An unmanned aerial vehicle anti-collision early warning device

Abstract

The utility model belongs to the technical field of unmanned plane, concretely relates to a kind of unmanned plane anti-collision early warning device, comprising: unmanned plane, the top of unmanned plane is provided with early warning trigger component, the outside of unmanned plane is provided with early warning protection ring, early warning protection ring is detachably installed with early warning trigger component;The top of early warning protection ring is fixedly connected with multiple connecting rods, and the surface of early warning protection ring is fixedly connected with multiple thickness grids.The utility model can be realized, through the design of movable connecting pipe, when more serious collision occurs, the position of collision object is determined immediately to make unmanned plane away, simultaneously rotate early warning protection ring to make it produce reverse thrust to reduce the speed due to inertia, to reduce the force received by unmanned plane when colliding;Through the design of early warning trigger component, it can be applied to various unmanned plane models, and only the diameter of early warning protection ring needs to be changed, which can offset the slight collision of unmanned plane.

Description

Technical Field

[0001] This utility model belongs to the field of unmanned aerial vehicle (UAV) technology, specifically relating to a UAV collision avoidance and early warning device. Background Technology

[0002] A drone collision avoidance warning device typically refers to a system that monitors the surrounding environment in real time, detects potential obstacles, and issues an alert. The main function of this device is to provide pre-collision warnings, that is, to issue an early warning before the drone collides with an obstacle, reminding the operator to take evasive action.

[0003] Problems with existing technology:

[0004] Existing drone collision avoidance warning devices are mostly optical cameras, which are popular because they are inexpensive and not easily damaged. However, optical cameras often fail to detect transparent glass or wires and cannot provide warnings, which may lead to further incorrect operations by the operator, putting the drone in a dangerous situation. In severe cases, collisions may occur, causing damage to the drone or even causing it to crash. In addition, drones lack necessary protective devices in the event of a collision. Utility Model Content

[0005] The purpose of this invention is to provide a drone collision avoidance warning device. Through the design of the movable connecting tube, it can immediately determine the position of the colliding object and move the drone away when a serious collision occurs. At the same time, it rotates the warning protection ring to generate a reverse thrust to reduce the speed caused by inertia, thereby reducing the force on the drone during the collision. Through the design of the warning trigger component, it can be applied to various drone models, and only the diameter of the warning protection ring needs to be changed. It can also offset the collision when the drone is involved in a minor collision.

[0006] The specific technical solution adopted by this utility model is as follows:

[0007] A drone collision avoidance warning device includes: a drone, a warning triggering component is provided on the top of the drone, and a warning protection ring is provided on the outer side of the drone, wherein the warning protection ring and the warning triggering component are detachably installed;

[0008] The top of the warning protection ring is fixedly connected to multiple connecting rods, the surface of the warning protection ring is fixedly connected to multiple thickness grids, the multiple thickness grids are arranged in a ring array along the warning protection ring, and a polygonal pin is fixedly connected to the middle position of the bottom of the multiple connecting rods.

[0009] The warning triggering component includes a rubber connecting pad, a rotating motor is fixedly connected to the top of the rubber connecting pad, a trigger is fixedly connected to the output end of the rotating motor, a movable cavity is provided inside the trigger, and a movable connecting tube is provided inside the movable cavity.

[0010] A movable ball is fixedly connected to the bottom of the movable connecting tube. The movable ball is slidably disposed with the inner wall of the movable cavity. The trigger is provided with multiple spring grooves corresponding to the position of the movable connecting tube. Limiting springs are provided inside the spring grooves. The two ends of the multiple limiting springs are respectively fixedly connected to the inner wall of the corresponding spring groove and the movable connecting tube.

[0011] Multiple electrical plates are fixedly installed at the end of the movable connecting tube corresponding to the movable cavity. The electrical plates are arranged in a circular array, and both the movable connecting tube and the electrical plates are connected to a low-voltage circuit.

[0012] The movable connecting tube has a polygonal insertion groove inside, and the polygonal pin is inserted into the polygonal insertion groove. A disassembly screw is provided on one side of the outside of the polygonal insertion groove, and the end of the disassembly screw extends into the inside of the movable connecting tube and is threadedly connected to the polygonal pin.

[0013] The technical effects achieved by this utility model are as follows:

[0014] This invention, through the design of the movable connecting tube, can immediately determine the position of the colliding object and move the drone away in the event of a severe collision. At the same time, it rotates the warning protection ring to generate a reverse thrust to reduce the speed caused by inertia, thereby reducing the force on the drone during the collision.

[0015] This invention, through the design of the early warning trigger component, can be applied to various drone models, and only requires changing the diameter of the early warning protection ring, which can offset the impact when the drone is involved in a minor collision. Attached Figure Description

[0016] Figure 1 This is a schematic diagram of the appearance structure of this utility model;

[0017] Figure 2 This is a schematic diagram of the early warning protection ring in this utility model;

[0018] Figure 3 This is a schematic diagram of the structure of the early warning triggering component in this utility model;

[0019] Figure 4 This is a cross-sectional view of the trigger structure in this utility model;

[0020] Figure 5 This is a schematic diagram of the trigger structure in this utility model.

[0021] The attached diagram lists the components represented by each number as follows:

[0022] 1. Unmanned Aerial Vehicle (UAV); 2. Early Warning Protection Ring; 3. Early Warning Trigger Component; 201. Connecting Rod; 202. Thickness Grid; 203. Polygonal Pin; 301. Rubber Connecting Pad; 302. Ring Battery; 303. Rotating Motor; 304. Trigger; 305. Movable Connecting Tube; 306. Limiting Spring; 307. Electric Plate; 308. Polygonal Insertion Slot; 309. Movable Ball; 310. Removal Screw. Detailed Implementation

[0023] To make the objectives and advantages of this utility model clearer, the following detailed description is provided in conjunction with embodiments. It should be understood that the following text is merely used to describe one or more specific embodiments of this utility model and does not strictly limit the scope of protection specifically claimed by this utility model.

[0024] like Figure 1 As shown, a drone collision avoidance warning device includes: a drone 1, a warning triggering component 3 is provided on the top of the drone 1, and a warning protection ring 2 is provided on the outer side of the drone 1. The warning protection ring 2 and the warning triggering component 3 are detachably installed.

[0025] The warning triggering component 3 is independently set and connected to the drone 1 by means of glue or other means. The warning triggering component 3 and the drone 1 are connected by a data cable to transmit some simple signals. The warning protection ring 2 can rotate under the control of the warning triggering component 3 to play a certain role in protecting the drone 1. At the same time, the warning protection ring 2 can promptly feed back to the warning triggering component 3 and send a collision signal when a collision occurs.

[0026] See attached document Figures 2-4 The warning triggering component 3 includes a rubber connecting pad 301, a rotating motor 303 fixedly connected to the top of the rubber connecting pad 301, a trigger 304 fixedly connected to the output end of the rotating motor 303, a movable cavity provided inside the trigger 304, and a movable connecting tube 305 provided inside the movable cavity; multiple connecting rods 201 fixedly connected to the top of the warning protection ring 2, multiple thickness grids 202 fixedly connected to the surface of the warning protection ring 2, the multiple thickness grids 202 arranged in a ring array along the warning protection ring 2, and a polygonal pin 203 fixedly connected to the middle position of the bottom of the multiple connecting rods 201; a polygonal insertion groove 308 is opened inside the movable connecting tube 305, the polygonal pin 203 is inserted into the polygonal insertion groove 308, a disassembly screw 310 is provided on one side of the polygonal insertion groove 308, the end of the disassembly screw 310 extends into the interior of the movable connecting tube 305 and is threadedly connected to the polygonal pin 203.

[0027] According to the above structure, the rubber connecting pad 301 is fixed to the top of the drone 1 with glue, and the rotating motor 303 is powered by the ring battery 302. When the drone 1 collides, the obstacle will first come into contact with the warning protection ring 2. Under the action of the reverse force, the warning protection ring 2 will be pushed by a force, which is transmitted to the movable connecting tube 305 through the polygonal pin 203. The thickness grid 202 is used to increase the protection range and adapt to the thickness of the drone 1. The setting of the limiting spring 306 can ensure the firmness of the polygonal pin 203 and facilitate the replacement of the warning protection ring 2.

[0028] See attached document Figures 4-5 A movable ball 309 is fixedly connected to the bottom of the movable connecting tube 305. The movable ball 309 is slidably disposed with the inner wall of the movable cavity. A trigger 304 is provided with multiple spring grooves corresponding to the position of the movable connecting tube 305. Limiting springs 306 are provided inside the spring grooves. The two ends of the multiple limiting springs 306 are fixedly connected to the inner wall of the corresponding spring groove and the movable connecting tube 305, respectively. Multiple electrical pieces 307 are fixedly installed at the end of the movable connecting tube 305 corresponding to the movable cavity. The electrical pieces 307 are arranged in a ring array. Both the movable connecting tube 305 and the electrical pieces 307 are connected to a low voltage circuit.

[0029] According to the above structure, when the pushing force is transmitted to the movable connecting tube 305, the movable connecting tube 305 will rotate around the movable ball 309 as the center. During its rotation, the elastic deformation of multiple limit springs 306 generates a force opposite to the pushing force on the movable connecting tube 305, thereby pushing the drone 1 away from the obstacle. Only the warning protection ring 2 contacts the obstacle, and the drone body will not contact it. When the collision force is too large, the rotation angle of the movable connecting tube 305 increases and it contacts the electric plate 307. At this time, an electrical signal is generated and transmitted to the drone 1. The built-in program of the drone 1 controls the drone 1 to move away from the obstacle. At the same time, the trigger 304 rotates under the drive of the rotating motor 303.

[0030] The warning protection ring 2 also rotates. The hardness of the corresponding thickness grid 202 of the warning protection ring 2 is relatively low. If a severe collision occurs, it will break into small segments. Under the influence of the rotation of the warning protection ring 2, the broken ends will tilt and pierce the obstacle, thus obtaining a tilted reverse thrust. Through force analysis, a force opposite to the inertial direction of the drone 1 and a force tangential to the rotation direction of the warning protection ring 2 can be obtained. The force opposite to the inertial direction cancels out the force generated by the inertia of the drone 1, quickly decelerates the drone 1, and reduces the collision damage to the drone 1. The force tangential to the rotation direction of the warning protection ring 2 changes the direction of movement of the drone. The force originally perpendicular to the obstacle changes a certain angle of movement, which can also reduce the impact of the collision on the drone 1.

[0031] The warning protection ring 2 is equipped with a traction rope inside to connect the broken parts and prevent them from flying everywhere; the electric plate 307 in the ring array can calculate and determine the direction of the obstacle on the drone 1 by the electrical signal sent through the contact with the movable connecting tube 305; the movable ball 309 is stuck inside the movable cavity and can only rotate but cannot move.

[0032] The working principle of this utility model is as follows: The rubber connecting pad 301 is fixed to the top of the drone 1. When the drone 1 collides, the obstacle will first contact the warning protection ring 2. Under the action of the reverse force, the warning protection ring 2 will be pushed. When the collision force is too large, the movable connecting tube 305 rotates at an increased angle and contacts the electric plate 307. At this time, an electrical signal is generated and transmitted to the drone 1. The drone 1 is controlled to move away from the obstacle by the built-in program. At the same time, the trigger 304 rotates under the drive of the rotating motor 303, and the warning protection ring 2 also rotates accordingly. The hardness of the warning protection ring 2 at the corresponding thickness grid 202 is relatively low. If... In the event of a severe collision, the drone will break into small segments. Under the influence of the rotation of the warning protection ring 2, the broken ends will tilt and pierce the obstacle, thus generating a tilted, reverse thrust. Through force analysis, a force opposite to the inertial direction of the drone 1 and a force tangential to the rotation direction of the warning protection ring 2 can be obtained. The force opposite to the inertial direction cancels out the force generated by the inertia of the drone 1, quickly decelerating the drone 1 and reducing the collision damage. The force tangential to the rotation direction of the warning protection ring 2 changes the drone's direction of motion. The force originally perpendicular to the obstacle changes by a certain angle, which can also reduce the impact of the collision on the drone 1.

[0033] The above description is merely a preferred embodiment of this utility model. It should be noted that those skilled in the art can make various improvements and modifications without departing from the principle of this utility model, and these improvements and modifications should also be considered within the scope of protection of this utility model. Structures, devices, and operating methods not specifically described or explained in this utility model, unless otherwise specified or limited, shall be implemented using conventional methods in the field.

Claims

1. A drone collision avoidance and early warning device, characterized in that, include: The drone (1) has a warning triggering component (3) on its top and a warning protection ring (2) on its outer side. The warning protection ring (2) and the warning triggering component (3) are detachable and installable. The top of the warning protection ring (2) is fixedly connected with multiple connecting rods (201), and the surface of the warning protection ring (2) is fixedly connected with multiple thickness grids (202). The multiple thickness grids (202) are arranged in a ring array along the warning protection ring (2), and a polygonal pin (203) is fixedly connected to the middle position of the bottom of the multiple connecting rods (201). The warning triggering component (3) includes a rubber connecting pad (301), a rotating motor (303) is fixedly connected to the top of the rubber connecting pad (301), a trigger (304) is fixedly connected to the output end of the rotating motor (303), a movable cavity is provided inside the trigger (304), and a movable connecting tube (305) is provided inside the movable cavity.

2. The drone collision avoidance and early warning device according to claim 1, characterized in that: The bottom of the movable connecting tube (305) is fixedly connected to a movable ball (309), which is slidably disposed with the inner wall of the movable cavity. The trigger (304) is provided with multiple spring grooves corresponding to the position of the movable connecting tube (305). Limiting springs (306) are provided inside the spring grooves. The two ends of the multiple limiting springs (306) are fixedly connected to the inner wall of the corresponding spring groove and the movable connecting tube (305) respectively.

3. The drone collision avoidance and early warning device according to claim 1, characterized in that: Multiple electrical pieces (307) are fixedly installed at the end of the movable connecting tube (305) corresponding to the movable cavity. The electrical pieces (307) are arranged in a ring array. Both the movable connecting tube (305) and the electrical pieces (307) are connected to a low-voltage circuit.

4. The drone collision avoidance and early warning device according to claim 1, characterized in that: The movable connecting tube (305) has a polygonal insertion groove (308) inside. The polygonal pin (203) is inserted into the polygonal insertion groove (308). A disassembly screw (310) is provided on one side of the polygonal insertion groove (308). The end of the disassembly screw (310) extends into the interior of the movable connecting tube (305) and is threadedly connected to the polygonal pin (203).

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