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1. 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.

2. 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）。

3. 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。

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

WO2009156120A8 AIR DUCT FOR SUPPLYING AMBIENT AIR IN AN AIRCRAFT 审中-公开
公开(公告)号：WO2009156120A8
公开(公告)日：2010-07-15
申请号：PCT/EP2009004513
申请日：2009-06-23
申请人： AIRBUS OPERATIONS GMBH , KASTELL DIRK , ROERING SEBASTIAN , CASAS NORIEGA WILSON WILLY
发明人： KASTELL DIRK , ROERING SEBASTIAN , CASAS NORIEGA WILSON WILLY
IPC分类号： B64D33/02
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56
摘要： The invention relates to an air duct (10) for supplying ambient air in an aircraft, comprising an air inlet (12), a duct channel section (16) extending downstream of the air inlet (12) and an air conveying device (22) which is adapted to convey ambient air through the air inlet (12) and the duct channel section (16). A flow control flap (24) closes the air inlet (12) in a first position, releases a first flow cross-section of the air inlet (12) in a second position and releases a second flow cross-section of the air inlet (12), which is larger than the first flow cross-section, in a third position. The flow control flap (24) is designed and arranged in such a manner that a first surface section (28) of the flow control flap (24) is oriented substantially parallel to an aircraft shell section (18) surrounding the air inlet (12) in the area of the air inlet (12) in the second position of the flow control flap (24) and that the first surface section (28) of the flow control flap (24) is oriented at an angle with respect to the aircraft shell section (18) surrounding the air inlet (12) in an area of the air inlet (12) in the third position of the flow control flap (14).

6. 发明申请

WO2009156120A4 AIR DUCT FOR SUPPLYING AMBIENT AIR IN AN AIRCRAFT 审中-公开
标题翻译：空气管道，用于环境的空气供应在飞机
公开(公告)号：WO2009156120A4
公开(公告)日：2010-05-20
申请号：PCT/EP2009004513
申请日：2009-06-23
申请人： AIRBUS OPERATIONS GMBH , KASTELL DIRK , ROERING SEBASTIAN , CASAS NORIEGA WILSON WILLY
发明人： KASTELL DIRK , ROERING SEBASTIAN , CASAS NORIEGA WILSON WILLY
IPC分类号： B64D33/02
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56
摘要： The invention relates to an air duct (10) for supplying ambient air in an aircraft, comprising an air inlet (12), a duct channel section (16) extending downstream of the air inlet (12) and an air conveying device (22) which is adapted to convey ambient air through the air inlet (12) and the duct channel section (16). A flow control flap (24) closes the air inlet (12) in a first position, releases a first flow cross-section of the air inlet (12) in a second position and releases a second flow cross-section of the air inlet (12), which is larger than the first flow cross-section, in a third position. The flow control flap (24) is designed and arranged in such a manner that a first surface section (28) of the flow control flap (24) is oriented substantially parallel to an aircraft shell section (18) surrounding the air inlet (12) in the area of the air inlet (12) in the second position of the flow control flap (24) and that the first surface section (28) of the flow control flap (24) is oriented at an angle with respect to the aircraft shell section (18) surrounding the air inlet (12) in an area of the air inlet (12) in the third position of the flow control flap (14).
摘要翻译：用于在飞行器中环境空气供应的空气通道（10）包括延伸所述空气入口的下游，其通过空气入口（12）和适于将环境空气的空气入口（12）（12）的流动通道段（16）和一个输送器（22）以促进所述流动通道部分（16）。一种流量控制翼片（24）在第一位置关闭所述空气入口（12）处于第二位置的空气入口（12）自由的第一流动横截面，并且在第三位置中，一个相对于该第一流动横截面放大的第二流动空气入口的横截面（12）自由，流动控制翼片（24）被设计和布置成使得在空气入口（12）的区域中的流量控制阀（24）的第二位置的流控制翼片（24）的第一表面部分（28），其与进气口平行基本上包围（12）飞机外蒙皮部分（18）对准，并且成角度地围绕所述空气入口（12）的飞机外蒙皮部分的区域中的空气入口（12）的区域中的流量控制阀（24）的第三位置时，流量控制翼片（24）的第一表面部分（28）（18 ）对齐。

7. 发明申请

WO2009156120A2 AIR DUCT FOR SUPPLYING AMBIENT AIR IN AN AIRCRAFT 审中-公开
标题翻译：空气管道，用于环境的空气供应在飞机
公开(公告)号：WO2009156120A2
公开(公告)日：2009-12-30
申请号：PCT/EP2009004513
申请日：2009-06-23
申请人： AIRBUS OPERATIONS GMBH , KASTELL DIRK , ROERING SEBASTIAN , CASAS NORIEGA WILSON WILLY
发明人： KASTELL DIRK , ROERING SEBASTIAN , CASAS NORIEGA WILSON WILLY
IPC分类号： B64D13/00
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56
摘要： The invention relates to an air duct (10) for supplying ambient air in an aircraft, comprising an air inlet (12), a duct channel section (16) extending downstream of the air inlet (12) and an air conveying device (22) which is adapted to convey ambient air through the air inlet (12) and the duct channel section (16). A flow control flap (24) closes the air inlet (12) in a first position, releases a first flow cross-section of the air inlet (12) in a second position and releases a second flow cross-section of the air inlet (12), which is larger than the first flow cross-section, in a third position. The flow control flap (24) is designed and arranged in such a manner that a first surface section (28) of the flow control flap (24) is oriented substantially parallel to an aircraft shell section (18) surrounding the air inlet (12) in the area of the air inlet (12) in the second position of the flow control flap (24) and that the first surface section (28) of the flow control flap (24) is oriented at an angle with respect to the aircraft shell section (18) surrounding the air inlet (12) in an area of the air inlet (12) in the third position of the flow control flap (14).
摘要翻译：用于在飞行器中环境空气供应的空气通道（10）包括延伸所述空气入口的下游，其通过空气入口（12）和适于将环境空气的空气入口（12）（12）的流动通道段（16）和一个输送器（22）以促进所述流动通道部分（16）。一种流量控制翼片（24）在第一位置关闭所述空气入口（12）处于第二位置的空气入口（12）自由的第一流动横截面，并且在第三位置中，一个相对于该第一流动横截面放大的第二流动空气入口的横截面（12）自由，流动控制翼片（24）被设计和布置成使得在空气入口（12）的区域中的流量控制阀（24）的第二位置的流控制翼片（24）的第一表面部分（28），其与进气口平行基本上包围（12）飞机外蒙皮部分（18）对准，并且成角度地围绕所述空气入口（12）的飞机外蒙皮部分的区域中的空气入口（12）的区域中的流量控制阀（24）的第三位置时，流量控制翼片（24）的第一表面部分（28）（18 ）对齐。

8. 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。

9. 发明专利

CA2726436A1 COOLING AN ELECTRONIC DEVICE IN AN AIRCRAFT BY CASE-BY-CASE SINGLE-PHASE OR TWO-PHASE COOLING 未知
公开(公告)号：CA2726436A1
公开(公告)日：2009-12-03
申请号：CA2726436
申请日：2009-05-13
申请人： AIRBUS OPERATIONS GMBH
发明人： REISS MATTHIAS , CASAS NORIEGA WILSON WILLY , ROERING SEBASTIAN
IPC分类号： H05K7/20 , F28D15/02
摘要： A method for cooling an electronic device in an aircraft (11) is proposed, comprising the following steps: - circulating a coolant in a cooling circuit, - cooling the electronic device (2) by means of a coolant and - emitting the heat absorbed by the coolant in an aircraft outer skin heat exchanger. The coolant at least partially evaporates during the cooling of the electronic device (2) and condenses in the aircraft outer skin heat exchanger (7). The coolant circulates on account of natural convection in the coolant circuit.

10. 发明专利

CA2774885A1 SYSTEM AND METHOD FOR CONTROLLING AN AIRCRAFT COOLING SYSTEM 未知
公开(公告)号：CA2774885A1
公开(公告)日：2011-04-07
申请号：CA2774885
申请日：2010-09-28
申请人： AIRBUS OPERATIONS GMBH
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： B64D13/00
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).

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