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1. 发明申请

WO2021087260A1 LANDING GEAR ACOUSTIC SHIELDS 审中-公开
公开(公告)号：WO2021087260A1
公开(公告)日：2021-05-06
申请号：PCT/US2020/058216
申请日：2020-10-30
申请人： FRION, Stéphane
发明人： FRION, Stéphane
IPC分类号： B64C25/14 , B64C25/02 , B64C25/16 , B64C7/00 , B64C25/12 , B64C25/10 , B64C25/34 , B64C25/00 , B64C25/60 , B64C25/04 , B64C25/18
摘要： Shield assemblies for an aircraft landing gear include an aerodynamic shield, a first support bracket assembly, and a second support bracket assembly. The first support bracket assembly is configured to couple with a structural member of the aircraft landing gear, to support a first end of the aerodynamic shield, and to have a first position that is fixed relative to the structural member in an x-direction, a y-direction, and a z-direction. The first support bracket assembly has a first clamp that is configured to fix the first support bracket assembly relative to the structural member in the x-direction. The second support bracket assembly is configured to support a second end of the aerodynamic shield and to have a second position that is fixed relative to the structural member in the y-direction and the z-direction.

2. 发明申请

WO2021064380A2 SYSTEMS AND METHODS FOR AIRCRAFT 审中-公开
公开(公告)号：WO2021064380A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052379
申请日：2020-10-01
申请人： ELECTRIC AVIATION GROUP LTD
发明人： WOOD, Norman , IQBAL, Kamran
IPC分类号： B64D33/08 , B64C11/02 , B64D29/00 , F02C7/12 , B60L1/02 , B60L1/20 , B60L15/2072 , B60L15/38 , B60L2200/10 , B60L2240/36 , B60L50/61 , B60L58/15 , B60T1/10 , B64C1/12 , B64C11/00 , B64C11/002 , B64C11/14 , B64C11/30 , B64C13/504 , B64C19/00 , B64C25/04 , B64C25/34 , B64C25/405 , B64C3/185 , B64C3/34 , B64C7/02 , B64D13/006 , B64D15/04 , B64D2013/0648 , B64D2027/026 , B64D2221/00 , B64D27/02 , B64D27/12 , B64D27/24 , B64D31/00 , B64D31/06 , B64D35/02 , B64D37/00 , B64D37/30 , B64D37/32 , B64D41/00 , B64D41/007 , B64D47/00 , F01D15/10 , F02C7/04 , F02C7/22 , F02C7/32 , F02C7/36 , F02C9/40 , F02D19/0626 , F02D19/0634 , F02D19/0652 , F02D19/0665 , F02D19/085 , F02D19/087 , F02D2200/0611 , F05D2220/76 , G01R31/367 , G01R31/371 , G01R31/382 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02J7/0048 , H02K7/1823
摘要： A thermal management system is provided for managing the temperature of one or more components in an aircraft nacelle. The thermal management system comprises a rotatable hub of an aircraft propulsion system, the hub comprising an aperture for facilitating airflow into the nacelle via the aperture.

3. 发明申请

WO2021064376A2 SYSTEMS AND METHODS FOR AIRCRAFT 审中-公开
公开(公告)号：WO2021064376A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052375
申请日：2020-10-01
申请人： ELECTRIC AVIATION GROUP LTD
发明人： WOOD, Norman , IQBAL, Kamran
IPC分类号： B64D33/08 , B64D29/00 , B64C7/02 , F02C7/12 , B64D27/02 , B60L1/02 , B60L1/20 , B60L15/2072 , B60L15/38 , B60L2200/10 , B60L2240/36 , B60L50/61 , B60L58/15 , B60T1/10 , B64C1/12 , B64C11/00 , B64C11/002 , B64C11/14 , B64C11/30 , B64C13/504 , B64C19/00 , B64C25/04 , B64C25/34 , B64C25/405 , B64C3/185 , B64C3/34 , B64D13/006 , B64D15/04 , B64D2013/0648 , B64D2027/026 , B64D2221/00 , B64D27/12 , B64D27/24 , B64D31/00 , B64D31/06 , B64D35/02 , B64D37/00 , B64D37/30 , B64D37/32 , B64D41/00 , B64D41/007 , B64D47/00 , F01D15/10 , F02C7/04 , F02C7/22 , F02C7/32 , F02C7/36 , F02C9/40 , F02D19/0626 , F02D19/0634 , F02D19/0652 , F02D19/0665 , F02D19/085 , F02D19/087 , F02D2200/0611 , F05D2220/76 , G01R31/367 , G01R31/371 , G01R31/382 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02J7/0048 , H02K7/1823
摘要： A thermal management system is provided for managing the temperature of one or more components in an aircraft nacelle. The thermal management system comprises an airflow generator provided within the nacelle, the airflow generator configured to generate an airflow past components within the nacelle.

4. 发明申请

WO2020180375A1 ENGINE LAYOUTS AND ASSOCIATED COMPARTMENTALIZATION OF A SYSTEM FOR A HYBRID ELECTRIC PROPULSION SYSTEM FOR AEROSPACE APPLICATION 审中-公开
公开(公告)号：WO2020180375A1
公开(公告)日：2020-09-10
申请号：PCT/US2019/065351
申请日：2019-12-10
申请人： UNITED TECHNOLOGIES ADVANCED PROJECTS, INC. , PRATT & WHITNEY CANADA CORP.
发明人： BECKER, Frank , LATULIPE, Eric , WANG, Xi
IPC分类号： B64D27/02 , B64D33/08 , B64D35/08 , B64C25/04
摘要： A power plant a for an aircraft having a hybrid-electric propulsion system including a nacelle body including therein an electric motor directly connected to a gearbox for driving a propeller, wherein the gearbox is connected directly to a heat motor for driving the propeller, and at least one heat exchanger for cooling the electric motor or the heat motor.

5. 发明申请

WO2017086834A1 ШАССИ БЕЗОПАСНОСТИ ВЗЛЕТА-ПОСАДКИ ВОЗДУШНОГО СУДНА 审中-公开
标题翻译：飞机着陆的安全底盘
公开(公告)号：WO2017086834A1
公开(公告)日：2017-05-26
申请号：PCT/RU2016/000692
申请日：2016-10-11
申请人： СТЕПАНОВ, Олег Федорович
发明人： СТЕПАНОВ, Олег Федорович
IPC分类号： B64C25/04
CPC分类号： B64C25/04
摘要： Изобретение относится к трехопорной конструкции опор шасси, снабженной дополнительной четвертой опорой шасси безопасности. Шасси безопасности взлета-посадки воздушного судна расположено в хвостовой части фюзеляжа и имеет такой вертикальный размер шасси, который обеспечивает его механический контакт с взлетно-посадочной полосой только в момент подъема носовой части фюзеляжа воздушного судна в процессе взлета-посадки воздушного судна. Достигается предотвращение соприкосновения хвостовой части фюзеляжа с взлетно-посадочной полосой в процессе взлета-посадки воздушного судна.
摘要翻译：本发明涉及设置有安全机架的附加第四支撑件的三轴承底盘支撑结构。底盘安全起飞和着陆的飞机位于机身后部并具有底架，这确保了与在飞机起飞和着陆期间起重仅飞行器的前机身的时间跑道机械接触的竖直尺寸。防止机身尾部与跑道的接触在飞机的起飞和着陆过程中实现。

6. 发明申请

WO2021064397A2 POWER MANAGEMENT SYSTEM FOR MANAGING LEVEL OF ENERGY STORAGE DEVICE IN AIRCRAFT 审中-公开
公开(公告)号：WO2021064397A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052396
申请日：2020-10-01
申请人： ELECTRIC AVIATION GROUP LTD
发明人： WOOD, Norman , IQBAL, Kamran
IPC分类号： G08G5/00 , B64D27/24 , B64D31/06 , B64D27/12 , B64D37/30 , B60L1/02 , B60L1/20 , B60L2200/10 , B60L2240/36 , B60L50/60 , B60L50/61 , B60L58/15 , B64C1/12 , B64C11/00 , B64C11/002 , B64C11/14 , B64C11/30 , B64C13/504 , B64C19/00 , B64C25/04 , B64C25/34 , B64C25/405 , B64C25/42 , B64C3/185 , B64C3/34 , B64C7/02 , B64D13/006 , B64D15/04 , B64D2013/0648 , B64D2027/026 , B64D2221/00 , B64D27/02 , B64D29/00 , B64D31/00 , B64D33/08 , B64D35/02 , B64D37/00 , B64D37/32 , B64D41/00 , B64D41/007 , B64D47/00 , F01D15/10 , F02C7/04 , F02C7/22 , F02C7/32 , F02C7/36 , F02C9/40 , F02D19/0626 , F02D19/0634 , F02D19/0652 , F02D19/0665 , F02D19/085 , F02D19/087 , F02D2200/0611 , F05D2220/76 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02K7/1823 , E60
摘要： According to the present disclosure there is provided an electrical power management system (552) for managing the level of an energy storage device (554) installed in an aircraft, the electrical power management system comprising: a receiver (556) arranged to receive second flight information relating to a second flight, the second flight subsequent to a first flight; and a processor (558) arranged to process the second flight information to determine a target level of the energy storage device suitable for use in the second flight, the electrical power management system being arranged to manage the level of the energy storage device during the first flight to achieve the target level at a target time in the first flight.

7. 发明申请

WO2021064394A2 SYSTEMS AND METHODS FOR AIRCRAFT 审中-公开
公开(公告)号：WO2021064394A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052393
申请日：2020-10-01
申请人： ELECTRIC AVIATION GROUP LTD
发明人： WOOD, Norman , IQBAL, Kamran
IPC分类号： B64C3/18 , B64C25/34 , B64D31/06 , B64D37/30 , B60L2200/10 , B60L50/61 , B60T1/10 , B64C11/00 , B64C11/002 , B64C11/02 , B64C11/14 , B64C11/30 , B64C13/50 , B64C13/504 , B64C19/00 , B64C25/04 , B64C25/405 , B64C3/185 , B64C3/34 , B64C7/02 , B64D13/006 , B64D2013/0648 , B64D2027/026 , B64D2221/00 , B64D27/02 , B64D27/12 , B64D27/24 , B64D29/00 , B64D31/00 , B64D33/08 , B64D35/02 , B64D37/00 , B64D37/32 , B64D41/00 , B64D41/007 , B64D47/00 , F01D15/10 , F02C7/04 , F02C7/22 , F02C7/32 , F02C7/36 , F02C9/40 , F02D19/0626 , F02D19/0634 , F02D19/0652 , F02D19/0665 , F02D19/085 , F02D19/087 , F02D2200/0611 , F05D2220/76 , G01R31/367 , G01R31/371 , G01R31/382 , G08G5/003 , H02J2310/44 , H02J3/14 , H02J4/00 , H02J7/0048 , H02K7/1823
摘要： An energy recovery system for an aircraft, an aircraft comprising such an energy recovery system and a method of energy recovery in an aircraft. The energy recovery system comprises: a transducer assembly arranged to selectively interact with one or more propellers of a propulsion system of the aircraft to extract energy from the propellers.

8. 发明申请

WO2021064392A2 SYSTEMS AND METHODS FOR AIRCRAFT 审中-公开
公开(公告)号：WO2021064392A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052391
申请日：2020-10-01
申请人： ELECTRIC AVIATION GROUP LTD
发明人： WOOD, Norman , IQBAL, Kamran
IPC分类号： B64C25/40 , B64C25/34 , B60T1/10 , B60L2200/10 , B60L50/61 , B64C11/00 , B64C11/002 , B64C11/02 , B64C11/14 , B64C11/30 , B64C13/50 , B64C13/504 , B64C19/00 , B64C25/04 , B64C25/405 , B64C3/185 , B64C3/34 , B64C7/02 , B64D13/006 , B64D2013/0648 , B64D2027/026 , B64D2221/00 , B64D27/02 , B64D27/12 , B64D27/24 , B64D29/00 , B64D31/00 , B64D31/06 , B64D33/08 , B64D35/02 , B64D37/00 , B64D37/30 , B64D37/32 , B64D41/00 , B64D41/007 , B64D47/00 , F01D15/10 , F02C7/04 , F02C7/22 , F02C7/32 , F02C7/36 , F02C9/40 , F02D19/0626 , F02D19/0634 , F02D19/0652 , F02D19/0665 , F02D19/085 , F02D19/087 , F02D2200/0611 , F05D2220/76 , G01R31/367 , G01R31/371 , G01R31/382 , G08G5/003 , H02J2310/44 , H02J3/14 , H02J4/00 , H02J7/0048 , H02K7/1823
摘要： An energy recovery system for an aircraft, an aircraft comprising such an energy recovery system and a method of energy recovery. The energy recovery system comprises: a transducer assembly arranged to selectively interact with one or more wheels of the aircraft to extract energy from the wheels; and an energy accumulator for storing the extracted energy.

9. 发明申请

WO2021064374A2 SYSTEMS AND METHODS FOR AIRCRAFT 审中-公开
公开(公告)号：WO2021064374A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052373
申请日：2020-10-01
申请人： ELECTRIC AVIATION GROUP LTD
发明人： WOOD, Norman , IQBAL, Kamran
IPC分类号： B64C25/04 , B64C25/40 , B64C25/34 , B64D27/24 , B64D27/12 , B64C3/18 , B64C7/02 , B64D29/00 , B64D33/08 , B64D13/00 , B64D41/00 , B60L1/02 , B60L1/20 , B60L2200/10 , B60L2240/36 , B60L50/60 , B60L50/61 , B60L58/15 , B64C1/12 , B64C11/00 , B64C11/002 , B64C11/14 , B64C11/30 , B64C13/504 , B64C19/00 , B64C25/405 , B64C25/42 , B64C3/185 , B64C3/34 , B64D13/006 , B64D15/04 , B64D2013/0648 , B64D2027/026 , B64D2221/00 , B64D27/02 , B64D31/00 , B64D31/06 , B64D35/02 , B64D37/00 , B64D37/30 , B64D37/32 , B64D41/007 , B64D47/00 , F01D15/10 , F02C7/04 , F02C7/22 , F02C7/32 , F02C7/36 , F02C9/40 , F02D19/0626 , F02D19/0634 , F02D19/0652 , F02D19/0665 , F02D19/085 , F02D19/087 , F02D2200/0611 , F05D2220/76 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02K7/1823 , E60
摘要： A propulsion management system for an aircraft, an aircraft comprising such a propulsion management system and a method of decelerating an aircraft. The aircraft comprises an air propulsion system having one or more propellers. The propulsion management system is arranged to control the air propulsion system to drive the one or more propellers in reverse in order to provide a reverse thrust.

10. 发明申请

WO2020212424A1 AIRCRAFT HAVING OUTRIGGER LANDING GEAR 审中-公开
公开(公告)号：WO2020212424A1
公开(公告)日：2020-10-22
申请号：PCT/EP2020/060595
申请日：2020-04-15
申请人： SAFRAN LANDING SYSTEMS UK LIMITED
发明人： SIMONNEAUX, Yann
IPC分类号： B64C1/26 , B64C25/04 , B64C25/10 , B64C25/12
摘要： An aircraft comprising a fuselage, a pair of wings connected to an upper portion of the fuselage, and a pair of wing support struts, each wing support strut being connected between a lower portion of the fuselage and an underside of the adjacent wing, wherein at least one centre landing gear assembly is connected to the fuselage and is configured to be retractable within the fuselage, and a respective outrigger landing gear is connected to each wing support strut, each outrigger landing gear being configured to be retractable within the respective wing support strut.

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