专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 外观设计

USD1032408S1 Drone 有权
公开(公告)号：USD1032408S1
公开(公告)日：2024-06-25
申请号：US35515552
申请日：2022-10-24
申请人： Autoflight (Kunshan) Co. Ltd.
设计人： Yu Tian
摘要： The patent or application file contains at least one drawing executed in color. Copies of this patent or patent application publication with color drawing(s) will be provided by the Office upon request and payment of the necessary fee.
1. Drone
FIG. 1.1 is a front elevation view of a drone;
FIG. 1.2 is a right elevation view thereof;
FIG. 1.3 is a rear elevation view thereof;
FIG. 1.4 is a top plan view thereof;
FIG. 1.5 is a bottom plan view thereof;
FIG. 1.6 is a perspective view thereof;
FIG. 1.7 is a left side view thereof;
FIG. 1.8 is another perspective view thereof;
FIG. 1.9 is another perspective view thereof; and
FIG. 1.10 is another perspective view thereof.
A new ornamental design for a drone as shown and described; the parts shown by means of green coloring in the reproductions are not part of the claimed design.

2. 外观设计

USD1032407S1 Drone 有权
公开(公告)号：USD1032407S1
公开(公告)日：2024-06-25
申请号：US35515516
申请日：2022-10-13
申请人： Autoflight (Kunshan) Co. Ltd.
设计人： Yu Tian
摘要： The patent or application file contains at least one drawing executed in color. Copies of this patent or patent application publication with color drawing(s) will be provided by the Office upon request and payment of the necessary fee.
1. Drone
FIG. 1.1 is a right side elevation view of a drone;
FIG. 1.2 is a rear elevation view thereof;
FIG. 1.3 is a top perspective view thereof;
FIG. 1.4 is a front elevation view thereof;
FIG. 1.5 is a top plan view thereof;
FIG. 1.6 is a bottom plan view thereof;
FIG. 1.7 is a perspective view thereof;
FIG. 1.8 is another perspective view thereof;
FIG. 1.9 is another perspective view thereof; and
FIG. 1.10 is a left side elevation view thereof.
The parts shown by means of green coloring in the reproductions are not part of the claim design.

3. 发明公开

US20230283143A1 Motor Shock-Absorbing Structure and an Unmanned Aerial Vehicle Using the Same 审中-公开
公开(公告)号：US20230283143A1
公开(公告)日：2023-09-07
申请号：US18180096
申请日：2023-03-07
申请人： Autoflight (Kunshan) Co., Ltd.
发明人： Yu Tian
IPC分类号： H02K5/24 , B64U20/30 , B64D27/26
CPC分类号： H02K5/24 , B64U20/30 , B64D27/26
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 connected to the 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).

4. 发明公开

US20230278722A1 Data Monitoring Method and Medium 审中-公开
公开(公告)号：US20230278722A1
公开(公告)日：2023-09-07
申请号：US18180110
申请日：2023-03-07
申请人： Autoflight (Kunshan) Co., Ltd.
发明人： Yu Tian
IPC分类号： B64D45/00
CPC分类号： B64D45/00 , B64D2045/0085
摘要： A data monitoring method and a data monitoring medium. The method has: acquiring current vibration data of a target flight device in real time; Determining an anomaly protection strategy of the target flight device based on the current vibration data; The target flight equipment is controlled to execute corresponding operations 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.

5. 发明公开

US20230216246A1 Connector for an Aircraft 审中-公开
公开(公告)号：US20230216246A1
公开(公告)日：2023-07-06
申请号：US18060961
申请日：2022-12-01
申请人： Autoflight (Kunshan) Co., Ltd.
发明人： Yu Tian
IPC分类号： H01R13/645
CPC分类号： H01R13/645 , H01R2103/00
摘要： An aircraft and its connector where the connector has a first pluggable unit and a second pluggable unit, the end of the first pluggable unit is provided with several terminal pins, the end of the second pluggable unit is provided with several terminal sockets, and the terminal pin and the terminal socket can be operatively connected in a corresponding manner. The end of the first pluggable unit and the end of the second pluggable unit are also provided with an error-proof protrusion part and an error-proof concave part respectively. The error-proof protrusion part and the error-proof concave part are operatively connected in a corresponding manner.

6. 发明授权

US12074481B2 Motor-driven power board and a motor driver using the same 有权
公开(公告)号：US12074481B2
公开(公告)日：2024-08-27
申请号：US18193489
申请日：2023-03-30
申请人： Autoflight (Kunshan) Co., Ltd.
发明人： Yu Tian
IPC分类号： H02K11/33 , H02K5/22 , H02K11/30
CPC分类号： H02K11/33 , H02K5/225 , H02K11/30 , H02K2211/03
摘要： A motor-driven power board having a PCB and a plurality of transistors uniformly arranged along the edge of the PCB and a plurality of capacitors uniformly arranged along the inner side of the transistor. There is a plurality of terminals uniformly arranged along the inner side of the transistor. The board further includes a positive pole of power bus, a negative pole of power bus and a signal wire which are all located in the middle of the PCB. The invention improves the heat dissipation and current-sharing capacity of the power board by uniformly setting the power components from the inside to the outside according to the heat value while at the same time reduces the heat value in the middle of the power board, so that the motor of the driver using the power board can be assembled near the middle of the power board.

7. 外观设计

USD1032409S1 Drone 有权
公开(公告)号：USD1032409S1
公开(公告)日：2024-06-25
申请号：US35515568
申请日：2022-10-24
申请人： Autoflight (Kunshan) Co. Ltd.
设计人： Yu Tian
摘要： The patent or application file contains at least one drawing executed in color. Copies of this patent or patent application publication with color drawing(s) will be provided by the Office upon request and payment of the necessary fee.
1. Drone
FIG. 1.1 is a right elevation view of a drone;
FIG. 1.2 is a front elevation view thereof;
FIG. 1.3 is a rear elevation view thereof;
FIG. 1.4 is a top plan view thereof;
FIG. 1.5 is a perspective view thereof;
FIG. 1.6 is a bottom plan view thereof;
FIG. 1.7 is a left side view thereof;
FIG. 1.8 is another perspective view thereof;
FIG. 1.9 is another perspective view thereof; and
FIG. 1.10 is another perspective view thereof.
A new ornamental design for a drone as shown and described; the parts shown by means of green coloring in the reproductions are not part of the claimed design.

8. 发明授权

US11952151B2 Vertical tail for a composite-wing UAV 有权
公开(公告)号：US11952151B2
公开(公告)日：2024-04-09
申请号：US18161084
申请日：2023-01-29
申请人： Autoflight (Kunshan) Co., Ltd.
发明人： Yu Tian
IPC分类号： B64U20/70 , B64C5/02 , B64U10/17 , B64U20/83
CPC分类号： B64U20/70 , B64C5/02 , B64U10/17 , B64U20/83
摘要： A vertical tail of a composite-wing unmanned aerial vehicle (UAV) having a body, a rudder face section, a rotor section, shock absorbing component and a quick installation assembly of circuit. The body includes a tail body frame and a shell. The rudder face section has a rudder machine and a rudder surface. The rudder surface is connected to one end of the tail for steering the directional deflection of the UAV. The shock absorbing component is connected to the lower end plate and the shock absorbing component absorbs the shock to the body. The quick installation assembly of circuit includes a plug, a positioning sleeve and a bias piece, the positioning sleeve is located on the outer circumference of the plug and slidingly connected to the plug, the bias piece is set between the plug and the positioning sleeve, the bias piece can absorb the impact on the plug.

9. 发明授权

US11855387B2 Plug-in assembly structure and an unmanned aerial vehicle with composite wing 有权
公开(公告)号：US11855387B2
公开(公告)日：2023-12-26
申请号：US18161087
申请日：2023-01-29
申请人： Autoflight (Kunshan) Co., Ltd.
发明人： Yu Tian
IPC分类号： H01R13/627 , B64U30/10 , B64U20/70 , B64U50/30 , H01R13/631 , B64C1/26 , B64C1/30 , H01R4/50 , H01R12/91 , H01R13/62
CPC分类号： H01R13/6276 , B64U20/70 , B64U30/10 , B64U50/30 , H01R13/631 , B64C1/26 , B64C1/30 , H01R4/5058 , H01R12/91 , H01R13/62
摘要： A plug-in assembly structure for a UAV includes a first component (1), a second component (2) and a limit assembly (3). The first component (1) includes a first plug (11) and a positioning sleeve (12), and the positioning sleeve (12) is provided with a first through hole (121). The second component (2) includes a second plug (21), the radial direction of the second plug (21) is provided with a limit hole (2111), the second plug (21) can be electrically connected to the first plug (11), and the limit hole (2111) is facing the first through hole (121). The limit assembly (3) is installed in the limit hole (2111). The limit assembly (3) includes a first elastic element (31) and a limit element (32).

10. 发明授权

US11820508B2 Combined vertical takeoff and landing UAV 有权
公开(公告)号：US11820508B2
公开(公告)日：2023-11-21
申请号：US18058262
申请日：2022-11-22
申请人： Autoflight (Kunshan) Co., Ltd.
发明人： Yu Tian
IPC分类号： B64C39/02 , B64U70/20 , B64U70/80 , B64U10/00 , B64U80/82
CPC分类号： B64C39/024 , B64U10/00 , B64U70/20 , B64U70/80 , B64U80/82
摘要： A combined vertical takeoff and landing UAV having a large vertical takeoff and landing UAV, a connecting device, and a small vertical takeoff and landing UAV. The connecting device having a clamping component and an adsorption component. The clamping component includes a clamping part, and a clamping groove is arranged on the clamping part. The clamping component having a snap-fitting part, and a snap-fitting groove is arranged on the snap-fitting part. The clamping groove and the snap-fitting groove are correspondingly set. A first holding space is arranged on the clamping part, and a second holding space is arranged on the snap-fitting part. The adsorption component comprises a first magnetic element located in the first holding space, and the adsorption component also comprises a second magnetic element, which is located in the second holding space.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式