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公开(公告)号：US11780602B2
公开(公告)日：2023-10-10
申请号：US17067686
申请日：2020-10-10
发明人： Yu Tian
CPC分类号： B64D43/02 , B64D15/12 , G01P5/165 , B64C39/024 , B64U2201/00
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.
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2.发明授权公开(公告)号：US11772786B2
公开(公告)日：2023-10-03
申请号：US17821480
申请日：2022-08-23
发明人： Yu Tian
CPC分类号： B64C29/0025 , B64C5/08 , B64C39/024 , B64U30/10 , B64U30/20 , B64U50/13
摘要： A method of flight control including having a vertical takeoff and landing aerial vehicle that has a plurality of lift propellers disposed on two linear support pieces, and there are two vertical stabilizers disposed at the rear of the two linear support pieces. A rotating shaft of each lift propeller from among the multiple lift propellers outwards forms an angle of 5 degrees to 15 degrees relative to a vertical plane of the aerial vehicle perpendicular to a horizontal plane of the aerial vehicle. The aerial vehicle of the present disclosure improves the heading axis control capacity of the aerial vehicle and reduces the restriction to the design size of the aerial vehicle.
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3.发明公开公开(公告)号：US20230294844A1
公开(公告)日：2023-09-21
申请号：US18309884
申请日：2023-05-01
发明人： Yu Tian
CPC分类号： B64F5/60 , G01R1/04 , G01R31/008 , B64C39/024
摘要： A method to test a power system and an avionics equipment of an unmanned aerial vehicle (UVA) including providing a support component, a power system load-bearing component, an avionics equipment load-bearing component, a jacking component and a roller component. The method further includes providing a plurality of power system load-bearing components that are fixedly arranged on the support components, respectively, and each power system load-bearing component is configured to carry the power system of a UAV; the avionics equipment load-bearing component is fixedly arranged on the support component, and the avionics equipment load-bearing component is configured to bear the avionics equipment of the UAV; the output end of the jacking component is fixedly connected to the bottom end of the support component.
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公开(公告)号：US20230288292A1
公开(公告)日：2023-09-14
申请号：US18309832
申请日：2023-05-01
发明人： Yu Tian
IPC分类号： G01M17/007 , B64F5/60
CPC分类号： G01M17/007 , B64F5/60
摘要： A method to test an unmanned aerial vehicle (UAV) using a support component, a universal rotating component, a fixed component and a return component. The method further includes wherein the universal rotating component slides along the Z direction and is arranged on the support component, and one end of the universal rotating component can rotate in a universal way relative to the other end of the universal rotating component. The fixed component is connected to one end of the universal rotating component, and the fixed component is configured to fix the UAV. One end of the return component is connected to the support component, the other end is connected to the other end of the universal rotating component, and the return component is configured to drive the universal rotating component and the fixed component to reset.
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公开(公告)号：US11745865B2
公开(公告)日：2023-09-05
申请号：US17396697
申请日：2021-08-07
发明人： Yu Tian
IPC分类号： B64C29/00 , B64C39/02 , B64D13/00 , B64D33/08 , B64D13/06 , B64U10/13 , B64U30/10 , B64U30/20 , B64U50/13 , B64U50/19 , B64U70/80
CPC分类号： B64C29/0025 , B64C39/024 , B64D13/006 , B64D33/08 , B64C2211/00 , B64D2013/0614 , B64U10/13 , B64U30/10 , B64U30/20 , B64U50/13 , B64U50/19 , B64U70/80
摘要： 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 at the front end of each of a left linear support and a right linear support 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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公开(公告)号：US20230264825A1
公开(公告)日：2023-08-24
申请号：US18309835
申请日：2023-05-01
发明人： Yu Tian
IPC分类号： B64D27/24 , H01M10/655 , H01M10/6563 , H01M10/625 , B64C39/02 , B60L50/64 , B60L58/27 , B60L53/14
CPC分类号： B64D27/24 , H01M10/655 , H01M10/6563 , H01M10/625 , B64C39/024 , B60L50/64 , B60L58/27 , B60L53/14 , B60L2200/10 , H01M2220/20 , B64U50/19
摘要： A method to transport a battery for an unmanned aerial vehicle using a battery transport box, the box having a box body shell and an upper cover. The unmanned aerial vehicle battery transport box further having a heat dissipating device and a heating device. When the temperature in the box body is lower than the lower limit of the set temperature range, the heating device heats the box body. When the temperature in the box body is higher than the upper limit of the set temperature range, the heat dissipating device dissipates heat of the box body. The temperature in the box body is adjusted by the heating device and the heat dissipating device.
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公开(公告)号：US11679899B2
公开(公告)日：2023-06-20
申请号：US17882567
申请日：2022-08-06
发明人： Yu Tian
CPC分类号： B64F5/60 , G01R1/04 , G01R31/008 , B64C39/024
摘要： 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, a power system load-bearing component, an avionics equipment load-bearing component, a jacking component and a roller component. A plurality of power system load-bearing components are provided, and are fixedly arranged on the support components, respectively, and each power system load-bearing component is configured to carry the power system of a UAV; the avionics equipment load-bearing component is fixedly arranged on the support component, and the avionics equipment load-bearing component is configured to bear the avionics equipment of the UAV; the output end of the jacking component is fixedly connected to the bottom end of the support component.
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公开(公告)号：US11608172B2
公开(公告)日：2023-03-21
申请号：US17827490
申请日：2022-05-27
发明人： Yu Tian
摘要： A vertical takeoff and landing (VTOL) UAV having a UAV main body, two rear landing gears and two front landing gears; the two rear landing gears are fixedly connected to both sides of the rear bottom of the UAV main body, respectively; the two front landing gears are rotatably connected to both sides of the front bottom of the UAV main body, respectively. One end of the front landing gear away from the UAV main body is provided with a locating block. Rotating the front landing gear enables the locating block mounted on the front landing gear to get close to or away from the UAV main body.
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公开(公告)号：US20230043316A1
公开(公告)日：2023-02-09
申请号：US17882567
申请日：2022-08-06
发明人： Yu Tian
摘要： 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, a power system load-bearing component, an avionics equipment load-bearing component, a jacking component and a roller component. A plurality of power system load-bearing components are provided, and are fixedly arranged on the support components, respectively, and each power system load-bearing component is configured to carry the power system of a UAV; the avionics equipment load-bearing component is fixedly arranged on the support component, and the avionics equipment load-bearing component is configured to bear the avionics equipment of the UAV; the output end of the jacking component is fixedly connected to the bottom end of the support component.
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公开(公告)号：US11535368B2
公开(公告)日：2022-12-27
申请号：US17396709
申请日：2021-08-08
发明人： Yu Tian
摘要： A vertical takeoff and landing aerial vehicle. A left linear support and a right linear support of the unmanned aerial vehicle are respectively provided with a first group of multiple lift propellers and a second group of lift propellers, and the aerial vehicle is provided with a left dorsal fin and a right dorsal fin. By arranging a plurality of lift propellers, a left dorsal fin, and a right dorsal fin on the vertical takeoff and landing aerial vehicle provided by the disclosure, the aerial vehicle is higher in stability in the flight process.
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