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1. 发明申请

WO2022014787A1 드론 스테이션 审中-公开
公开(公告)号：WO2022014787A1
公开(公告)日：2022-01-20
申请号：PCT/KR2020/014543
申请日：2020-10-22
申请人： 주시회사 휴머놀러지
发明人： 박명준
IPC分类号： B64F1/22 , B64C39/02 , B60L53/80 , E05F15/63 , F16H7/02 , B60L2200/10 , B64C2201/201 , B64C39/024 , B64F1/222 , E05Y2201/656 , E05Y2201/686 , E05Y2900/60
摘要： 본 발명은 외부 프레임(40); 상기 외부 프레임(40) 내부에 위치하는 내부 프레임(60); 상기 외부 및 내부 프레임의 상부에 위치하는 직사각형 형상의 상부 플레이트(31); 상기 상부 플레이트(31)의 상부면 각각의 모서리에 위치하는 제1 내지 제4 지지 블록(28a, 28b, 28c, 28d); 상기 제1 및 제4 지지 블록(28a, 28d) 사이에 위치하는 제1 상부 회전 축(21a) 및 제1 고정 가이드 축(26a); 상기 제2 및 제3 지지 블록(28b, 28c) 사이에 위치하는 제2 상부 회전축(21b) 및 제2 고정 가이드 축(26b); 상기 제1 및 제2 지지 블록(28a, 28b) 사이에 위치하는 제3 상부 회전축(23a) 및 제3 고정 가이드 축(22a); 상기 제3 및 제4 지지 블록(28c, 28d) 사이에 위치하는 제4 상부 회전축(23b) 및 제4 고정 가이드 축(22b); 상기 제1 고정 가이드 축(26a)와 제2 고정 가이드 축(26b) 사이에서 상기 제1 및 제2 고정 가이드 축(26a, 26b)를 따라 이동하는 제1 및 제2 이동 축(24a, 24b); 및 상기 제3 고정 가이드 축(22a)와 제4 고정 가이드 축(22b) 사이에서 상기 제3 및 제4 고정 가이드 축(22a, 22b)를 따라 이동하는 제3 및 제4 이동 축(25a, 25b)을 포함하는 것을 특징으로 하는 드론 스테이션에 관한 것이다.

2. 发明申请

WO2021242414A2 FLYING VEHICLE SYSTEMS AND METHODS 审中-公开
公开(公告)号：WO2021242414A2
公开(公告)日：2021-12-02
申请号：PCT/US2021/025985
申请日：2021-04-06
申请人： WORKHORSE GROUP INC.
发明人： RATAJCZAK, Jay , WEI, Wei , ZHANG, Haonan , BORT, Thaddeus , WILSON, Scott
IPC分类号： B64D1/02 , B64D1/08 , B64D1/12 , B64D47/00 , B64C27/02 , B60L2200/10 , B60L2240/62 , B60L5/36 , B60L50/66 , B60L53/14 , B60L53/16 , B60L53/36 , B60L53/80 , B64C1/061 , B64C1/30 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/128 , B64C2201/141 , B64C2201/165 , B64C2201/18 , B64C2201/182 , B64C2201/201 , B64C2201/208 , B64C25/001 , B64C39/024 , B64D1/10 , B64D1/22 , B64D2045/0085 , B64D27/24 , B64D31/00 , B64D41/00 , B64F1/32 , B64F1/364 , B66C1/36 , B66D1/48 , B66F19/00 , G05D1/0094 , G05D1/101 , G05D1/106 , G08G5/0069
摘要： An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, and a winch mounted to the chassis. The winch includes a reel and a motor. The reel has a line wound thereon, the line having a free end. The reel includes a circumferential channel in which a wound portion of the line is wound onto the reel. The circumferential channel includes an inner portion, an outer portion, and a passage connecting the inner portion and the outer portion. The motor is operable to rotate the reel under control of the control system to thereby cause the line to wind onto and off of the reel, thereby causing the free end of the line to raise and lower.

3. 发明申请

WO2021064385A2 SYSTEMS AND METHODS FOR AIRCRAFT 审中-公开
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
申请人： ELECTRIC AVIATION GROUP LTD
发明人： WOOD, Norman , IQBAL, Kamran
IPC分类号： 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
摘要： 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.

4. 发明申请

WO2021064379A2 SYSTEMS, ARRANGEMENTS, STRUCTURES AND METHODS FOR AIRCRAFT 审中-公开
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
申请人： ELECTRIC AVIATION GROUP LTD
发明人： WOOD, Norman , IQBAL, Kamran
IPC分类号： 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
摘要： 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.

5. 发明申请

WO2021064377A2 SYSTEMS, ARRANGEMENTS, STRUCTURES AND METHODS FOR AIRCRAFT 审中-公开
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
申请人： ELECTRIC AVIATION GROUP LTD
发明人： WOOD, Norman , IQBAL, Kamran
IPC分类号： 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
摘要： 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.

6. 发明申请

WO2022237817A1 一种电池管理系统审中-公开
公开(公告)号：WO2022237817A1
公开(公告)日：2022-11-17
申请号：PCT/CN2022/092126
申请日：2022-05-11
申请人：深圳市道通智能航空技术股份有限公司
发明人：秦威
IPC分类号： B60L58/12 , B60L58/18 , B60L2200/10
摘要：一种电池管理系统，包括：电池组（10），电量计量装置（11）和微处理器（12）；电量计量装置（11），分别与电池组（10）和微处理器（12）连接，用于检测电池组（10）的电压、电流及温度信息，确定电池组（10）的电池电量，并将电池电量传递给微处理器（12）；微处理器（12），用于根据电池电量生成用于电池管理的第一控制信号；电池组（10）至少包括两节串联的电池（101），还与微处理器（12）连接，用于向电量计量装置（11）及微处理器（12）供电。该电池管理系统将电池组（10）作为一个整体计算其电池电量，提升了电量计算精度，实现了对多电池电池组的高精度管理，提升了电池管理灵活性，同时降低了微处理器（12）的信息处理复杂度。

7. 发明申请

WO2022236337A2 SYSTEMS AND METHODS FOR REGULATING VOLTAGE FOR HYDROGEN-ELECTRIC ENGINES 审中-公开
公开(公告)号：WO2022236337A2
公开(公告)日：2022-11-10
申请号：PCT/US2022/072190
申请日：2022-05-07
申请人： ZEROAVIA, INC.
发明人： LAWES, Stephen , TEJPAL, Ritish
IPC分类号： H01M8/04111 , H01M8/04858 , H01M8/1007 , H01M8/2457 , H01M8/04537 , H01M8/04082 , B60L58/30 , B60L58/33 , H01M8/04007 , H01M8/10 , B60L2200/10 , B60L2220/42 , H01M2008/1095 , H01M2250/20 , H01M2250/407 , H01M8/04074 , H01M8/04201 , H01M8/04552 , H01M8/04873
摘要： A hydrogen-electric engine includes a fuel cell stack including a plurality of fuel cells. Each fuel cell of the plurality of fuel cells includes an anode and a cathode. The hydrogen-electric engine also includes an air compressor system configured to supply compressed air to the cathode, a hydrogen fuel source configured to supply hydrogen gas, an elongated shaft supporting the air compressor system and the fuel cell stack, and a motor assembly disposed in electrical communication with the fuel cell stack. Each fuel cell generates a voltage, as an open cell voltage, by forming water with the supplied compressed air and the supplied hydrogen gas and is electrically coupled with a clamp circuit.

8. 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.

9. 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.

10. 发明申请

WO2020152613A1 AN ELECTRICAL DRIVE SYSTEM FOR AN ELECTRICALLY DRIVEN AIRCRAFT 审中-公开
公开(公告)号：WO2020152613A1
公开(公告)日：2020-07-30
申请号：PCT/IB2020/050520
申请日：2020-01-23
申请人： H55 SA
发明人： DEMONT, Sébastien
IPC分类号： B64D27/24 , G05D1/00 , G05B9/03 , B64D27/02 , B60L15/20 , B60L2200/10 , B60L3/0084 , B60L3/0092 , B64D2027/026 , B64D2221/00 , B64D31/00 , H02P29/028 , H02P6/16
摘要： An electrical drive system for an electrically driven aircraft comprising:a power source (130);at least one motor (110);a main motor controller (222A) using at least one sensor (115) for controlling said at least one motor based on parameters measured with said sensors; a redundant motor controller (222B) for controlling said at least one motor, said redundant motor controller being sensorless.

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