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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
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: 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
Abstract: 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.
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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
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: 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
Abstract: 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.
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公开(公告)号：WO2021064385A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052384
申请日：2020-10-01
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: B64C25/40 , B64D31/06 , B60L15/38 , B60L15/20 , B64C25/34 , B64D27/24 , 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 , B64C25/405 , B64C25/42 , B64C3/185 , B64C3/34 , B64C7/02 , B64D13/006 , B64D15/04 , B64D2013/0648 , B64D2027/026 , B64D2221/00 , B64D27/02 , B64D27/12 , B64D29/00 , B64D31/00 , 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 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02K7/1823 , E60
Abstract: A propulsion management system for an aircraft, an aircraft comprising such a propulsion management system and a method of aircraft takeoff. The aircraft (1) comprises one or more wheels (2), and a ground propulsion system (4) arranged to drive the one or more wheels. The propulsion management system (20) is arranged to control the ground propulsion system to drive the one or more wheels of the aircraft during a takeoff roll, the takeoff roll being subsequent to a taxiing phase.
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公开(公告)号：WO2021064379A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052378
申请日：2020-10-01
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: B64C13/04 , B64C13/50 , B60L1/02 , B60L1/20 , B60L2200/10 , B60L2240/36 , B60L50/60 , 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 , 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 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02J7/0048 , H02K7/1823 , E60
Abstract: According to the present disclosure there is provided a power system structure for an aircraft, the aircraft comprising a flight control actuator system, the power system comprising one or more energy storage devices arranged to provide power to the flight control actuator system via power cables, the energy storage device being located proximal to the flight control actuator system.
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公开(公告)号：WO2021064377A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052376
申请日：2020-10-01
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: B64D13/00 , B64C25/04 , B64C25/40 , B64D41/00 , B64D35/02 , B64D27/02 , B64D13/06 , B60L1/02 , B60L1/20 , B60L2200/10 , B60L2240/36 , B60L50/60 , B60L50/61 , B60L58/15 , B60T1/10 , B64C1/12 , B64C11/00 , B64C11/002 , B64C11/14 , B64C11/30 , B64C13/504 , B64C19/00 , B64C25/34 , B64C25/405 , B64C3/185 , B64C3/34 , B64C7/02 , B64D13/006 , B64D15/04 , B64D2013/0648 , B64D2027/026 , B64D2221/00 , B64D27/12 , B64D27/24 , B64D29/00 , B64D31/00 , B64D31/06 , B64D33/08 , 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 , G01R31/367 , G01R31/371 , G01R31/382 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02J7/0048 , H02K7/1823 , E60
Abstract: According to the present disclosure there is provided a propulsion management system for an aircraft, the aircraft comprising an air propulsion system having one or more propellers, the propulsion management system being arranged to selectively: interact a transducer assembly with the one or more propellers to extract energy from the propellers; and/or control the air propulsion system to drive the one or more propellers in reverse in order to provide a reverse thrust.
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Patent Agency Ranking
公开(公告)号：WO2021064393A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052392
申请日：2020-10-01
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: B64D33/08 , B64D29/00 , B64C7/02 , F02C7/12 , B64D27/02 , B60L1/02 , B60L1/20 , B60L2200/10 , B60L2240/36 , B60L50/60 , 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 , E60
Abstract: 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 nacelle having a profile and one or more electric components having an outer profile, the outer profile of the electric components being shaped to be conformal with the profile of the nacelle. The electric components comprise an electric motor and/or power electronics.
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公开(公告)号：WO2021064388A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052387
申请日：2020-10-01
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: B64D27/24 , B64D41/00 , 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 , B64D29/00 , B64D31/00 , B64D31/06 , B64D33/08 , 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 , G01R31/367 , G01R31/371 , G01R31/382 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02J7/0048 , H02K7/1823
Abstract: An energy recovery system (31) for an aircraft (200) is provided. The energy recovery system (31) is for an aircraft (200). The aircraft (200) comprises a plurality of motors, the plurality of motors comprising at least one driving motor (208), each driving motor (208) being configured to provide drive to a propeller (206) of a propulsion system of the aircraft (200). The energy recovery system (31) comprises a transducer assembly (212) arranged to selectively interact with rotation of the propeller (206) driven by the driving motor (208) to extract energy from the rotation.
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公开(公告)号：WO2021064378A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052377
申请日：2020-10-01
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: B64D31/06 , B64D37/30 , B60L1/02 , B60L1/20 , B60L2200/10 , B60L2240/36 , B60L50/60 , 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 , 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 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02J7/0048 , H02K7/1823 , E60
Abstract: According to the present disclosure there is provided a fluid fuel monitoring system for a vehicle arranged to be fuelled by a fluid fuel supply, the system comprising: a sensing apparatus arranged to sense a fluid flow property of the fluid fuel supply, the fluid flow property being indicative of the composition of the fluid fuel supply; and a controller arranged to control operation of the vehicle based on the fluid flow property.
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公开(公告)号：WO2021064375A2
公开(公告)日：2021-04-08
申请号：PCT/GB2020/052374
申请日：2020-10-01
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: B64C3/18 , B64C25/34 , B64D31/06 , B64D37/30 , B60L1/02 , B60L1/20 , B60L2200/10 , B60L2240/36 , B60L50/60 , B60L50/61 , B60L58/15 , B60T1/10 , B64C1/12 , B64C11/00 , B64C11/002 , B64C11/14 , B64C11/30 , B64C13/504 , B64C19/00 , B64C25/04 , B64C25/405 , B64C3/185 , B64C3/34 , B64C7/02 , B64D13/006 , B64D15/04 , 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 , H01M10/65 , H02J2310/44 , H02J3/14 , H02J4/00 , H02J7/0048 , H02K7/1823 , E60
Abstract: According to the present disclosure there is provided a spar arrangement for segregating components installed in an aircraft, the spar arrangement being locatable between the components, to provide one or more voids therebetween. Additionally, the present disclosure provides a method of segregating components installed in an aircraft, the method comprising the steps of: providing one or more spar arrangements; and locating the one or more spar arrangements between the components to provide a void therebetween.
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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
Applicant: ELECTRIC AVIATION GROUP LTD
Inventor： WOOD, Norman , IQBAL, Kamran
IPC: 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
Abstract: 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.
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