加热飞行器装置（16,18）。该系统（10）还包括冷却和/或加热能量供给装置，其适于通过所述第一和/或第二Einzelkühl-和/或加热单元产生的（28）（20，22，24，26）的冷却和/或第一和/或第二要被冷却和/或加热的飞行器装置（12,14,16,18）供给的能量。的控制装置（30），适合于接收和所需的第一和/或第二的冷却和/或加热需求的过程信号被冷却和/或加热的空气的车辆设备（12，14，16，18）和第一和/或第二单个冷却和/或加热系统（20,22,24,26）的负载状况是特征性的。另外，控制装置（30）适于将这些信号的第一和/或第二Einzelkühl-和/或-heizsystems的操作（20，22，24，26）和/或冷却的供给的基础上和/ 或者从所述第一和/或第二Einzelkühl-和/或产生的热能-heizsysteme（20，22，24，26）到所述第一和/或第二被冷却和/或（被加热的空气的车辆设备12， 14，16，18）。

7. 发明申请

WO2011026844A3 SYSTEM AND METHOD FOR COOLING AT LEAST ONE HEAT-PRODUCING DEVICE IN AN AIRCRAFT 审中-公开
标题翻译：系统和方法用于冷却至少一个发热设备放在飞机
公开(公告)号：WO2011026844A3
公开(公告)日：2011-08-11
申请号：PCT/EP2010062734
申请日：2010-08-31
申请人： AIRBUS OPERATIONS GMBH , MUEHLTHALER GEORG , ERDLE ANJA , DITTMAR JAN , ROERING SEBASTIAN , TERZI CHERIF , BLENNER JEAN
发明人： MUEHLTHALER GEORG , ERDLE ANJA , DITTMAR JAN , ROERING SEBASTIAN , TERZI CHERIF , BLENNER JEAN
IPC分类号： B64D13/08
CPC分类号： B64D13/08 , B64D2013/0614 , F25B29/003 , Y02T50/56
摘要： A system (2) for cooling at least one heat-producing device (4) in an aircraft has at least one coolant circuit. A coolant absorbs heat from the heat-producing device (4), and dissipates heat via a heat dissipation apparatus (8) to the area surrounding the aircraft. A temperature spreading apparatus (14) reduces the temperature of the coolant in an inlet (10) of the coolant circuit, and increases the heat dissipation temperature of the heat dissipation apparatus (8) in comparison to the temperature of the coolant in an outlet (12) of the coolant circuit. This makes it possible to avoid the normal ram-air channels or systems which consume precooled air in the prior art, which make avionics cooling or the like difficult, particularly when the aircraft is on the ground on hot days.
摘要翻译：一种用于在飞行器中冷却至少一个发热装置（4）的系统（2）包括至少一个冷却剂回路。冷却剂从热发生装置（4）吸收热量，并通过热传递装置（8）连接到飞机的环境释放热量。的温度差速装置（14），降低了制冷剂回路的流（10）的冷却剂的温度并提高了传热装置（8）的相对的热排放温度的冷却剂的冷却剂回路的跟随器（12）的温度。因此，共同的冲压空气通道或预冷却的空气消耗系统可以在现有技术中被避免，航空电子设备冷却或可能是困难特别是在像在飞机的底部停留热天。

8. 发明专利

BRPI0818111A2 Processo de gerenciamento dos efluentes térmicos de uma aernave, dispositivo de resfriamento de uma aeronave e aeronave. 未知
公开(公告)号：BRPI0818111A2
公开(公告)日：2015-03-31
申请号：BRPI0818111
申请日：2008-11-12
申请人： AIRBUS GMBH , DITTMAR JAN , AIRBUS OPERATIONS SAS
发明人： BULIN GUILLAUME , DITTMAR JAN
IPC分类号： B64D37/34 , F02C7/18

9. 发明申请

WO2009068807A3 METHOD FOR CONTROLLING THERMAL EFFLUENTS GENERATED BY AN AIRCRAFT AND COOLING DEVICE FOR AN AIRCRAFT IMPLEMENTING SAID METHOD 审中-公开
标题翻译：用于控制飞行器产生的热流的方法和用于飞机的冷却装置实施所述方法
公开(公告)号：WO2009068807A3
公开(公告)日：2009-12-03
申请号：PCT/FR2008052028
申请日：2008-11-12
申请人： AIRBUS OPERATIONS SAS , AIRBUS GMBH , BULIN GUILLAUME , DITTMAR JAN
发明人： BULIN GUILLAUME , DITTMAR JAN
IPC分类号： B64D37/34 , F02C7/18
CPC分类号： B64D37/34 , B64D33/10 , B64D2013/0614 , B64D2013/0659 , F02C7/224 , Y02T50/54 , Y02T50/545 , Y02T50/671
摘要： The invention relates to a method for controlling the thermal effluents of an aircraft including an airframe (110) and at least one propulsion unit (112), wherein said at least one propulsion unit (112) includes a turbomachine (116) supplied with fuel via a fuel supply circuit (122) extending from a tank (124) provided at the airframe (110), said airframe (110) including at least one thermal effluent source (134), characterised in that it comprises scattering at least partially, at the level of at least one propulsion unit (112), the thermal effluents generated at the airframe (110) by using the fuel used for supplying the turbomachine (116) as a heat-carrier fluid.
摘要翻译：本发明涉及一种用于控制飞行器的热流出物的方法，所述飞机包括机身（110）和至少一个推进单元（112），其中所述至少一个推进单元（112）包括涡轮机（116）（110）延伸的燃料供应回路（122），所述机身（110）包括至少一个热流出物源（134），其特征在于，所述燃料供应回路包括至少部分地在所述通过使用用于供应涡轮机械（116）的燃料作为热载体流体而在机身（110）处产生热流出物。

10. 发明申请

WO2009068265A1 AIR CONDITIONING SYSTEM WITH HYBRID MODE BLEED AIR OPERATION 审中-公开
标题翻译：混合模式空调系统空调系统
公开(公告)号：WO2009068265A1
公开(公告)日：2009-06-04
申请号：PCT/EP2008010030
申请日：2008-11-26
申请人： AIRBUS GMBH , AIRBUS SAS , DITTMAR JAN , ANTOINE NICOLAS , BUCHHOLZ UWE
发明人： DITTMAR JAN , ANTOINE NICOLAS , BUCHHOLZ UWE
IPC分类号： B64D13/06
CPC分类号： B64D13/06 , B64D2013/0607 , B64D2013/0611 , B64D2013/0618 , B64D2013/0644 , B64D2013/0696 , B64D2221/00 , Y02T50/44 , Y02T50/56
摘要： The invention relates to an energy supply system for operating at least one air conditioning system (26) of an aircraft, with at least one air line network and at least one electric line network, wherein the air line network is connected to the air conditioning system and at least one bleed air connection (18, 20) for routing bleed air to the air conditioning system, the electric line network is connected to the air conditioning system and at least one electrical energy source (28) for routing electrical energy to the air conditioning system, and the air conditioning system has an electrically operable cooling device. The invention also relates to an air conditioning system and a method for air-conditioning an aircraft. By means of the energy supply system according to the invention the energy withdrawn from the power units is better adapted to the energy necessary for operating the air conditioning system and other systems - such as, for example, wing de-icing - and therefore reduces the excess fuel consumption of the aircraft.
摘要翻译：用于运行飞机的至少一个空调系统（26）的能量供应系统技术领域本发明涉及一种用于运行飞机的至少一个空调系统（26）的能量供应系统，其具有至少一个空中线路网络和至少一个电网线路，其中空中线路网络连接到空调系统和用于将空气引导到空调系统的至少一个引气连接（18,20），电线网络连接到空调系统，并且至少一个电能源（28）用于将电能引导到空气空调系统，并且空调系统具有可电动操作的冷却装置。本发明还涉及用于空调飞机的空调系统和方法。通过根据本发明的能量供应系统，从动力单元抽取的能量更好地适应于操作空调系统和其他系统所需的能量 - 例如机翼除冰 - 并因此减少飞机燃油消耗过多。

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