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71. 发明公开

EP3604132A1 HYBRID VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING DRONE 审中-公开
公开(公告)号：EP3604132A1
公开(公告)日：2020-02-05
申请号：EP19185660.8
申请日：2019-07-11
申请人： Shanghai Autoflight Co., Ltd.
发明人： Shanghai Autoflight Co., Ltd.
IPC分类号： B64C39/02 , B64C39/04 , B64C39/12
摘要： A long-distance drone 100 is disclosed having a canard body style with a main body 110, a left main wing 113, a right main wing 114, a left forewing 111, and a right forewing 112. The left forewing 111 is attached to the main body 110 forward of the left main wing 113, and the right forewing 112 is attached to the main body 110 forward of the right main wing 114. There is a left linear support 120 connecting the left forewing 111 to the left main wing 113, and a right linear support 121 connecting the right forewing 112 to the right main wing 114. A plurality of propellers 131, 132, 133, 134, 135, 136 are disposed on the left and the right linear supports 120, 121.

72. 发明公开

EP4243252A1 MOTOR SHOCK-ABSORBING STRUCTURE AND AN UNMANNED AERIAL VEHICLE USING THE SAME 审中-公开
公开(公告)号：EP4243252A1
公开(公告)日：2023-09-13
申请号：EP23160565.0
申请日：2023-03-07
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： H02K5/24 , F16F15/08 , F16F1/373
摘要： A motor shock-absorbing structure having a mounting plate (1), a shock-absorbing assembly (2) and a mounting piece. The mounting plate (1) is provided with a first mounting hole (11), and the shock-absorbing assembly (2) is provided with a shock-absorbing seat (21) and a flange bushing (22). The shock-absorbing seat (21) is embedded in the first mounting hole (11), and the shock-absorbing seat (21) is provided with a second mounting hole. The flange bushing (22) is sleeved in the second mounting hole, and the flange bushing (22) is provided with a third mounting hole (221). The mounting piece passes through the third mounting hole (221) and is configured to be connected to a motor (100). The shock-absorbing seat (21) is embedded in the first mounting hole (11) of the mounting plate (1), the flange bushing (22) is clamped between the motor (100) and the mounting plate (1).

73. 发明公开

EP4230459A1 LEAK-PROOF FUEL TANK AND AN UNMANNED AERIAL VEHICLE 审中-公开
公开(公告)号：EP4230459A1
公开(公告)日：2023-08-23
申请号：EP23157235.5
申请日：2023-02-17
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B60K15/03 , B60K15/067 , B64D37/06 , F16L5/00 , F02M37/10
摘要： A leak-proof fuel tank and an unmanned aerial vehicle wherein the leak-proof fuel tank has a tank body (1) and a fuel tank cover (2), wherein the upper surface of the tank body (1) is depressed downward to form a sealing groove (11) and the bottom of the sealing groove (11) is provided with a mounting opening (12) in vertical direction. The fuel tank cover (2) is provided with an inner cover (21), a first flange cover (22) and a first sealing part (23), wherein the inner cover (21) is arranged in the mounting opening (12). The first flange cover (22) is set on the inner cover (21); the first sealing part (23) is vertically sleeved on the inner cover (21) so that the first flange cover (22) can press the first sealing part (23) into the sealing groove (11).

74. 发明公开

EP4206077A1 UNMANNED AERIAL VEHICLE 审中-公开
公开(公告)号：EP4206077A1
公开(公告)日：2023-07-05
申请号：EP22216378.4
申请日：2022-12-23
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64U60/10 , B64U30/10 , B64U30/40 , B64U10/20 , A62C3/02
摘要： The invention relates to the field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle. The unmanned aerial vehicle of this invention includes: a fuselage (20), a water collection and emission equipment, wings (40), linear reinforcements (50), a landing gear and a vertical fin (70); the water collection and emission equipment comprises buoyancy units, a sealed cabin (32), a water pump and a water collection and emission pipe; the sealed cabin (32) is detachably connected to the fuselage (20), a compartment is arranged in the sealed cabin (32), and the water pump is arranged in the compartment; the side wall of the sealed cabin (32) in its length direction comprises at least one concave part (60) which is concave towards the direction of the inner cavity. It is used for slowing down the swaying of water; the invention provides the unmanned aerial vehicle that can reuse the water collection and emission equipment to collect and discharge water to execute the rescue task of extinguishing fire.

75. 发明公开

EP4183681A1 COMBINED VERTICAL TAKEOFF AND LANDING UAVS 审中-公开
公开(公告)号：EP4183681A1
公开(公告)日：2023-05-24
申请号：EP22208687.8
申请日：2022-11-22
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64C39/02 , B64D5/00 , B64U80/82 , B64U10/20 , B64U70/20 , B64U101/20
摘要： The invention relates to the technical field of unmanned aerial vehicle (UAV), which discloses a combined vertical takeoff and landing UAV, comprising a large vertical takeoff and landing UAV (1), a connecting device (3), and a small vertical takeoff and landing UAV (2). The connecting device (3) comprises a clamping component (31) and an adsorption component (32). The clamping component (31) includes a clamping part (311), and a clamping groove (312) is arranged on the clamping part (311). The clamping component (31) comprises a snap-fitting part (313), and a snap-fitting groove (314) is arranged on the snap-fitting part (313). The clamping groove (312) and the snap-fitting groove (314) are correspondingly set. A first holding space (321) is arranged on the clamping part (311), and a second holding space (323) is arranged on the snap-fitting part (313). The adsorption component (32) comprises a first magnetic element (322) located in the first holding space (321), and the adsorption component (32) also comprises a second magnetic element (324), which is located in the second holding space (323). The invention relates to a connecting device (3) between large and small vertical takeoff and landing UAVs (1, 2), which is provided with a clamping component (31) and an adsorption component (32) at the same time. The configuration of double connecting parts makes the connection performance of the combined vertical takeoff and landing UAV more stable and reliable.

76. 发明公开

EP4181385A1 A DELIVERY DEVICE, A DELIVERY ASSEMBLY AND AN AIRCRAFT 审中-公开
公开(公告)号：EP4181385A1
公开(公告)日：2023-05-17
申请号：EP22207379.3
申请日：2022-11-15
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： H02N15/00 , H01F6/04 , B64D1/22 , B64D17/38 , B64U101/66 , B66C1/00
摘要： The invention relates to the technical field of aircraft delivery, and discloses a delivery device, a set of delivery assembly and an aircraft. The delivery device includes a mounting part (1), a biasing part (2) and a blocking part (3). The mounting part (1) is provided with a mounting slot (11) of which the opening extends upward. The object to be delivered (100) can be hooked into the mounting slot (11). The biasing part (2) is configured to deform under the gravity of the object to be delivered (100) when it is lifted, which resets to drive the object to be delivered (100) out of the mounting slot (11) when the object to be delivered (100) falls to the ground. The blocking part (3) is configured to seal the opening of the mounting slot (11) when the object to be delivered (100) is not lifted and to open the opening of the mounting slot (11) when the object to be delivered (100) is lifted. The delivery device can realize the automatic dropping of the object to be delivered (100). It can limit the position of object to be delivered (100) which is prevented to fall out of the mounting slot (11). It can open the opening of the mounting slot (11) after lifting to enable the automatic unhooking of the object to be delivered (100) after they fall to the ground, which makes the delivery device easy to use and efficient in transporting the to-be-dropped object.

77. 发明公开

EP4147983A1 AN UNMANNED AERIAL VEHICLE (UAV) 审中-公开
公开(公告)号：EP4147983A1
公开(公告)日：2023-03-15
申请号：EP22195084.3
申请日：2022-09-12
申请人： Shanghai Autoflight Co., Ltd.
发明人： YU, Tian
IPC分类号： B64U20/20 , B64U20/65 , B64U50/11 , B64U50/13 , B64U50/19 , B64U50/23
摘要： The invention discloses an unmanned aerial vehicle (UAV). The UAV comprises a UAV body, a propeller, an engine, a motor and a battery; the engine comprises an engine body and an engine output shaft arranged on the engine body; the motor comprises stator, rotor and stator connector; the stator connector is arranged on the engine body, the rotor is coaxially arranged on the engine output shaft, and the propeller is coaxially arranged on the rotor; the battery can be discharged to provide electric energy to the motor or receive the electric energy output by the motor for charging. The UAV of the invention provides the motor rotor, propeller and engine output shaft to be coaxially connected, and the motor can be used as a generator to charge the battery by doing negative work on the engine output shaft, or as an electric motor, that is, to receive the power of the battery and do positive work on the engine output shaft to realize power output, so that the UAV can realize high energy utilization and power redundancy at the same time.

78. 发明公开

EP4129833A1 AN UNMANNED AERIAL VEHICLE (UAV) TEST BENCH 审中-公开
公开(公告)号：EP4129833A1
公开(公告)日：2023-02-08
申请号：EP22188544.5
申请日：2022-08-03
申请人： Shanghai Autoflight Co., Ltd.
发明人： YU, Tian
IPC分类号： B64F5/60 , B64F5/10 , B64C39/02
摘要： The invention discloses an unmanned aerial vehicle (UAV) test bench, which falls within the technical field of UAV test, comprising a support component (1), a universal rotating component (2), a fixing component (3) and a return component (4): the universal rotating component (2) slides along the Z direction and is arranged on the support component (1), and one end of the universal rotating component (2) can rotate in a universal way relative to the other end of the universal rotating component (2). The fixing component (3) is connected to one end of the universal rotating component (2), and the fixing component (3) is configured to fix the UAV. One end of the return component (4) is connected to the support component (1), the other end is connected to the other end of the universal rotating component (2), and the return component (4) is configured to drive the universal rotating component (2) and the fixing component (3) to reset. The lifting test and the pitching test of the UAV can be carried out on the UAV test bench provided by the invention, without multiple transfers of the UAV, thereby reducing the time required for intermediate transfers and improving the efficiency of the UAV test.

79. 发明公开

EP4129832A1 AN EXPERIMENTAL BENCH FOR A UAV PROPULSION SYSTEM AND AVIONICS EQUIPMENT 审中-公开
公开(公告)号：EP4129832A1
公开(公告)日：2023-02-08
申请号：EP22188542.9
申请日：2022-08-03
申请人： Shanghai Autoflight Co., Ltd.
发明人： YU, Tian
IPC分类号： B64F5/60 , B64F5/10 , B64C39/02
摘要： The invention discloses an experimental bench for an unmanned aerial vehicle (UAV) power system and avionics equipment, which relates to the technical field of UAV test, comprising a support component (1), a power system load-bearing component (2), an avionics equipment load-bearing component (3), a jacking component (4) and a roller component (5). A plurality of power system load-bearing components (2) are provided, and are fixedly arranged on the support components (1), respectively, and each power system load-bearing component (2) is configured to carry the power system of a UAV; the avionics equipment load-bearing component (3) is fixedly arranged on the support component (1), and the avionics equipment load-bearing component (3) is configured to bear the avionics equipment of the UAV; the output end of the jacking component (4) is fixedly connected to the bottom end of the support component (1); the roller component (5) comprises a roller stand (51) and a guide wheel (52) which is connected to the roller stand (51) through rolling, and the roller stand (51) is fixedly connected to the jacking component (4). The invention can be used for the test of power system and avionics equipment, can shorten the duration of power system test and avionics equipment test, thereby improving the efficiency.

80. 发明公开

EP3950495A1 VERTICAL TAKEOFF AND LANDING UNMANNED AERIAL VEHICLE WITH A COOLING SYSTEM 审中-公开
公开(公告)号：EP3950495A1
公开(公告)日：2022-02-09
申请号：EP21190116.0
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. Heat dissipation in an arm of an unmanned aerial vehicle is achieved by providing a forward-facing opening (190) at the front end of each of a left linear support (103A) and a right linear support (103B) of the unmanned aerial vehicle, thereby achieving the purposes of lowering temperature in the arm and protecting equipment in the arm.

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