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51. 发明申请

US20210362867A1 VERTICAL TAKEOFF AND LANDING AERIAL VEHICLE AND COOLING SYSTEM 有权
公开(公告)号：US20210362867A1
公开(公告)日：2021-11-25
申请号：US17396700
申请日：2021-08-08
申请人： Shanghai Autoflight Co., Ltd.
发明人： Yu Tian
IPC分类号： B64D33/08 , B64C29/00 , B64D27/24 , B64C39/02 , B64C11/00
摘要： A vertical takeoff and landing aerial vehicle and a cooling system for the aerial vehicle. Heat dissipation in an arm of an aerial vehicle is achieved by installing a fan in a hollow interior of each of a left linear support and a right linear support of the aerial vehicle, thereby achieving the purposes of lowering temperature in the arm and protecting equipment in the arm.

52. 发明申请

US20210107678A1 INTEGRATED HEATING AIRSPEED TUBE AND UNMANNED AERIAL VEHICLE INCLUDING SAME 有权
公开(公告)号：US20210107678A1
公开(公告)日：2021-04-15
申请号：US17067686
申请日：2020-10-10
申请人： Shanghai Autoflight Co., Ltd.
发明人： Yu Tian
IPC分类号： B64D43/02 , G01P5/165 , B64D15/12
摘要： An integrated heating airspeed tube and an unmanned aerial vehicle where the integrated heating airspeed tube has 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 includes the integrated heating airspeed tube as described above. The integrated heating airspeed tube and the unmanned aerial vehicle 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.

53. 发明公开

EP4219320A1 A VERTICAL TAIL OF A COMPOSITE-WING UAV 审中-公开
公开(公告)号：EP4219320A1
公开(公告)日：2023-08-02
申请号：EP23153179.9
申请日：2023-01-25
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64U60/50 , B64U40/10 , B64U30/40 , B64U20/80 , H01R13/627
摘要： The present invention relates to the technical field of unmanned aerial vehicle (UAV) and discloses a vertical tail for a composite-wing UAV, comprising: a body (1), a rudder face section (2), a rotor section (3), a shock absorbing component (4) and a quick installation assembly of circuit (5). The body (1) includes a tail body frame (11) and a shell (12). The rudder face section (2) comprises a rudder machine (21) and a rudder surface (22). The rudder surface (22) is connected to one end of the tail for steering the directional deflection of the UAV. The rudder machine (21) is used to drive the rudder surface (22). The shock absorbing component (4) is connected to the lower end plate (111) and the shock absorbing component (4) absorbs the shock to the body (1). The quick installation assembly of circuit (5) includes a plug (51), a positioning sleeve (52) and a bias piece (513), the positioning sleeve (52) is located on the outer circumference of the plug (51) and slidingly connected to the plug (51), the bias piece (513) is set between the plug (51) and the positioning sleeve (52), the bias piece (513) can absorb the impact on the plug (51). When the composite-wing UAV lands, the shock absorbing component (4) can absorb the energy generated by the rigid impact of the composite-wing UAV with the ground, and the quick installation assembly of circuit (5) can ensure the reliable connection of the electrical system of the composite-wing UAV, thus protecting the body of the composite-wing UAV and the internal electronic devices.

54. 发明公开

EP4151540A1 HYBRID VTOL FIXED-WING AERIAL VEHICLE 审中-公开
公开(公告)号：EP4151540A1
公开(公告)日：2023-03-22
申请号：EP22196541.1
申请日：2022-09-20
申请人： Shanghai Autoflight Co., Ltd.
发明人： YU, Tian
IPC分类号： B64U10/20 , B64U10/25 , B64U50/13 , B64U20/40 , B64U101/60 , B64C39/12
摘要： A long-distance drone is disclosed having a canard wing configuration with a cabin (270) attached to a left main wing (213) and a right main wing (214). There is a left forewing (211) and a right forewing (212) connected together to form a single-piece forewing. There is a left linear support (220) connecting the left forewing (211) to the left main wing (213), and a right linear support (221) connecting the right forewing (212) to the right main wing (214). A plurality of propellers is disposed on the left and the right linear supports (220, 221).

55. 发明公开

EP4092824A2 A BATTERY TAB CONNECTION STRUCTURE AND A BATTERY PACK 审中-公开
公开(公告)号：EP4092824A2
公开(公告)日：2022-11-23
申请号：EP22174353.7
申请日：2022-05-19
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： H01M50/533
摘要： The application discloses a battery tab connection structure and a battery pack, which relates to the technical field of lithium batteries. The battery tab connection structure includes a first tab 1, a second tab 2 and a fastener 4, at least one of the first tab 1 and the second tab 2 is provided with a notch 11, the first tab 1 and the second tab 2 are inserted and fixed through the notch 11 and fit with each other, and the fastener 4 can be detachably and fixedly connected with the first tab 1 and the second tab 2. The application is provided with the notch 11 on at least one of the first tab 1 and the second tab 2, the first tab 1 and the second tab 2 are inserted and fixed through the notch 11 and fit with each other, and then detachably and fixedly connected with the first tab 1 and the second tab 2 through the fastener 4, so that the first tab 1 and the second tab 2 can ensure the insertion stability and fit of the two through the notch insertion. At the same time, it achieves the detachable fixation of the first tab 1 and the second tab 2, which is convenient for the disassembly and maintenance of a single tab, thus saving the economic cost.

56. 发明公开

EP3708492A1 VTOL AIRCRAFT WITH STEP-UP OVERLAPPING PROPELLERS 审中-公开
公开(公告)号：EP3708492A1
公开(公告)日：2020-09-16
申请号：EP20163169.4
申请日：2020-03-13
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64C29/00 , B64C11/46 , B64C39/08
摘要： A vertical takeoff and landing (VTOL) fixed-wing aircraft having overlapping propellers (131, 133, 135, 137) disposed on a top surface of each of the left and right lateral supports (130) connecting the left and right main and secondary wings (122, 124) and low hanging vertical stabilizers (140) disposed on the rear end of the aircraft. A vertical takeoff and landing (VTOL) fixed-wing aircraft having a plurality of propellers (131, 133, 135, 137) disposed on a top surface of each of the left and right lateral supports (130) connecting the left and right main and secondary wings (122, 124), wherein the propellers (134, 138) disposed at the rear end of the aircraft are vertically offset to the other propellers.

57. 发明公开

EP4257427A1 AIRCRAFT TRANSPORT TRAILER 审中-公开
公开(公告)号：EP4257427A1
公开(公告)日：2023-10-11
申请号：EP23166129.9
申请日：2023-03-31
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B60P3/11 , B64U80/86
摘要： An aircraft transport trailer having a frame (100), a wheel assembly, a lower bracket, and an upper bracket. The wheel assembly is rotationally installed on the frame (100) to support and move the frame (100). The lower bracket is fixedly installed on the frame (100), and the top of the lower bracket is provided with a body slot. The preset first surface of the inner wall of the body slot is fitted with the part of the lower surface of the body, the aircraft body can be partially seated in the aircraft body slot under the action of gravity.

58. 发明公开

EP4253227A1 QUICK-RELEASE WING STRUCTURE AND AN UNMANNED AERIAL VEHICLE USING THE SAME 审中-公开
公开(公告)号：EP4253227A1
公开(公告)日：2023-10-04
申请号：EP23164693.6
申请日：2023-03-28
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64C1/26 , B64U10/25 , B64U30/14 , F16B21/18 , F16B21/16
摘要： A quick-release wing structure includes a lock cylinder assembly and a lock head. The lock cylinder assembly is installed in the fuselage. The lock cylinder assembly includes a shell and a lock plate. An installation slot is opened inside the shell. The side wall of the installation slot is provided with a clamping hole connected with the installation slot. The lock plate is sliding and arranged in the installation slot. The lock head is installed in the wing. A locking slot is set on the periphery of the lock head. The lock head can pass through the clamping hole and drive the lock plate to move. When the locking slot is facing the lock plate, the lock head is clamped onto the locking slot and fixed. The UAV includes the quick-release wing structure described above.

59. 发明公开

EP4212715A1 ENGINE, AN AIRCRAFT, AND A THROTTLE THEREOF 审中-公开
公开(公告)号：EP4212715A1
公开(公告)日：2023-07-19
申请号：EP23151494.4
申请日：2023-01-13
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： F02M35/10 , F02C7/04 , F02C9/00 , F02D9/02 , F02D9/10 , F02C7/232 , F02M57/00
摘要： An aircraft having an engine and a throttle thereof. The throttle has a throttle body (1), the throttle body (1) is provided with a cavity (10) and comprises an inlet port (11) and an outlet port (12) both of which are connected to the cavity (10); a plurality of fuel injectors (2), each of the fuel injectors (2) is arranged on the throttle body (1) and can spray fuel into the cavity (10) of the throttle body (1); and an air filter (3). The air filter (3) is arranged on the throttle body (1) and connected to the inlet port (11). There is an air door (4) that can rotate in the cavity (10) to connect or block the inlet port (11) and the outlet port (12). Additionally, there is an air door driving part connected to the air door (4) and controls the rotation of the air door (4).

60. 发明公开

EP4180327A1 AN UNMANNED AERIAL VEHICLE 审中-公开
公开(公告)号：EP4180327A1
公开(公告)日：2023-05-17
申请号：EP22207366.0
申请日：2022-11-15
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64D1/22 , B66C1/38 , B64U101/64
摘要： The invention relates to the technical field of unmanned aerial vehicle manufacturing, and discloses an unmanned aerial vehicle (UAV). The UAV comprises an unmanned aerial vehicle body and a releasing mechanism, the releasing mechanism comprises a mounting piece and a reset component; the mounting piece is provided with a mounting groove; the opening direction of the mounting groove extends upwards; and a to-be-transported piece can be hooked in the mounting groove. The reset component is configured to deform under the gravity effect of the to-be-transported piece when the to-be-transported piece is lifted, and when the to-be-transported piece (100) lands to the ground, the reset component is reset to drive the to-be-transported piece to be separated from the mounting groove. During transportation, the to-be-transported piece is hooked to the bottom of the mounting groove under the gravity effect of the to-be-transported piece and deform the reset component. When the to-be-transported piece lands to the ground, the force of the to-be-transported piece on the reset component disappears, and the to-be-transported piece moves towards the opening direction of the mounting groove under the reset function of the reset component and is automatically separated from the mounting groove. The UAV can realize automatic releasing of a to-be-transported piece, the structure is simple and easy to realize, and can reduce the manufacturing cost of the UAV and improve the endurance ability of the UAV.

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