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61. 发明公开

EP3617069A1 AIRCRAFT VERTICAL STABILIZER HAVING A LIFT PROPELLER AND THE METHOD OF USING THE SAME 审中-公开
公开(公告)号：EP3617069A1
公开(公告)日：2020-03-04
申请号：EP19185667.3
申请日：2019-07-11
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64C39/04 , B64C29/00 , B64C39/02 , B64C39/12
摘要： An aircraft design where the one or multiple numbers of vertical stabilizer (304) each has a lifting propeller (310).

62. 发明公开

EP4242114A1 DATA MONITORING METHOD, SYSTEM, EQUIPMENT AND MEDIUM 审中-公开
公开(公告)号：EP4242114A1
公开(公告)日：2023-09-13
申请号：EP23160562.7
申请日：2023-03-07
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64D45/00 , B64C27/00
摘要： A data monitoring method, a data monitoring system, data monitoring equipment and a data monitoring medium. The method has: acquiring current vibration data of a target flight device in real time (S110); Determining an anomaly protection strategy of the target flight device based on the current vibration data (S120); The target flight equipment is controlled to execute corresponding operations (S130) according to an abnormality protection strategy. Embodiments of the invention, by acquiring the current vibration data of the target flight equipment in real time, determining an anomaly protection strategy of the target flight device based on the current vibration data.

63. 发明公开

EP4223650A1 TRANSPORT VEHICLE AND AN UNMANNED AERIAL VEHICLE 审中-公开
公开(公告)号：EP4223650A1
公开(公告)日：2023-08-09
申请号：EP23155332.2
申请日：2023-02-07
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64U80/10 , B60P1/44 , B64U80/70 , B64U80/86
摘要： A transport vehicle and an unmanned aerial vehicle (UAV) having a head (1), a control assembly arranged in the head (1) used for controlling the movement state of the transport vehicle. The carrying plate (2) is connected to the head (1) to form an open carriage space so as to accommodate container (3). The container (3) is provided on the carrying plate (2) and at least comprises a base plate (31) and an opening (32). The base plate (31) is provided with an overturning assembly (4), the overturning assembly (4) is rotatably connected to the base plate (31) and is used for driving the piece to be transported to rotate from a first predetermined position around the side direction of the base plate (31) until the piece to be transported is arranged at a second predetermined position through the opening (32).

64. 发明公开

EP4180676A1 AN UNMANNED AERIAL VEHICLE (UAV) 审中-公开
公开(公告)号：EP4180676A1
公开(公告)日：2023-05-17
申请号：EP22207386.8
申请日：2022-11-15
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： F16B45/02 , B64D1/22 , B64U101/64
摘要： The invention relates to the technical field of unmanned aerial vehicle (UAV) transportation, and discloses a UAV, which comprises a UAV body and a delivery structure, wherein the delivery structure comprises a mounting piece (1), a reset assembly (2) and a limiting piece (3). The reset piece (21) is configured to deform when the piece to be transported (100) is lifted, which resets to drive the piece to leave the mounting groove (11) when the piece to be transported (100) touches the ground. The first end of the limiting piece (3) is connected to the reset piece (21), and when the piece to be transported (100) is not lifted, the second end of the limiting piece (3) can be connected to the mounting piece (1) by magnet to seal the opening of the mounting groove (11).
The reset piece (21) can drive the limiting piece (3) to move so as to separate the second end from the mounting piece (1) when the piece to be transported (100) is lifted. The UAV can realize the automatic release of the piece to be transported (100), and limit the position when the piece to be transported (100) is not lifted, so as to avoid a fall from the mounting groove (11). The limiting piece (3) can open the mounting groove (11) after lifting. The invention can enable automatic decoupling of the piece to be transported (100) after landing, thereby enabling UAV convenience and high transportation efficiency.

65. 发明公开

EP4177173A1 A DEVICE FOR UNMANNED AERIAL VEHICLE TO INSTALL RAINFALL CATALYTIC BOMB 审中-公开
公开(公告)号：EP4177173A1
公开(公告)日：2023-05-10
申请号：EP22206045.1
申请日：2022-11-08
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64U10/20 , B64U10/25 , A01G15/00 , F42B12/36 , F42B15/01 , F42B15/08 , B64U101/18 , B64U101/35
摘要： The invention belongs to the technical field of unmanned aerial vehicle application and artificial rainfall, and discloses a device for unmanned aerial vehicle to install rainfall catalytic bomb which comprises an unmanned aerial vehicle, a cannonball for artificial precipitation and a cylinder, wherein the unmanned aerial vehicle is connected with the cannonball for artificial precipitation through a soft lock, the cannonballs for artificial precipitation are multiple and are wrapped in the cylinders, a second sensor is arranged in the cylinder, wing surfaces are arranged on the outer side of the cylinder, the wing surfaces are multiple and are arranged at one end of the cylinder in the long shaft direction, and one end of the soft lock is connected to the other end of the cylinder in the long shaft direction. The unmanned aerial vehicle carries the cannonball for artificial precipitation to carry out rainfall, the unmanned aerial vehicle does not need to enter a cloud layer, the unmanned aerial vehicle can safely run to reduce the accident rate, the operation is simple, and the rainfall cost is low. The position of the cannonball for artificial precipitation can be accurately monitored in real time, so that it can be conveniently and accurately thrown in and detonated. The wing surface is arranged, so that the stability and the posture adjustment of the cannonball for artificial precipitation can be controlled conveniently.

66. 发明公开

EP3950496A1 VERTICAL TAKEOFF AND LANDING UNMANNED AERIAL VEHICLE WITH A COOLING SYSTEM 审中-公开
公开(公告)号：EP3950496A1
公开(公告)日：2022-02-09
申请号：EP21190123.6
申请日：2021-08-06
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64C29/00 , B64C39/02 , B64D13/00 , B64D33/08 , B64D47/00 , B64D13/06
摘要： The invention provides a vertical takeoff and landing unmanned aerial vehicle and a cooling system for the unmanned aerial vehicle. The vertical takeoff and landing unmanned aerial vehicle comprises at least one air inlet (170A; 170B) provided on the top side of a linear support (103A; 103B) below a lift propeller, and at least one air outlet provided on the linear support (103A; 103B). In the vertical takeoff and landing stage of the unmanned aerial vehicle provided by the invention, airflow generated by rotation of a lift propeller forms a rapid-flowing spatial flow field, which can achieve efficient heat dissipation of a motor and an electronic speed controller in an arm; and in the vertical takeoff and landing unmanned aerial vehicle provided by the invention, the takeoff weight of the unmanned aerial vehicle cannot be increased, power consumption of airborne equipment cannot be increased, and interior space of the arm cannot be occupied.

67. 发明公开

EP3838750A1 MULTI-ROTOR AIRCRAFT WITH MULTI-AXIS MISALIGNMENT LAYOUT 审中-公开
公开(公告)号：EP3838750A1
公开(公告)日：2021-06-23
申请号：EP20214800.3
申请日：2020-12-17
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64C27/08 , B64C39/02
摘要： The present invention discloses a multi-rotor aircraft with a multi-axis misalignment layout, which comprises a frame (10), a plurality of upper power sources (20), a plurality of lower power sources (30), a plurality of upper propellers (40), and a plurality of lower propellers (50). The plurality of upper propellers (40) are provided at intervals and are connected to the upper part of the frame (10) through the plurality of upper power sources (20). The plurality of lower propellers (50) are provided at intervals and are connected to the lower part of the frame (10) through the plurality of lower power sources (30). In the vertical projection direction of the frame (10), the plurality of upper propellers (40) and the plurality of lower propellers (50) are staggered. The upper propellers (40) and the lower propellers (50) are staggered so that the pitch between the upper propellers (40) and the lower propellers (50) is large. The central axis of the upper power sources (20) and the central axis of the lower power sources (30) are not collinear or overlapped. In the vertical projection direction of the frame (10), the overlapping area between the upper propellers (40) and the lower propellers (50) is less. Compared with the multi-rotor aircraft in the prior art, the multi-rotor aircraft with the multi-axis misalignment layout can significantly reduce flight resistance and volume, and improve propeller efficiency at the same load capacity.

68. 发明公开

EP3828087A1 LANDING PLATFORM AND METHOD FOR UNMANNED AERIAL VEHICLE, AND CHARGING SYSTEM 审中-公开
公开(公告)号：EP3828087A1
公开(公告)日：2021-06-02
申请号：EP18927894.8
申请日：2018-07-23
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64F1/00
摘要： A UAV landing platform having movable covers to securely store/maintain/charge a UAV. The UAV may be launched from the landing platform, and the landing platform can have visual indicators to guide the landing of the UAV back onto the landing platform. There can be an optional mechanism to self-adjust/self-level the landing surface such that a UAV can safely land onto the landing platform even when the landing platform is on a traveling vehicle.

69. 发明公开

EP3828083A1 UNMANNED AERIAL VEHICLE AND CONTROL METHOD THEREOF 审中-公开
公开(公告)号：EP3828083A1
公开(公告)日：2021-06-02
申请号：EP20210076.4
申请日：2020-11-26
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64C39/02 , B64C29/00 , G05D1/00
摘要： The present invention discloses an unmanned aerial vehicle and a control method thereof. The unmanned aerial vehicle includes a control module (1), motor arms (2), a plurality of lift motors (3) and lift propellers (4). The control module (1) is used to preset a correspondence between two ends of each motor arm (2) and the corresponding lift motors (3); the control module (1) is used to control each lift motor (3) to be initiated; the control module (1) is also used to determine whether a lift motor fails, determine a target lift motor and a target position if so, and adjust the power of other lift motors in all the lift motors corresponding to the target position apart from the target lift motor. The present invention improves the flight stability and safety of the unmanned aerial vehicle.

70. 发明公开

EP3806580A1 INTEGRATED HEATING AIRSPEED TUBE AND UNMANNED AERIAL VEHICLE INCLUDING SAME 审中-公开
公开(公告)号：EP3806580A1
公开(公告)日：2021-04-14
申请号：EP20201275.3
申请日：2020-10-12
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： H05B3/42 , B64D15/12 , B64D43/02 , G01P5/165
摘要： The present invention discloses an integrated heating airspeed tube and an unmanned aerial vehicle including the same. The integrated heating airspeed tube comprises a tube body and a heating component. The tube body is provided with a heating cavity, the heating component is located inside the heating cavity, and the heating component and the tube body are integrally formed. The unmanned aerial vehicle comprises the integrated heating airspeed tube as described above. The integrated heating airspeed tube of the present invention and the unmanned aerial vehicle including the same are heated in the tube body through the heating component, so that the heating removes liquid, effectively preventing liquid from blocking the integrated heating airspeed tube, and meeting the using requirements in severe weather. At the same time, the integrated heating structure design is higher in reliability and is not easy to cause operation failure, and saves the assembly cost. The overall appearance is relatively simple and beautiful, and the transmission accuracy is high.

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