Launching type unmanned aerial vehicle capturing and countering device
The design of the umbrella-shaped conical limiting track and slider structure solves the problem of the capture net being difficult to deploy, ensuring that the capture net deploys after launch, expanding the capture range and improving the convenience and accuracy of operation.
Patent Information
- Application Number
- CN202423181447.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-23
- Publication Date
- 2025-11-07
- Estimated Expiration
- 2034-12-23
AI Technical Summary
Existing drone capture and countermeasure devices often have difficulty deploying the capture net when launching it, which affects the capture range.
A launch-type drone capture and countermeasure device was designed, which adopts an umbrella-rib conical limiting track and a slider structure. The capture net is deployed along the limiting track by the ejection action of the spring. Combined with the operation of the gate-shaped handle and grip rod, the capture net is ensured to be in the deployed state after launch.
The capture net was successfully deployed, the capture range was expanded, and the accuracy of the launch and ease of operation were improved.
Smart Images
Figure CN223525678U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to an unmanned plane countermeasure field more specifically relates to a launch type unmanned plane capture countermeasure device. BACKGROUND
[0002] Unmanned plane countermeasure technology refers to through adopting various technical means, the illegal intrusion unmanned plane is detected, identified, interfered, destroyed and the like operation, thereby eliminating unmanned plane threat, guarantee personnel and property safety.
[0003] At present, when capturing the unmanned plane, generally, the capture net is launched to the unmanned plane, makes the capture net and the unmanned plane contact, prevents the unmanned plane through preventing the rotating wing, but, the prior art, when launching the capture net, the capture net is not easy to unfold, influence the capture range. CONTENT OF THE UTILITY MODEL
[0004] The utility model provides a launch type unmanned plane capture countermeasure device can make the capture net unfold.
[0005] The utility model discloses a launch type unmanned plane capture countermeasure device, including the launch pipe for placing the capture net, the outer surface of launch pipe is evenly equipped with a plurality of limit tracks, and a plurality of limit tracks are in the umbrella rib formula conical radiation state, and the sliding block for the fixed connection of the limit track edge of the capture net slides, and every limit track is internally fixed with spring I far from the launch end of launch pipe, and spring I is used for the ejection of sliding block to limit track, and when a plurality of sliding blocks eject limit track simultaneously, will take the capture net out of launch pipe and gradually unfold.
[0006] A launch type unmanned plane capture countermeasure device, including the launch pipe for placing the capture net, the outer surface of launch pipe is evenly equipped with a plurality of limit tracks, and a plurality of limit tracks are in the umbrella rib formula conical radiation state, and the sliding block for the fixed connection of the limit track edge of the capture net slides, and every limit track is internally fixed with spring I far from the launch end of launch pipe, and spring I is used for the ejection of sliding block to limit track, and when a plurality of sliding blocks eject limit track simultaneously, will take the capture net out of launch pipe and gradually unfold.
[0007] The launch pipe is conical, facilitating the sliding of the capture net.
[0008] The sliding block is provided with a protrusion penetrating the limit track at the end away from the axis of the launch pipe, and the limit track is provided with a rectangular frame rotating at the launch end away from the launch pipe, which can be sleeved on the protrusion to limit the sliding block.
[0009] The launch pipe is provided with a door-shaped handle away from the launch end.
[0010] Two slide rods penetrate the door-shaped handle, and the two slide rods are provided with a push ring near the launch end of the launch pipe. Each rectangular frame is provided with a push edge. The push ring can simultaneously push multiple push edges by pushing the push ring towards the launch end of the launch pipe, so that the rectangular frame rotates and then releases the limitation on the sliding block.
[0011] A control frame is rotatingly arranged on the launch pipe corresponding to the middle part of the door-shaped handle, and the control frame is provided with a hook part near the launch end of the launch pipe. A spring II is arranged between the push ring and the door-shaped handle, and the push ring abuts against the hook part.
[0012] The hook part is provided with a protrusion near the end of the launching tube axis.
[0013] The launching tube is provided with a holding rod away from the center of the launching end.
[0014] The holding rod can slide axially away from the launching end of the launching tube.
[0015] Both ends of the holding rod are provided with a baffle.
[0016] The utility model has the advantages of:
[0017] The plurality of sliding blocks fly in the umbrella rib type conical radiation state along the plurality of limiting tracks, and then drive the capture net to slide out of the launching tube and gradually unfold, so that the capture net can be captured in the unfolded state after launching.
[0018] Through the cooperation of the door-shaped handle and the holding rod, the operator can hold the device conveniently, and the launching accuracy is increased. BRIEF DESCRIPTION OF DRAWINGS
[0019] Figure 1 And Figure 2 It is a structural schematic view of a launching type unmanned plane capture countermeasure device.
[0020] Figure 3 It is a structural schematic view of the launching tube and the limiting track.
[0021] Figure 4 It is a structural schematic view of the sliding block.
[0022] Figure 5 It is a structural schematic view of the rectangular frame.
[0023] Figure 6 It is a structural schematic view of the control frame.
[0024] Figure 7 It is a structural schematic view of the push ring.
[0025] Figure 8 It is a structural schematic view of the holding rod.
[0026] In the drawing:
[0027] Launching tube 1; limiting track 2; door-shaped handle 3; spring I 4; sliding block 5; protrusion 6; rectangular frame 7; push rib 8; control frame 9; hook part 10; sliding rod 11; push ring 12; spring II 13; holding rod 14. DETAILED DESCRIPTION
[0028] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments of the present application. Based on the embodiments of the present application, all the other embodiments obtained by those skilled in the art without creative work fall within the scope of protection of the present application.
[0029] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments of the present application. Based on the embodiments of the present application, all the other embodiments obtained by those skilled in the art without creative work fall within the scope of protection of the present application.
[0030] As shown in the description of the embodiments of the present application: Figures 1-8
[0031] A launch type unmanned plane capturing countermeasure device, comprising a launch tube 1 for placing a capturing net, a plurality of limiting tracks 2 are uniformly arranged on the outer surface of the launch tube 1 in a circumferential direction, the plurality of limiting tracks 2 are in a conical umbrella type radiation state, the limiting track 2 is used for sliding with the sliding block 5 fixedly connected with the edge of the capturing net, and a spring I 4 is fixedly arranged in the inside of each limiting track 2 away from the launch end of the launch tube 1, the spring I 4 is used for ejecting the sliding block 5 out of the limiting track 2, and when the plurality of sliding blocks 5 are ejected out of the limiting track 2 at the same time, the capturing net will be taken out of the launch tube 1 and gradually unfolded.
[0032] In use, the capturing net is inserted into the launch tube 1 from the launch end of the launch tube 1, and the plurality of sliding blocks 5 fixedly arranged around the capturing net are sequentially inserted into the plurality of limiting tracks 2 from the launch end of the launch tube 1, and the spring I 4 is pressed, then the plurality of sliding blocks 5 are ejected out of the limiting track 2 by the spring I 4 at the same time, the plurality of sliding blocks 5 will fly along the plurality of limiting tracks 2 in a conical umbrella type radiation state, and then drive the capturing net to slide out of the launch tube 1 and gradually unfold, so that the capturing net can be captured in an unfolded state after being launched.
[0033] Further:
[0034] The launch tube 1 is conical, so that the capturing net can slide out.
[0035] As shown in the description of the embodiments of the present application: Figures 1-8
[0036] The door-shaped handle 3 is arranged on the launch tube 1 away from the launch end, so that the device can be easily taken;
[0037] The slider 5 is provided with a protrusion 6 penetrating the limiting track 2 at the end away from the axis of the launching tube 1, and the limiting track 2 is provided with a rectangular frame 7 rotating away from the launching end of the launching tube 1, which can be sleeved on the protrusion 6 to limit the slider 5 and keep the slider 5 in the compressed spring I 4 state in the limiting track 2.
[0038] Two slide rods 11 penetrate the door-shaped handle 3, and the two slide rods 11 are provided with a push ring 12 near the launching end of the launching tube 1, and each rectangular frame 7 is provided with a push rib 8, which pushes the push ring 12 towards the launching end of the launching tube 1, and the push ring 12 can simultaneously push multiple push ribs 8 to rotate the rectangular frame 7, thereby releasing the limitation of the slider 5.
[0039] A control frame 9 is provided on the launching tube 1 corresponding to the middle part of the door-shaped handle 3, the control frame 9 is provided with a hook part 10 near the launching end of the launching tube 1, the push ring 12 and the door-shaped handle 3 are provided with a spring II 13, and the push ring 12 is in contact with the hook part 10.
[0040] When controlling the launching, the control frame 9 is pressed away from the hook part 10, the control frame 9 slides upwards, thereby driving the hook part 10 to slide upwards, so that the push ring 12 loses the limitation, the compressed spring II 13 pushes the push ring 12 to move towards the launching end of the launching tube 1, thereby simultaneously pushing multiple push ribs 8 to make multiple rectangular frames 7 rotate, thereby simultaneously releasing the limitation of multiple sliders 5, so that multiple sliders 5 are ejected to form the launching of the capture net.
[0041] Further:
[0042] The hook part 10 is provided with a protrusion near the axis of the launching tube 1, which forms a limitation to avoid the automatic sliding of the hook part 10 and the push ring 12, thereby causing a misfire.
[0043] Further:
[0044] The launching tube 1 is provided with a holding rod 14 away from the center of the launching end, which is convenient for the user to hold the door-shaped handle 3 with one hand and hold the holding rod 14 with the other hand, and the launching end of the launching tube 1 is aimed at the unmanned aerial vehicle to launch the capture net.
[0045] Further:
[0046] The holding rod 14 can slide axially away from the launching end of the launching tube 1, and when not in use, the holding rod 14 can be slid into the launching tube 1 to reduce the volume, and the holding rod 14 is provided with a baffle at both ends to avoid disengagement from the launching tube 1.
[0047] Of course, the above description is not a limitation of the present use instruction, and the present utility model is not limited to the above examples. Changes, modifications, additions or replacements made by ordinary skilled persons in the technical field within the essential scope of the present utility model also belong to the protection scope of the present utility model.
Claims
1. A drone-capture countermeasure device of the transmitting type, characterized in that: The utility model provides a net shooting device, including the launching tube (1) for placing the capture net, the outer surface of launching tube (1) is uniformly equipped with a plurality of limit rail (2) periphery, a plurality of limit rail (2) are in the umbrella rib type conical radiation state, limit rail (2) are used for the sliding block (5) fixed connection of capture net edge sliding, and each limit rail (2) is away from the inside of the launching end of launching tube (1) and is fixed with spring I (4), spring I (4) is used to eject the sliding block (5) out of limit rail (2), a plurality of sliding blocks (5) eject out of limit rail (2) simultaneously, will bring the capture net out of launching tube (1) and gradually unfold.
2. The launch-type UAV capture countermeasure device of claim 1, wherein: The launching tube (1) is conical, facilitating the sliding of the capture net.
3. The launch-type UAV capture countermeasure device of claim 1, wherein: The sliding block (5) is provided with a protrusion (6) penetrating the limit rail (2) at the end away from the axis of the launching tube (1), the limit rail (2) is provided with a rectangular frame (7) rotating at the end away from the launching end of the launching tube (1), the rectangular frame (7) can be sleeved on the protrusion (6) to limit the sliding block (5).
4. The drone capture countermeasure device of claim 3, wherein: The launching tube (1) is provided with a door-shaped handle (3) away from the launching end.
5. The drone capture countermeasure device of claim 4, wherein: Two slide rods (11) penetrate the door-shaped handle (3), the two slide rods (11) are provided with a push ring (12) near the launching end of the launching tube (1), each rectangular frame (7) is provided with a push rib (8), the push ring (12) can push multiple push ribs (8) simultaneously by pushing the push ring (12) towards the launching end of the launching tube (1), so that the rectangular frame (7) rotates and then releases the limitation of the sliding block (5).
6. The drone capture countermeasure device of claim 5, wherein: The door-shaped handle (3) is provided with a control frame (9) rotating on the launching tube (1) at the middle part, the control frame (9) is provided with a hook portion (10) near the launching end of the launching tube (1), the push ring (12) and the door-shaped handle (3) are provided with a spring II (13) therebetween, and the push ring (12) abuts against the hook portion (10).
7. The drone capture countermeasure device of claim 6, wherein: The hook portion (10) is provided with a protrusion near the axis end of the launching tube (1).
8. The drone capture countermeasure device of claim 6, wherein: The launching tube (1) is provided with a holding rod (14) away from the center of the launching end.
9. The drone capture countermeasure device of claim 8, wherein: The holding rod (14) can slide axially away from the launching end of the launching tube (1).
10. The drone capture countermeasure device of claim 9, wherein: The holding rod (14) is provided with a baffle at both ends.