Unmanned aerial vehicle with anti-collision device

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with an anti-collision device, which comprises a rack, a flight controller fixedly mounted in the rack, a propeller arranged on the side surface of the rack, and a camera arranged at one end of the rack. Mounting grooves are formed in the two mounting blocks correspondingly, connecting rods are detachably arranged in the mounting grooves through buckle assemblies correspondingly, anti-collision nets used for protecting the propeller against collision are arranged at the two ends of each connecting rod correspondingly, and the connecting rods with the anti-collision nets arranged at the two ends are detachably connected through the limiting grooves, the limiting rods and the limiting holes; and the anti-collision net can be quickly disassembled, so that the propeller can be conveniently maintained or replaced, and meanwhile, the anti-collision net can be quickly replaced after collision occurs.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a unmanned aerial vehicle with an anti-collision device. Background Art

[0002] A drone is an aircraft that can be remotely controlled or fly autonomously. A drone is an autonomous system that can perform tasks without human intervention. There are different types and uses of drones, such as reconnaissance, surveillance, traffic control, firefighting, agriculture, and entertainment. When a drone is in use, it may sometimes collide with some objects, causing damage to the drone's propellers. Therefore, anti-collision nets are installed on the propellers of drones to protect the propellers. When an emergency occurs again, the propellers will not be hit, thereby avoiding damage to the power unit, causing the drone to lose balance, and preventing the drone from being unable to land safely.

[0003] However, in the prior art, the anti-collision nets of drones are all fixed on the outside of the propellers. When the propellers need to be repaired, the anti-collision nets need to be removed with the help of tools and then the propellers are repaired. At the same time, when a collision occurs, it is not convenient to quickly remove and replace the anti-collision nets, which affects work efficiency. Utility Model Content

[0004] The purpose of the utility model is to provide a UAV with an anti-collision device, which solves the problem that in the prior art, the anti-collision nets of UAVs are all fixed on the outside of the propellers. When the propellers need to be repaired, the anti-collision nets need to be removed with the help of tools and then the propellers are repaired. At the same time, when a collision occurs, it is not convenient to quickly disassemble and replace the anti-collision nets, which affects work efficiency.

[0005] In order to solve the above technical problems, the utility model adopts the following technical solutions:

[0006] A UAV with an anti-collision device comprises a frame, a flight controller is fixedly installed inside the frame, a propeller is arranged on the side of the frame, and a camera is arranged at one end of the frame. The invention is characterized in that mounting blocks are respectively arranged at two ends of the top of the frame, mounting grooves are respectively opened on the two mounting blocks, connecting rods are detachably arranged in the mounting grooves through buckle assemblies, and anti-collision nets for protecting the propeller from collision are respectively arranged at two ends of the connecting rod.

[0007] A further technical solution is that the snap assembly includes a limit rod, a limit slot is provided on the mounting block above the mounting slot, two sliding rods are vertically fixed in the limit slot, and the same lifting plate is slidably connected to the two sliding rods; the limit rod is vertically fixed on the bottom side of the lifting plate, and the bottom end of the limit rod is movably passed through the bottom of the limit slot through a movable hole and is placed in the mounting slot; a limit hole is provided on the connecting rod and is plugged and matched with the limit rod.

[0008] A further technical solution is that a support spring is sleeved on the outer wall of the sliding rod, the lower end of the support spring is fixedly connected to the top of the lifting plate, and the upper end of the support spring is fixedly connected to the top side of the limiting groove.

[0009] A further technical solution is that a pull rod is vertically provided at the top of the lifting plate, and the top of the pull rod movably passes through the limit groove through the through hole and is connected with a pull ring.

[0010] A further technical solution is that the limiting rods and the limiting holes are arranged in two groups.

[0011] A further technical solution is that the anti-collision net includes an upper half ring and a lower half ring, and a plurality of anti-collision strips are vertically arranged between the upper half ring and the lower half ring. When the anti-collision net is arranged at both ends of the connecting rod, the connecting rod is fixedly connected to the inner side of the upper half ring, and the propeller is located on the inner side of the anti-collision net.

[0012] A further technical solution is that the outer sides of the upper half ring and the lower half ring are fixedly connected with buffer arc strips through buffer springs.

[0013] Compared with the prior art, the beneficial effect of the utility model is that the connecting rods with anti-collision nets at both ends are detachably connected through limit grooves, limit rods and limit holes, so that the anti-collision net can be quickly disassembled, thereby facilitating the maintenance or replacement of the propeller. At the same time, when a collision occurs, the anti-collision net can be quickly replaced. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 The utility model is a three-dimensional schematic diagram of an unmanned aerial vehicle with an anti-collision device.

[0015] Figure 2 This is a cross-sectional view of the mounting block and the connecting rod of the utility model.

[0016] Figure 3 It is a schematic diagram of the structure of the anti-collision net of the utility model.

[0017] Icon: 1-frame, 2-propeller, 3-camera, 4-mounting block, 5-mounting slot, 6-connecting rod, 7-anti-collision net, 8-limit rod, 9-limit slot, 10-sliding rod, 11-lifting plate, 12-limiting hole, 13-support spring, 14-pull rod, 15-pull ring, 16-upper half ring, 17-lower half ring, 18-anti-collision strip, 19-buffer spring, 20-buffer arc strip, 21-movable hole. DETAILED DESCRIPTION

[0018] In order to make the purpose, technical solution and advantages of the utility model more clear, the utility model is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the utility model and are not used to limit the utility model.

[0019] Example:

[0020] refer to Figures 1 to 3 Shown is a drone with an anti-collision device, comprising a frame 1, a flight controller fixedly installed inside the frame 1, a propeller 2 arranged on the side of the frame 1, a camera 3 arranged at one end of the frame 1, mounting blocks 4 respectively arranged at both ends of the top of the frame 1, mounting grooves 5 respectively opened on the two mounting blocks 4, connecting rods 6 detachably arranged in the mounting grooves 5 through snap-fit ​​assemblies, anti-collision assemblies for protecting the propeller 2 from collision are respectively arranged at both ends of the connecting rod 6, in actual use, the connecting rod 6 is arranged by setting the snap-fit ​​assemblies, and anti-collision assemblies for protecting the propeller 2 from collision are arranged at both ends of the connecting rod 6, when the propeller 2 needs to be maintained or replaced, the connecting rod 6 can be easily disassembled through the snap-fit ​​assemblies, and then the anti-collision assemblies can be quickly disassembled, which is convenient for maintenance personnel to maintain or replace the propeller 2 and improve work efficiency.

[0021] refer to Figure 1 , Figure 2 The buckle assembly includes a limit rod 8, a limit groove 9 is provided on the mounting block 4 above the mounting groove 5, two sliding rods 10 are vertically fixed in the limit groove 9, and the two sliding rods 10 are slidably connected with the same lifting plate 11; the limit rod 8 is vertically fixed to the bottom side of the lifting plate 11, and the bottom end of the limit rod 8 is movably penetrated through the bottom of the limit groove 9 through the movable hole 21 and placed in the mounting groove 5; a limit hole 12 is provided on the connecting rod 6 to match the limit rod 8; a support spring 13 is sleeved on the outer wall of the sliding rod 10, the lower end of the support spring 13 is fixedly connected to the top of the lifting plate 11, and the upper end of the support spring 13 is fixedly connected to the top side of the limit groove 9; a pull rod 14 is vertically provided at the top of the lifting plate 11, and the top of the pull rod 14 is movably penetrated through the limit groove 9 through the through hole and is connected with a pull ring 15; the limit rod 8 and the limit hole 12 are both set in two groups, and when the anti-collision net 7 needs to be disassembled during actual use When the propeller 2 is maintained or replaced, the pull ring 15 is manually pulled, and the pull ring 15 drives the pull rod 14 to rise. During the process of the pull rod 14 driving the lifting plate 11 to rise, the lifting plate 11 squeezes the supporting spring 13, and the lifting plate 11 drives the limiting rod 8 to rise. At this time, the connecting rod 6 is placed between the limiting grooves 9. After being inserted to the specified position, the pull ring 15 is released, and the limiting rod 8 is driven down by the movable plate under the elastic restoring force of the supporting spring 13. The limiting rod 8 descends and is inserted into the limiting hole 12, so that the connecting rod 6 is installed, and the anti-collision net 7 is quickly installed on both sides of the propeller 2. Conversely, during installation, the pull ring 15 is manually pulled up to release the limit, which is convenient for the quick disassembly and maintenance of the anti-collision net 7 as a whole, and the operation is more convenient; by setting two sets of limiting rods 8 and limiting holes 12, the connecting rod 6 can be better limited to prevent the connecting rod 6 from rotating, thereby ensuring the stability of the anti-collision net 7.

[0022] refer to Figure 1 , Figure 3 As shown, the anti-collision net 7 includes an upper half ring 16 and a lower half ring 17, and a plurality of anti-collision strips 18 are vertically arranged between the upper half ring 16 and the lower half ring 17. When the anti-collision net 7 is arranged at both ends of the connecting rod 6, the connecting rod 6 is fixedly connected to the inner side of the upper half ring 16, and the propeller 2 is located on the inner side of the anti-collision net 7; the outer sides of the upper half ring 16 and the lower half ring 17 are fixedly connected with a buffer arc strip 20 through a buffer spring 19; by setting the anti-collision net 7, the rotor of the device is protected to prevent the device from being damaged by collision, and the outer sides of the upper half ring 16 and the lower half ring 17 are fixedly connected with the buffer arc strip 20 through the buffer spring 19, so that when the device collides with an external object, the external object first contacts the buffer arc strip 20, and the buffer spring 19 between the upper half ring 16 and the lower half ring 17 and the buffer arc strip 20 can weaken the collision force of the device to prevent excessive damage to the device.

[0023] Although the utility model is described herein with reference to a plurality of illustrative embodiments of the utility model, it should be understood that those skilled in the art may devise many other modifications and implementations that fall within the scope and spirit of the principles disclosed herein. More specifically, within the scope of the disclosure, drawings, and claims of the present application, various modifications and improvements may be made to the components and / or layout of the subject combination layout. In addition to the modifications and improvements made to the components and / or layout, other uses will also be apparent to those skilled in the art.

Claims

1. An unmanned aerial vehicle with an anti-collision device, comprising a frame (1), a flight controller fixedly mounted inside the frame (1), a propeller (2) disposed on the side of the frame (1), and a camera (3) disposed at one end of the frame (1), characterized in that: Mounting blocks (4) are respectively provided at both ends of the top of the frame (1), and mounting grooves (5) are respectively provided on the two mounting blocks (4), and connecting rods (6) are detachably provided in the mounting grooves (5) via snap-fit ​​assemblies, and anti-collision nets (7) for protecting the propeller (2) from collision are respectively provided at both ends of the connecting rods (6).

2. The UAV with an anti-collision device according to claim 1, characterized in that: The buckle assembly comprises a limit rod (8), a limit groove (9) is provided on the mounting block (4) above the mounting groove (5), two sliding rods (10) are vertically fixed in the limit groove (9), and the two sliding rods (10) are slidably connected to the same lifting plate (11); the limit rod (8) is vertically fixed on the bottom side of the lifting plate (11), and the bottom end of the limit rod (8) is movably penetrated through the bottom of the limit groove (9) through a movable hole (21) and is placed in the mounting groove (5); and a limit hole (12) is provided on the connecting rod (6) and is plugged and matched with the limit rod (8).

3. The UAV with anti-collision device according to claim 2, characterized in that: A support spring (13) is sleeved on the outer wall of the sliding rod (10), the lower end of the support spring (13) is fixedly connected to the top of the lifting plate (11), and the upper end of the support spring (13) is fixedly connected to the top side of the limiting groove (9).

4. The UAV with anti-collision device according to claim 2, characterized in that: A pull rod (14) is vertically provided at the top end of the lifting plate (11), and the top end of the pull rod (14) movably penetrates through the limiting groove (9) through a through hole and is connected to a pull ring (15).

5. The UAV with anti-collision device according to claim 2, characterized in that: The limiting rods (8) and the limiting holes (12) are both provided in two groups.

6. The UAV with anti-collision device according to claim 1, characterized in that: The anti-collision net (7) comprises an upper half ring (16) and a lower half ring (17), and a plurality of anti-collision strips (18) are vertically arranged between the upper half ring (16) and the lower half ring (17). When the anti-collision net (7) is arranged at both ends of the connecting rod (6), the connecting rod (6) is fixedly connected to the inner side of the upper half ring (16), and the propeller (2) is located on the inner side of the anti-collision net (7).

7. The UAV with anti-collision device according to claim 6, characterized in that: The outer sides of the upper half ring (16) and the lower half ring (17) are fixedly connected with buffer arc strips (20) via buffer springs (19).

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