Anti-collision unmanned aerial vehicle
By installing protective frames and buffer components on the outside of the drone propeller, the problem of vulnerability of the drone is solved, and the anti-collision protection and landing buffer of the propeller are achieved, reducing the cost of use and the risk of damage to internal components.
Patent Information
- Application Number
- CN202422637525.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-30
- Publication Date
- 2025-08-22
- Estimated Expiration
- 2034-10-30
AI Technical Summary
The existing drones lack anti-collision protection structures, which leads to vulnerability to rotor power components and precision components, increasing the cost of use.
The protective frame is installed on the outside of the propeller of the drone, and is equipped with buffer blocks, dampers, springs and oil storage seats. The buffer protection is achieved through the cooperation of damping oil and springs.
Effectively prevent the propeller from directly contacting the colliding object from damage, reduce the cost of use, and reduce the damage to the internal components of the drone by vibration shock when landing.
Smart Images

Figure CN223253318U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), in particular to an anti-collision UAV. Background Art
[0002] A drone, short for unmanned aerial vehicle (UAV), also known as a drone, is an unmanned aircraft controlled by a radio remote control device or a self-contained programmable controller. With the continuous development of technology, drones have gained widespread use in a variety of fields, including aerial photography, agriculture, plant protection, micro selfies, express delivery, disaster relief, wildlife observation, infectious disease monitoring, surveying and mapping, news reporting, power inspections, disaster relief, film and television production, and creating romantic moments.
[0003] A search of patent application number CN202020787347.6 discloses a drone comprising a fuselage, an arm assembly, and a rotor power assembly. The fuselage comprises a housing with an internal accommodating cavity, the arm assembly is rotatably connected to an arm hinge formed on the wall of the housing, and the rotor power assembly is disposed on the arm assembly. The drone described in this utility model has a lightweight structure, which can improve the drone's carrying capacity, avoid increasing the drone's waste weight, improve the carrying capacity, and extend the flight time. The foldable structure effectively reduces the occupied volume, has high space utilization, is convenient for storage, and is conducive to transportation.
[0004] However, this patent still has some shortcomings. The drone lacks an anti-collision protection structure, and during flight, the drone often collides with other objects due to external factors and operational problems. At this time, the rotor power assembly directly collides with other objects, causing damage to the propeller, which needs to be replaced and repaired, greatly increasing the cost of using the drone. At the same time, this patent does not have a landing buffer component. Since the drone is equipped with a chip motherboard, it is often equipped with precision components such as cameras according to usage needs. The impact force during landing is too large, which can easily cause damage to the precision components.
[0005] To this end, we propose a collision-avoidance UAV. Utility Model Content
[0006] The purpose of the present invention is to provide an anti-collision drone to solve the problems raised in the above background technology.
[0007] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: an anti-collision drone, comprising a drone body, a plurality of connecting arms fixedly mounted on the outer side of the drone body, a plurality of connecting arms being rotatably connected to a propeller on a side away from the drone body, a plurality of propellers being sleeved on the outer sides thereof, a mounting groove being provided on each connecting arm between the drone body and the propeller, a damper being fixedly mounted on a side close to the drone body in the plurality of mounting grooves, a buffer block being fixedly mounted on the output end of the plurality of dampers, a connecting plate being fixedly mounted on the front and rear parts of each buffer block, two connecting plates being fixedly mounted on the corresponding protective frame on a side away from the buffer block, a first spring being sleeved on the outer side of each damper, and an oil storage seat being fixedly mounted on the bottom end of the drone body.
[0008] Optionally, an extrusion plate is slidably connected to the oil storage seat, and a plurality of overflow holes are provided on the extrusion plate, so that the extrusion plate can extrude the damping oil through the plurality of overflow holes.
[0009] Optionally, a plurality of second springs are fixedly mounted on the outside of the overflow hole on the extrusion plate, and the tops of the plurality of second springs are fixedly mounted on the top inner side of the oil storage seat, so that the extrusion plate can be driven to reset by the second springs.
[0010] Optionally, a plurality of support rods are fixedly mounted on the bottom end of the extrusion plate, and two rubber support columns are provided at the bottom of the oil storage seat. The bottom ends of the plurality of support rods are respectively fixedly mounted on corresponding rubber support columns, so that the rubber support columns can provide preliminary cushioning when the UAV body lands.
[0011] Optionally, one side of each first spring is fixedly mounted on the buffer block, and the side of each first spring away from the buffer block is fixedly mounted on the inner wall of the mounting groove. This design is convenient for use of the device.
[0012] Optionally, arc-shaped buffer pads are fixedly installed on the outer sides of the plurality of protective frames, and the arc-shaped buffer pads can provide buffering protection.
[0013] Optionally, the plurality of protective frames are all arranged in a C-shape, and this design is beneficial to the use of the device.
[0014] Compared with the prior art, the beneficial effects of the present invention are:
[0015] Through the mutual cooperation of the buffer block, the first spring, the damper, the connecting plate, the arc-shaped buffer pad, the protective frame, the oil storage seat, the extrusion plate, the second spring, the overflow hole, the rubber support column and the support rod, multiple propellers can be protected from collision during flight, avoiding damage caused by direct contact between the propeller and the colliding object in the event of a collision, thereby greatly reducing the cost of using this type of drone. At the same time, it can provide buffering and shock absorption when the drone lands, avoiding damage to precision components such as the camera inside the drone body due to vibration and impact. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] Figure 1 This is a schematic diagram of the overall structure of an anti-collision drone of the utility model;
[0017] Figure 2 This is a cross-sectional view of an anti-collision UAV according to the present invention;
[0018] Figure 3 This is a cross-sectional view of an oil storage seat in an anti-collision drone of the utility model.
[0019] In the figure: 1. UAV body; 2. Connecting arm; 3. Propeller; 4. Mounting slot; 5. Buffer block; 6. First spring; 7. Damper; 8. Connecting plate; 9. Arc-shaped buffer pad; 10. Protective frame; 11. Oil storage seat; 12. Extrusion plate; 13. Second spring; 14. Overflow hole; 15. Rubber support column; 16. Support rod. DETAILED DESCRIPTION
[0020] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.
[0021] See also Figures 1 to 3The utility model provides an anti-collision drone, including a drone body 1, a plurality of connecting arms 2 are fixedly installed on the outer side of the drone body 1, a propeller 3 is rotatably connected to the side of the plurality of connecting arms 2 away from the drone body 1, and a protective frame 10 is sleeved on the outer sides of the plurality of propellers 3, a mounting groove 4 is provided on each connecting arm 2 between the drone body 1 and the propeller 3, a damper 7 is fixedly installed on the side close to the drone body 1 in the plurality of mounting grooves 4, a buffer block 5 is fixedly installed on the output end of the plurality of dampers 7, a connecting plate 8 is fixedly installed on the front and rear parts of each buffer block 5, and the two connecting plates 8 are fixedly installed on the corresponding protective frame 10 on the side away from the buffer block 5, a first spring 6 is sleeved on the outer side of each damper 7, and an oil storage seat 11 is fixedly installed at the bottom end of the drone body 1.
[0022] An extrusion plate 12 is slidably connected to the oil storage seat 11. A plurality of overflow holes 14 are provided on the extrusion plate 12. The plurality of overflow holes 14 facilitate the extrusion plate 12 to extrude the damping oil. A plurality of second springs 13 are fixedly installed on the extrusion plate 12 on the outside of the overflow holes 14. The tops of the plurality of second springs 13 are fixedly installed on the top of the oil storage seat 11. The second springs 13 can drive the extrusion plate 12 to reset. A plurality of support rods 16 are fixedly installed on the bottom end of the extrusion plate 12. Two rubber support columns 15 are provided at the bottom of the oil storage seat 11. The bottom ends of the plurality of support rods 16 are respectively It is fixedly mounted on the corresponding rubber support column 15, and the rubber support column 15 can provide preliminary buffering when the drone body 1 lands. One side of each first spring 6 is fixedly mounted on the buffer block 5, and the side of each first spring 6 away from the buffer block 5 is fixedly mounted on the inner wall of the mounting groove 4. This design is beneficial to the use of this equipment. The outer sides of multiple protective frames 10 are fixedly mounted with arc-shaped buffer pads 9, which can provide buffering protection. Multiple protective frames 10 are all arranged in a C-shape, which is beneficial to the use of this equipment.
[0023] Working principle: When in use, an appropriate amount of damping oil can be added to the oil storage seat 11. When the drone body 1 collides with other objects during flight, the arc-shaped buffer pad 9 and the protective frame 10 slide toward the side of the drone body 1, so that the buffer block 5 compresses the first spring 6, and then the first spring 6 cooperates with the damper 7 to buffer and eliminate vibration, and then the buffer block 5 drives the protective frame 10 to reset, which can provide buffering protection for the propeller 3 and avoid damage caused by direct contact between the propeller 3 and the colliding object. During the landing process, the two rubber support columns 15 will land first, and the rubber support columns 15 will undergo a certain deformation and rebound to perform preliminary shock absorption. The squeezed rubber support columns 15 will drive multiple support rods 16 to push the squeezed rubber support columns 15 upward. The pressure plate 12 and the extrusion plate 12 compress the second spring 13 and squeeze the damping oil, so that the damping oil enters the oil storage seat 11 through the overflow hole 14 and is located below the extrusion plate 12 to consume the vibration potential energy. Then the second spring 13 drives the extrusion plate 12 to return, so that the drone body 1 lands smoothly on the ground. This anti-collision drone is easy to use. Through the above components, it can play an anti-collision protection role for multiple propellers 3 during flight, avoiding direct contact between the propeller 3 and the collision object in the event of a collision and causing damage, thereby greatly reducing the use cost of this drone. At the same time, it can perform buffering and shock absorption when this drone lands, avoiding damage to precision components such as the camera inside the drone body 1 due to vibration impact.
[0024] Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A collision avoidance drone, characterized in that: The invention comprises a drone body (1), wherein a plurality of connecting arms (2) are fixedly mounted on the outer side of the drone body (1), a propeller (3) is rotatably connected to the side of the plurality of connecting arms (2) away from the drone body (1), a protective frame (10) is sleeved on the outer side of the plurality of propellers (3), a mounting groove (4) is provided on each connecting arm (2) between the drone body (1) and the propeller (3), a damper (7) is fixedly mounted on the side close to the drone body (1) in the plurality of mounting grooves (4), a buffer block (5) is fixedly mounted on the output end of the plurality of dampers (7), a connecting plate (8) is fixedly mounted on the front and rear parts of each buffer block (5), and the sides of the two connecting plates (8) away from the buffer block (5) are fixedly mounted on the corresponding protective frame (10), a first spring (6) is sleeved on the outer side of each damper (7), and an oil storage seat (11) is fixedly mounted on the bottom end of the drone body (1).
2. The anti-collision drone according to claim 1, characterized in that: An extrusion plate (12) is slidably connected in the oil storage seat (11), and a plurality of overflow holes (14) are provided on the extrusion plate (12).
3. The anti-collision drone according to claim 2, characterized in that: A plurality of second springs (13) are fixedly mounted on the extrusion plate (12) outside the overflow hole (14), and the tops of the plurality of second springs (13) are fixedly mounted on the top end of the oil storage seat (11).
4. The anti-collision drone according to claim 2, characterized in that: A plurality of support rods (16) are fixedly mounted on the bottom end of the extrusion plate (12), two rubber support columns (15) are provided at the bottom of the oil storage seat (11), and the bottom ends of the plurality of support rods (16) are respectively fixedly mounted on corresponding rubber support columns (15).
5. The anti-collision drone according to claim 1, characterized in that: One side of each first spring (6) is fixedly mounted on the buffer block (5), and the side of each first spring (6) away from the buffer block (5) is fixedly mounted on the inner wall of the mounting groove (4).
6. The anti-collision drone according to claim 1, characterized in that: Arc-shaped buffer pads (9) are fixedly mounted on the outer sides of the plurality of protective frames (10).
7. The anti-collision drone according to claim 1, characterized in that: The plurality of protective frames (10) are all arranged in a C-shape.
Citation Information
Patent Citations
Unmanned aerial vehicle
CN212448037U