公开(公告)号：US11679871B2

公开(公告)日：2023-06-20

申请号：US17819628

申请日：2022-08-14

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: B64C27/26 ,  B64C39/12 ,  B64C39/04 ,  B64D31/00 ,  B64C39/02 ,  B64U10/25 ,  B64U30/10 ,  B64U50/13

CPC classification number: B64C27/26 ,  B64C39/04 ,  B64C39/12 ,  B64C39/024 ,  B64D31/00 ,  B64U10/25 ,  B64U30/10 ,  B64U50/13

Abstract: A long-distance drone having a main body, a left hind wing, a right hind wing, a left forewing, and a right forewing. There is a left linear support connecting the left forewing to the left hind wing, and a right linear support connecting the right forewing to the right hind wing. A plurality of propellers are disposed on the left and the right linear supports.

公开(公告)号：US11673677B2

公开(公告)日：2023-06-13

申请号：US17065540

申请日：2020-10-08

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: B64D27/24 ,  H01M10/655 ,  H01M10/6563 ,  H01M10/625 ,  B64C39/02 ,  B60L50/64 ,  B60L58/27 ,  B60L53/14 ,  B64U50/19

CPC classification number: B64D27/24 ,  B60L50/64 ,  B60L53/14 ,  B60L58/27 ,  B64C39/024 ,  H01M10/625 ,  H01M10/655 ,  H01M10/6563 ,  B60L2200/10 ,  B64U50/19 ,  H01M2220/20

Abstract: An unmanned aerial vehicle battery transport 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.

公开(公告)号：US20230166837A1

公开(公告)日：2023-06-01

申请号：US17821480

申请日：2022-08-23

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: B64C29/00 ,  B64C5/08 ,  B64C39/02

CPC classification number: B64C29/0025 ,  B64C5/08 ,  B64C39/024 ,  B64U30/10

Abstract: 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.

公开(公告)号：US11623746B2

公开(公告)日：2023-04-11

申请号：US17751706

申请日：2022-05-24

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: B64C37/02 ,  B64C39/02 ,  B64D27/24 ,  B63B7/08

Abstract: A method of navigating an UAV over water with vertical takeoff and landing (VTOL) function. The UAV having a plurality of lift propellers; a cabin engaged with a plurality of lift propellers; a water propulsion system engaged with the cabin to push the cabin in a forward direction when the cabin is at least partially immersed in water; at least one water inlet engaged with the water propulsion system; the cabin is a cargo hold or a passenger cabin. The UAV provided by the disclosure can realize vertical takeoff and landing in the water area, and fly, drive and navigate freely in the whole area.

公开(公告)号：US11623745B2

公开(公告)日：2023-04-11

申请号：US17819629

申请日：2022-08-14

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: B64C29/00 ,  B64C39/02

Abstract: The disclosure provides a method of controlling the yaw of a fixed-wing UAV, with two propulsion propellers arranged parallel to each other and providing thrust for the UAV; A plurality of motors configured to drive the two propulsion propellers, wherein the thrust ratio provided by the two propulsion propellers is changed to generate asymmetric thrust which controls the active yaw of the UAV. The fixed-wing UAV provided by the disclosure improves the reliability of the thrust system and active yaw.

公开(公告)号：US20230091309A1

公开(公告)日：2023-03-23

申请号：US17819949

申请日：2022-08-16

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: H02J7/00

Abstract: A method of balanced charging that includes the use of a plurality of charging modules, each of which independently charges a battery unit and is provided with a positive port and a negative port with independent functions; the positive port is connected with the positive port of the battery unit corresponding to the charging module, and the negative port is connected with the negative port of the battery unit corresponding to the charging module.

公开(公告)号：US11535372B2

公开(公告)日：2022-12-27

申请号：US17751714

申请日：2022-05-24

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: B64C37/02 ,  B64C39/02 ,  B64D27/24 ,  B63B7/08

Abstract: A method of navigating a detached cabin of an UAV over water. The UAV having a plurality of lift propellers; a cabin engaged with a plurality of lift propellers; a water propulsion system engaged with the cabin to push the cabin in a forward direction when the cabin is at least partially immersed in water; at least one water inlet engaged with the water propulsion system; the cabin is a cargo hold or a passenger cabin. The UAV provided by the disclosure can realize vertical takeoff and landing in the water area, and fly, drive and navigate freely in the whole area.

公开(公告)号：US11518536B2

公开(公告)日：2022-12-06

申请号：US17396700

申请日：2021-08-08

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: B64D33/08 ,  B64C29/00 ,  B64D27/24 ,  B64C11/00 ,  B64C39/02

Abstract: 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.

公开(公告)号：US20220380047A1

公开(公告)日：2022-12-01

申请号：US17827490

申请日：2022-05-27

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: B64C39/02 ,  B64C29/00 ,  B64C25/06

Abstract: 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.

公开(公告)号：US20220380046A1

公开(公告)日：2022-12-01

申请号：US17827383

申请日：2022-05-27

Applicant: Shanghai Autoflight Co., Ltd.

Inventor： Yu Tian

IPC: B64C39/02 ,  B64C35/00

Abstract: An amphibious cargo carrying unmanned aerial vehicle (UAV) having a fuselage, two wings and two frames, in which a cargo hold is arranged at the lower end of the fuselage, the cargo hold is provided with a cargo chamber for cargo carrying, and the cargo hold can touch the water surface at the same time. When taking off or landing on the water surface, the hollow structure of the cargo chamber can provide additional buoyancy. The two wings are symmetrically arranged on both sides of the fuselage, the two frames are correspondingly arranged on the two wings, and the buoyancy parts can be detachably arranged on the two frames to provide buoyancy.