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1. 发明授权

EP2980901B1 Improved cooling concept for a fuel cell system for a vehicle and aircraft having such a fuel cell system 有权
公开(公告)号：EP2980901B1
公开(公告)日：2018-10-24
申请号：EP14179124.4
申请日：2014-07-30
申请人： Airbus Operations GmbH
发明人： Klewer, Guido , Lüdders, Hauke-Peer
IPC分类号： H01M8/04029 , H01M8/04701 , H01M8/04044 , H01M8/04089 , H01M8/04007
CPC分类号： H01M8/04074 , B64D41/00 , B64D2041/005 , H01M8/04029 , H01M8/04044 , H01M8/04067 , H01M8/04089 , H01M8/04723 , H01M8/04731 , H01M2250/20 , Y02T90/32
摘要： A fuel cell system (2) for a vehicle comprises at least one fuel cell (4), at least one fuel cell heat exchanger (10) arranged in or at the at least one fuel cell (4) for receiving heat of the at least one fuel cell (4), at least one thermal dissipation unit (26), at least one additional heat exchanger (18, 28) and a cooling loop (12) having a plurality of fluid line segments for conveying a coolant. The at least one fuel cell heat exchanger (10) is coupled with the at least one thermal dissipation unit (26) through the cooling loop (12), and the additional heat exchanger (18, 28) is arranged in the cooling loop (12) and is adapted for receiving heat from an external source and for raising the temperature of a coolant flowing in the cooling loop (12).

2. 发明公开

EP3344545A1 A VEHICLE COMPRISING AN ENGINE RESTART SYSTEM 有权
公开(公告)号：EP3344545A1
公开(公告)日：2018-07-11
申请号：EP16760141.8
申请日：2016-08-26
申请人： BAE SYSTEMS plc
发明人： WOODHOUSE, Gordon, Charles , BOSTON, Luke, Michael
IPC分类号： B64D31/06 , B64D45/04 , G05D1/10
CPC分类号： B64D31/06 , B64C39/024 , B64C2201/141 , B64D41/00 , B64D45/04 , B64D2041/005 , B64D2045/0085 , G05D1/0088 , G05D1/105 , G07C5/0808 , Y02T50/54
摘要： A vehicle (100) comprising: an engine (102); a system for starting the engine (102); a fault detection module (120); an electrical power source (110); and a controller (116, 122). The controller (116, 122) is configured to, responsive to the fault detection module (120) detecting a fault occurring with the engine (102): determine a window in which to attempt to start the engine (102); control the electrical power source (110) to provide electrical power to the system for starting the engine (102); and control the system for starting the engine (102) to attempt to start the engine (102) using the supplied electrical power only during the determined window.

3. 发明授权

EP2979731B1 Supply system and method for providing electric energy, oxygen depleted air and water as well and aircraft having such a supply system 有权
公开(公告)号：EP2979731B1
公开(公告)日：2018-05-30
申请号：EP14178937.0
申请日：2014-07-29
申请人： Airbus Operations GmbH
发明人： Hoffjann, Claus , Law, Barnaby , Klewer, Guido , Lüdders, Hauke-Peer
IPC分类号： A62C3/08 , B64D37/32 , H01M8/06 , B64D41/00 , A62C99/00 , A62D1/00 , B01J19/00 , C01B5/00 , H01M8/04828 , H01M8/04858 , H01M8/04119 , H01M8/04291 , H01M8/04746
CPC分类号： A62C3/08 , A62C5/008 , A62C99/0018 , A62D1/0092 , B01J19/0006 , B01J19/0053 , B01J2219/00186 , B01J2219/00761 , B64D37/32 , B64D2041/005 , C01B5/00 , H01M8/04164 , H01M8/04291 , H01M8/04761 , H01M8/04843 , H01M8/04932 , H01M2220/20 , H01M2250/20 , Y02T50/44 , Y02T90/32 , Y02T90/36
摘要： A supply system(2) for providing at least oxygen depleted air and water in a vehicle, the system (2) comprising a catalytic converter (4), at least one hydrogen supply means (6), at least one air supply means (12, 14), at least one outlet for oxygen depleted air, and a control unit (46) coupled with the catalytic converter (4). The catalytic converter is couplable with the hydrogen supply means and is adapted for producing water under consumption of hydrogen from the at least one hydrogen supply means and oxygen. The catalytic converter is further couplable with the at least one air supply means for additionally producing oxygen depleted air. Further, the control unit is adapted for selectively operating the catalytic converter based on a demand of water and oxygen depleted air.

4. 发明公开

EP3231032A2 AUTONOMOUS AIRCRAFT FUEL CELL SYSTEM 有权
标题翻译：自主飞机燃料电池系统
公开(公告)号：EP3231032A2
公开(公告)日：2017-10-18
申请号：EP15820622.7
申请日：2015-12-09
申请人： Zodiac Aerotechnics
发明人： FILANGI, Sébastien , D'ARBIGNY, Julien , BOUILLO, Loic , ELLEBOODE, Christophe , MASSET, Franck , GAGER, Guillaume , MARTY, Claire , ZRAIAA, Hanane
IPC分类号： H01M8/2475 , B60L11/18 , H01M16/00 , H02J3/28 , H02J3/38 , H01M8/04082
CPC分类号： B64D41/00 , B60L11/1883 , B60L11/1887 , B60L2200/10 , B64D27/24 , B64D31/06 , B64D2041/005 , B64D2221/00 , H01M8/04201 , H01M8/2475 , H01M16/006 , H01M2250/20 , H02J3/387 , Y02E60/721 , Y02T90/32 , Y02T90/34 , Y04S10/126
摘要： Embodiments of the present disclosure relate generally to systems and methods for providing improved aircraft fuel cell systems. In one embodiment, the system provides separate zones, maintaining various equipment components in separate controlled hydrogen concentration zones. In one embodiment, the fuel cell system provided may be simpler such that it functions without a power converter and autonomous such that it functions without need for power from any aircraft supply.
摘要翻译：本公开的实施例总体上涉及用于提供改进的飞机燃料电池系统的系统和方法。在一个实施例中，系统提供单独的区域，将各种设备部件维持在单独的受控氢浓度区域中。在一个实施例中，所提供的燃料电池系统可以更简单，使得其在没有功率转换器的情况下起作用并且是自主的，使得其起作用而不需要来自任何飞机供应的电力。

5. 发明公开

EP3199791A1 TURBOFAN HYBRID PROPULSION SYSTEM 审中-公开
标题翻译： TURBOFAN混合推进系统
公开(公告)号：EP3199791A1
公开(公告)日：2017-08-02
申请号：EP17151918.4
申请日：2017-01-18
申请人： General Electric Company
发明人： SENNOUN, Mohammed El Hacin
IPC分类号： F02K3/06 , F02C6/00 , F02C7/12 , F02C7/36
CPC分类号： F02C3/305 , B64D27/24 , B64D2027/026 , B64D2041/005 , F02C6/00 , F02C6/206 , F02C7/00 , F02C7/12 , F02C7/36 , F02K3/06 , F05D2260/40311 , H01M8/00 , H01M8/0618 , H01M2250/20 , Y02T50/64 , Y02T50/675 , Y02T90/32 , Y02T90/36
摘要： An aeronautical propulsion system including a turbine engine having a fan (38) and an electric motor (82) drivingly coupled to at least one of the fan (38) or the turbine engine. The aeronautical propulsion system additionally includes a fuel cell (86) for providing electrical energy to the electric motor (82), the fuel cell (86) generating water as a byproduct. The aeronautical portion system directs the water generated by the fuel cell (86) to the turbine engine during operation to improve an efficiency of the aeronautical propulsion system.
摘要翻译：一种包括涡轮发动机的航空推进系统，该涡轮发动机具有风扇（38）和驱动地联接到风扇（38）或涡轮发动机中的至少一个的电动机（82）。航空推进系统还包括用于向电动机（82）提供电能的燃料电池（86），燃料电池（86）产生水作为副产品。航空部分系统在运行期间将由燃料电池（86）产生的水引导至涡轮发动机，以提高航空推进系统的效率。

6. 发明授权

EP2772436B1 Aircraft inerting system 有权
标题翻译：飞机惰化系统
公开(公告)号：EP2772436B1
公开(公告)日：2017-04-26
申请号：EP14156709.9
申请日：2014-02-26
申请人： Airbus Operations Limited , Airbus Operations GmbH
发明人： Tichborne, Franklin , Hughes, Brian , Renouard-Vallet, Gwénaëlle Marie Lucette , Burnell, Stephen Edward
IPC分类号： B64D41/00 , B64D37/06 , B64D37/32
CPC分类号： B64D37/32 , B64D37/06 , B64D2041/005 , Y02T50/44 , Y02T90/36 , Y10T137/0379 , Y10T137/3099

7. 发明授权

EP2213571B2 Localized utility power system for aircraft 有权
标题翻译： Lokales Leistungssystemfürein Luftfahrzeug
公开(公告)号：EP2213571B2
公开(公告)日：2017-01-11
申请号：EP10250159.0
申请日：2010-01-29
申请人： The Boeing Company
发明人： Breit, Joseph Sherman , Witting, Michael Neil , Laib, Trevor , Rankin, Richard L. , Trela, John Anthony , Gates, Markland T. , Mansouri, Ali Reza
IPC分类号： B64D11/02 , B64D11/04
CPC分类号： B64D11/02 , B64D11/04 , B64D2041/005 , Y02T50/46 , Y02T90/36 , Y10T307/344

8. 发明授权

EP2683610B1 HYDRODYNAMIC RAM MITIGATING FUEL TANK STRUCTURE 有权
标题翻译：水动力减弱PUSH燃料箱构造
公开(公告)号：EP2683610B1
公开(公告)日：2016-08-10
申请号：EP11867667.5
申请日：2011-06-13
申请人： Bell Helicopter Textron Inc.
发明人： SPARKS, Chad, Elliot
IPC分类号： B64D37/08
CPC分类号： F02M37/00 , B64D37/32 , B64D2037/325 , B64D2041/005 , H01M8/04089 , H01M8/04201 , H01M2250/20 , Y02E60/50 , Y02T50/44 , Y02T90/32 , Y02T90/36 , Y10T137/6906 , Y10T137/86212 , Y10T137/86228

9. 发明公开

EP3040275A1 AIRCRAFT HAVING A REDUNDANT AND EFFICIENT BLEED SYSTEM 审中-公开
标题翻译： FLUGZEUG MIT EINEM REDUNDANTEN UND EFFIZENENENTLÜFTUNGSSYSTEM
公开(公告)号：EP3040275A1
公开(公告)日：2016-07-06
申请号：EP15161787.5
申请日：2015-03-30
申请人： Airbus Operations GmbH
发明人： Hoffjann, Claus , Tappermann, Joerg , Engel, Wolfgang
IPC分类号： B64D13/06 , B64D37/32 , B64D41/00
CPC分类号： H01M8/1007 , B64D13/06 , B64D41/00 , B64D2013/0611 , B64D2013/0644 , B64D2041/005 , H01M8/04014 , H01M8/241 , H01M8/2457 , H01M2008/1095 , H01M2250/20 , H01M2300/0082 , Y02T50/44 , Y02T50/56 , Y02T90/32 , Y02T90/36
摘要： An aircraft (2) having at least one thrust providing jet engine (4, 6) and a fuselage with an integrated pressurized cabin comprises an environmental control system (16) comprising at least one pneumatic air cycle air conditioning unit (90, 92), a bleed air port (94, 96) in the at least one thrust providing jet engine (4, 6), a non thrust providing auxiliary supply unit (20) adapted for providing electricity and compressed air on ground and during flight, and at least one compressed air line (10, 36). The at least one compressed air line (10, 36) is coupled with the bleed air port (94, 96) and the auxiliary supply unit (20). The environmental control system (16) is coupled with the at least one compressed air line (10, 36). Further, the auxiliary supply unit (20) is dimensioned so as to exclusively operate the environmental control system (16) by delivering compressed air, and bleed air from the bleed air port (94, 96) is selectively providable to the environmental control system (16) for redundancy.
摘要翻译：具有至少一个推力提供喷气发动机（4,6）和具有集成加压舱的机身的飞机（2）包括环境控制系统（16），其包括至少一个气动空气循环空调单元（90,92）所述至少一个推力提供喷气发动机（4,6）中的排气口（94,96），非推力提供辅助供应单元（20），适于在地面和飞行期间提供电和压缩空气，并且至少一个压缩空气管路（10,36）。所述至少一个压缩空气管路（10,36）与所述排气口（94,96）和所述辅助供应单元（20）联接。环境控制系统（16）与至少一个压缩空气管线（10,36）联接。此外，辅助供应单元20的尺寸被设计成通过输送压缩空气专门地操作环境控制系统（16），并且可以选择地向排气口（94,96）排出空气给环境控制系统 16）冗余。

10. 发明公开

EP3037351A1 Self sufficient galley system, method for operating electrical galley devices and aircraft having such a galley system 审中-公开
标题翻译：自主厨房系统，电气设备厨房和飞行器的操作的这种系统厨房方法
公开(公告)号：EP3037351A1
公开(公告)日：2016-06-29
申请号：EP14200084.3
申请日：2014-12-23
申请人： Airbus Operations GmbH
发明人： Reiss, Matthias , Palit, Yener , Dr. Becker, Lars-Ole , Dr. Otto, Thorsten
IPC分类号： B64D11/04 , B64D41/00
CPC分类号： B64D11/04 , B64D41/00 , B64D2041/005 , H02J3/387 , H02M3/04 , H02M7/06 , H02M7/44 , Y02T50/44 , Y02T50/46 , Y02T90/36
摘要： A galley system (2) comprises at least one electrically operated galley device, a galley frame having at least one compartment for housing the at least one galley device, at least one fuel cell unit (4), and a power control and monitoring unit (12) coupled with the at least one galley device and the at least one fuel cell unit (4). The power control and monitoring unit (12) is adapted for receiving a power request signal from the at least one galley device, for determining, whether the at least one fuel cell unit (4) is able to provide the requested power and for sending an acknowledgment signal to the respective galley device, when the at least one fuel cell unit (4) is able to provide the requested power, and wherein the galley system is independent from an external power supply.
摘要翻译：甲厨房系统（2）包括至少一个电操作的厨房设备，其具有用于容纳至少一个隔室的所述至少一个厨房装置的厨房帧，至少一个燃料电池单元（4），和功率控制和监测单元（ 12）加上至少一个厨房设备和所述至少一个燃料电池单元（4）。功率控制和监测单元（12）是angepasst用于接收从所述至少一个厨房设备的功率请求信号，用于确定性采矿，无论所述至少一个燃料电池单元（4）能够提供所要求的功率和用于发送确认信号发送到respectivement厨房设备，至少一个当所述燃料电池单元（4）能够提供所要求的功率，并worin厨房系统是独立于在外部电源。

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