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1. 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。

2. 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).

3. 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。

4. 发明申请

WO2008025462A8 COOLING SYSTEM FOR COOLING HEAT LOADS ON BOARD AN AIRCRAFT AND METHOD FOR OPERATING SUCH A COOLING SYSTEM 审中-公开
标题翻译：用于冷却飞机上的热负荷的冷却系统和用于操作这种冷却系统的方法
公开(公告)号：WO2008025462A8
公开(公告)日：2008-05-29
申请号：PCT/EP2007007295
申请日：2007-08-17
申请人： AIRBUS GMBH , EBIGT WOLFGANG , CASAS NORIEGA WILSON WILLY , FREY ANDREAS , KASTELL DIRK
发明人： EBIGT WOLFGANG , CASAS NORIEGA WILSON WILLY , FREY ANDREAS , KASTELL DIRK
IPC分类号： B64D13/00 , B64D13/06
CPC分类号： F25B25/005 , B64D13/06 , B64D2013/0629 , B64D2013/064 , B64D2013/0674 , Y02T50/44 , Y02T50/56
摘要： A cooling system (10) for cooling heat loads (28, 34) on board an aircraft comprises a cold producing device (12), a first cold carrier fluid circuit (24), which is thermally coupled to the cold producing device (12) and is connected to a first heat load (28) in order to carry off heat from the first heat load (28), and a second cold carrier fluid circuit (30), which is connected to a second heat load (34) in order to carry off heat from the second heat load. A coupling system of the cooling system (10) is adapted to selectively thermally couple the first cold carrier fluid circuit (24) to the second cold carrier fluid circuit (30) or thermally uncouple it from the second cold carrier fluid circuit (30). In a method for operating such a cooling system (10) for cooling heat loads (28, 34) on board an aircraft, the first cold carrier fluid circuit (24) is selectively thermally coupled to the second cold carrier fluid circuit (30) or thermally uncoupled from the second cold carrier fluid circuit (30) by means of the coupling system.
摘要翻译：用于冷却飞机上的热负荷（28,34）的冷却系统（10）包括冷产生装置（12），与冷产生装置（12）热耦合的第一冷载体流体回路（24）并连接到第一热负荷（28）以便从第一热负荷（28）传出热量;以及第二冷载体流体回路（30），其依次连接到第二热负荷（34）以从第二热负荷中传出热量。冷却系统（10）的联接系统适于选择性地将第一冷载体流体回路（24）热耦合到第二冷载体流体回路（30），或者使其与第二冷载体流体回路（30）热分离。在用于操作用于冷却飞机上的热负荷（28,34）的这种冷却系统（10）的方法中，第一冷载体流体回路（24）选择性地热耦合到第二冷载体流体回路（30）或通过耦合系统与第二冷载体流体回路（30）热耦合。

5. 发明专利

AT515435T 未知
公开(公告)号：AT515435T
公开(公告)日：2011-07-15
申请号：AT07801737
申请日：2007-08-17
申请人： AIRBUS OPERATIONS GMBH
发明人： EBIGT WOLFGANG , CASAS NORIEGA WILLY , FREY ANDREAS , KASTELL DIRK
IPC分类号： B64D13/00 , B64D13/06
摘要： The system (10) has a cold carrier fluid circuit (24) thermally coupled to a cold producing device (12) comprising a condenser (20), and connected to a heat load (28) to carry-off the heat from the load (28). A cold carrier fluid circuit (30) is connected to a heat load (34) to carry-off the heat from the load (34). A heat exchanger (44) in the fluid circuit (30) carries off the heat from the fluid circuit (30) to the surroundings. A coupling system selectively couples the cold carrier fluid circuits. A heat exchanger (36) is connected to one of the cold carrier fluid circuits. An independent claim is also included for a method for operating a cooling system for cooling heat loads on board in an aircraft.

6. 发明专利

BRPI0914270A2 duto de ar para fornecer ar ambiente em uma aeronave, e, método para operar o mesmo 未知
公开(公告)号：BRPI0914270A2
公开(公告)日：2015-11-03
申请号：BRPI0914270
申请日：2009-06-23
申请人： AIRBUS OPERATIONS GMBH
发明人： KASTELL DIRK , ROERING SEBASTIAN , NORIEGA WILSON WILLY CASSAS
IPC分类号： B64D33/02

7. 发明专利

DE102008009274B4 System und Verfahren zur Belüftung eines Bereichs, insbesondere eines explosionsgefährdeten Bereichs eines Luftfahrzeugs 未知
公开(公告)号：DE102008009274B4
公开(公告)日：2011-06-01
申请号：DE102008009274
申请日：2008-02-15
申请人： AIRBUS OPERATIONS GMBH
发明人： KASTELL DIRK , CASAS NORIEGA WILSON WILLY
IPC分类号： B64D37/32 , B64D13/00

8. 发明专利

RU2429992C2 СИСТЕМА ОХЛАЖДЕНИЯ ДЛЯ ОХЛАЖДЕНИЯ ТЕПЛОВОЙ НАГРУЗКИ НА БОРТУ ВОЗДУШНОГО СУДНА И СПОСОБ РАБОТЫ ТАКОЙ СИСТЕМЫ 未知
公开(公告)号：RU2429992C2
公开(公告)日：2011-09-27
申请号：RU2009109837
申请日：2007-08-17
申请人： AIRBUS OPERATIONS GMBH
发明人： EHBIGT VOL FGANG , KAZAS NORIGA VIL ZON VILLI , FREJ ANDREAS , KASTELL DIRK
IPC分类号： B64D13/00
摘要： Группаизобретенийотноситсяк техникеобработкивоздухав помещенияхвоздушногосудна. Системаохлаждения, предназначеннаядляохлаждениятепловыхнагрузокнабортувоздушногосудна, содержитохлаждающееустройство. Имеетсяпервыйконтурциркуляциитекучейсредыхладоносителя, которыйтермическисоединенс охлаждающимустройствоми присоединенк первойтепловойнагрузкес цельюотведенияотнеетепла. Имеетсявторойконтурциркуляциитекучейсредыхладоносителя, которыйприсоединенковторойтепловойнагрузкес цельюотведенияотнеетепла. Соединительнаясистемасистемыохлаждениявыполненас возможностьюобеспечения, повыбору, термическогосоединенияпервогоконтурациркуляциитекучейсредыхладоносителясовторымконтуромтекучейсредыхладоносителяилитермическогоотсоединенияпервогоконтурациркуляциитекучейсредыхладоносителяотвторогоконтурациркуляциитекучейсредыхладоносителя. Вспособеработытакойсистемыохлаждениядляохлаждениятепловыхнагрузокнабортувоздушногосуднапервыйконтурциркуляциитекучейсредыхладоносителяповыборутермическисоединяютсовторымконтуромциркуляциитекучейсредыхладоносителяилитермическиотсоединяютотвторогоконтурациркуляциитекучейсредыхладоносителяпосредствомсоединительнойсистемы. Группаизобретенийпозволяетэнергоэффективноохлаждатьтепловыенагрузки, находящиесянаразличныхуровняхтемпературы. 2 н. и 9 з.п. ф-лы, 2 ил.

9. 发明专利

CA2729473A1 AIR DUCT FOR SUPPLYING AMBIENT AIR IN AN AIRCRAFT 未知
公开(公告)号：CA2729473A1
公开(公告)日：2009-12-30
申请号：CA2729473
申请日：2009-06-23
申请人： AIRBUS OPERATIONS GMBH
发明人： KASTELL DIRK , ROERING SEBASTIAN , CASAS NORIEGA WILSON WILLY
IPC分类号： B64D33/02
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).

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