Airborne high-explosive gas type anti-unmanned aerial vehicle catching net launching device
By designing an airborne high-explosive gas anti-drone capture net launching device, and utilizing the thrust of high-explosive gas and a limiting and separating structure, the problems of low capture efficiency and poor stability of existing anti-drone devices are solved, achieving fast, stable, and long-distance drone capture effects.
Patent Information
- Application Number
- CN202423267037.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-30
- Publication Date
- 2025-12-19
- Estimated Expiration
- 2034-12-30
AI Technical Summary
Existing anti-drone devices are inefficient at capturing targets, making it difficult to capture them quickly and accurately. They are also unstable, easily affected by environmental factors, and have a short attack range, making them ineffective against long-range threats.
An airborne high-explosive gas anti-drone capture net launching device was designed. Through the separation structure of the high-explosive chamber and the launch chamber inside the launching cylinder, the high-explosive gas is used to generate thrust to launch the capture net. Combined with the limiting unit and the separation unit, the positional stability of the rubber ball and the stability of the device are ensured, and the leakage of the gas generator is prevented.
It enables rapid and stable capture of drones, reduces environmental interference, extends attack range, and ensures the stability and efficient launch of the capture net.
Smart Images
Figure CN223691614U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to transmitter technical field especially is related to a kind of airborne high-explosive gas type anti-unmanned aerial vehicle capture net launching device. BACKGROUND
[0002] The rapid development of unmanned aerial vehicle technology makes unmanned aerial vehicle widely used in various fields, but also brings serious threat to safety, but the traditional anti-unmanned aerial vehicle means has obvious defects, and it is difficult to meet the current safety needs, the current anti-unmanned aerial vehicle device capture efficiency is low, often difficult to quickly and accurately capture target unmanned aerial vehicle, and these devices are easily disturbed by environmental factors during use, such as crosswind, leading to capture failure or poor effect, the attack distance of the existing anti-unmanned aerial vehicle device is relatively short, and it is difficult to cope with long-distance unmanned aerial vehicle threat, so the utility model provides a kind of airborne high-explosive gas type anti-unmanned aerial vehicle capture net launching device. UTILITY MODEL CONTENT
[0003] The utility model provides a kind of airborne high-explosive gas type anti-unmanned aerial vehicle capture net launching device for the defects of prior art, overcomes the anti-unmanned aerial vehicle device capture efficiency is low, often difficult to quickly and accurately capture target unmanned aerial vehicle, and the problem of poor stability.
[0004] To achieve the above object, the utility model provides the following technical scheme: a kind of airborne high-explosive gas type anti-unmanned aerial vehicle capture net launching device, including launch cylinder, the inside of launch cylinder is provided with separation round plate, separation round plate is separated into high-explosive chamber and launch chamber by the inside of launch cylinder, high-explosive chamber is used to store gas generating agent, launch chamber is used to place capture net, separation round plate is fixed with launch cylinder pipe in the circumferential array on separation round plate, launch cylinder pipe is respectively used to place rubber ball block on the corner of capture net 4, the end of launch cylinder pipe closest to high-explosive chamber is communicated with high-explosive chamber, limit unit and separation unit are further provided on launch cylinder, limit unit includes four limit sliding plates, limit sliding plate is slidably matched with corresponding launch cylinder pipe, limit sliding plate is used to limit the position of rubber ball block on launch cylinder pipe, separation unit includes four separation sliding plates, the end of separation sliding plate closest to separation round plate axis is fixedly provided with separation round block, separation round block is respectively used to block the communication of corresponding launch cylinder pipe and high-explosive chamber.
[0005] Further, the end face of launch cylinder farthest from launch chamber is fixedly installed with controller, and the high-explosive chamber is also fixedly installed with a striker, the controller is used to control the striker, the striker is used to detonate the gas in the high-explosive chamber, and the end of the launch cylinder farthest from the high-explosive chamber is fixedly provided with a thin plate.
[0006] Further, the four limiting sliding plates are circumferentially arranged and slidably mounted on the launching cylinder, limiting springs are arranged between the limiting sliding plates and the launching cylinder, and side surfaces of the limiting sliding plates are fixedly provided with adjusting blocks two, four limiting blocks two are fixedly arranged on the circumferential array of the separating disc, and the limiting blocks two are used for limiting the moving positions of the corresponding adjusting blocks two.
[0007] Further, the outer side of the launching cylinder is also slidably provided with an annular sliding seat, an annular chamber is arranged in the inner side of the annular sliding seat, four arc-shaped electromagnets are fixedly arranged in the circumferential array of the annular chamber of the annular sliding seat, the arc-shaped electromagnets are used for adjusting the positions of the corresponding limiting sliding plates, the outer side of the launching cylinder is also fixedly provided with an annular limiting plate, and the annular limiting plate is used for limiting the moving positions of the annular sliding seat.
[0008] Further, the four separating sliding plates are circumferentially arranged and slidably mounted on the launching cylinder, separating springs are arranged between the separating sliding plates and the launching cylinder, side surfaces of the separating sliding plates are also fixedly provided with adjusting blocks one, and the side surfaces of the separating sliding plates are also provided with two limiting blocks one, the limiting blocks one are fixedly mounted on the separating disc, the adjusting blocks one are located between the corresponding two limiting blocks one, and the limiting blocks one are used for limiting the moving positions of the adjusting blocks one.
[0009] Further, the outer side of the launching cylinder is also slidably provided with an annular sliding seat, an annular chamber is arranged in the inner side of the annular sliding seat, four arc-shaped electromagnets are fixedly arranged in the circumferential array of the annular chamber of the annular sliding seat, the arc-shaped electromagnets are used for adjusting the positions of the corresponding limiting sliding plates, the outer side of the launching cylinder is also fixedly provided with an annular limiting plate, and the annular limiting plate is used for limiting the moving positions of the annular sliding seat.
[0010] Further, the outer side of the launching cylinder is also slidably provided with an annular sliding seat, an annular chamber is arranged in the inner side of the annular sliding seat, four arc-shaped electromagnets are fixedly arranged in the circumferential array of the annular chamber of the annular sliding seat, the arc-shaped electromagnets are used for adjusting the positions of the corresponding limiting sliding plates, the outer side of the launching cylinder is also fixedly provided with an annular limiting plate, and the annular limiting plate is used for limiting the moving positions of the annular sliding seat.
[0011] Further, the outer side of the launching cylinder is also slidably provided with an annular sliding seat, an annular chamber is arranged in the inner side of the annular sliding seat, four arc-shaped electromagnets are fixedly arranged in the circumferential array of the annular chamber of the annular sliding seat, the arc-shaped electromagnets are used for adjusting the positions of the corresponding limiting sliding plates, the outer side of the launching cylinder is also fixedly provided with an annular limiting plate, and the annular limiting plate is used for limiting the moving positions of the annular sliding seat.
[0012] Further, the outer side of the launching cylinder is also slidably provided with an annular sliding seat, an annular chamber is arranged in the inner side of the annular sliding seat, four arc-shaped electromagnets are fixedly arranged in the circumferential array of the annular chamber of the annular sliding seat, the arc-shaped electromagnets are used for adjusting the positions of the corresponding limiting sliding plates, the outer side of the launching cylinder is also fixedly provided with an annular limiting plate, and the annular limiting plate is used for limiting the moving positions of the annular sliding seat.
[0013] The utility model discloses the beneficial effect compared with prior art is: (1) the utility model discloses can through high blast gas and produce the thrust, and the capture net is rapidly launched, has quick, and the interference of side wind is small and attack distance long characteristics, thereby can capture the fast flight of the through machine. BRIEF DESCRIPTION OF DRAWINGS
[0014] Figure 1 It is the whole structure schematic diagram of the utility model.
[0015] Figure 2 It is the structure schematic diagram of annular protection cover inside of the utility model.
[0016] Figure 3 It is the structure schematic diagram of annular slide plate place of the utility model.
[0017] Figure 4 It is Figure 3 The partial close -up schematic drawing of A place in.
[0018] Figure 5 It is the structure schematic diagram of the utility model separation round plate place.
[0019] Figure 6 It is the structure schematic diagram of the utility model launch cylinder inside.
[0020] Figure 7 It is the structure schematic diagram of the utility model separation slide plate place.
[0021] Figure 8 It is Figure 7 The partial close -up schematic drawing of B place in.
[0022] Figure 9 It is the structure schematic diagram of the utility model launch pipe place.
[0023] Figure 10 It is Figure 9 The partial close -up schematic drawing of C place in.
[0024] Figure 11 It is the sectional view of the whole structure of the utility model.
[0025] 101 - launching cylinder; 102 - annular protective cover; 103 - thin plate; 104 - controller; 105 - annular slide; 106 - annular slide plate; 107 - annular electromagnet I; 108 - annular electromagnet II; 109 - right-angle push plate; 110 - unfolding short column; 111 - separating slide plate; 112 - limiting plate; 113 - separating spring; 114 - separating circular plate; 115 - launching cylinder pipe; 116 - firing device; 117 - separating circular block; 118 - limiting slide plate; 119 - annular limiting plate; 120 - position adjusting block I; 121 - limiting block I; 122 - position adjusting block II; 123 - limiting block II; 124 - limiting spring; 125 - arc-shaped electromagnet; 126 - high-explosive chamber; 127 - launching chamber. DETAILED DESCRIPTION
[0026] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model.
[0027] Embodiment: Reference Figures 1-11 A kind of airborne high-explosive gas type anti-unmanned aerial vehicle capture net launching device, including launching cylinder 101, the inner side of launching cylinder 101 is provided with separating circular plate 114, separating circular plate 114 separates the inside of launching cylinder 101 into high-explosive chamber 126 and launching chamber 127, the end of launching cylinder 101 farthest from high-explosive chamber 126 is fixedly provided with thin plate 103, high-explosive chamber 126 is located between launching cylinder 101 and separating circular plate 114, launching chamber 127 is located between launching cylinder 101, thin plate 103, separating circular plate 114, high-explosive chamber 126 is used to store gas generating agent, launching chamber 127 is used to place capture net, separating circular plate 114 is fixedly provided with launching cylinder pipe 115 in the circumferential array on separating circular plate 114, and launching cylinder pipe 115 is respectively used to place rubber ball block on the four corners of capture net 4, and the end of launching cylinder pipe 115 closest to high-explosive chamber 126 is communicated with high-explosive chamber 126.
[0028] The end face of launching cylinder 101 farthest from launching chamber 127 is fixedly installed with controller 104, and firing device 116 is also fixedly installed in high-explosive chamber 126, controller 104 is used to control firing device 116, and firing device 116 is used to detonate the gas in high-explosive chamber 126, and the gas generating agent in the inside of high-explosive chamber 126 is sodium azide and potassium nitrate.
[0029] When the controller 104 receives the firing signal, the controller 104 controls the firing device 116 to ignite the gas generating agent in the high-explosion chamber 126. A large amount of gas is generated in the high-explosion chamber 126, and the gas is sprayed out along the launch cylinder 115. The rubber ball blocks in the launch cylinder 115 move outward under the action of the gas thrust. The rubber ball blocks break the thin plate 103 and fly outward, so that the capture net in the launch chamber 127 flies outward under the action of the rubber ball blocks, and the rubber ball blocks break the thin plate 103 and fly outward.
[0030] The launch cylinder 101 is also provided with a limiting unit. The limiting unit includes four limiting sliding plates 118. The four limiting sliding plates 118 are circumferentially arrayed and slidingly installed on the launch cylinder 101. The limiting sliding plate 118 is slidingly matched with the corresponding launch cylinder 115. The limiting sliding plate 118 is used to limit the position of the rubber ball block on the launch cylinder 115. A limiting spring 124 is arranged between the limiting sliding plate 118 and the launch cylinder 101. The side surface of the limiting sliding plate 118 is fixedly provided with a position adjusting block two 122. Four limiting blocks two 123 are circumferentially arrayed and fixedly arranged on the separation circular plate 114. The limiting block two 123 is used to limit the movement position of the corresponding position adjusting block two 122.
[0031] The outer side of the launch cylinder 101 is also slidingly installed with an annular sliding seat 105. The inner side of the annular sliding seat 105 is provided with an annular chamber. Four arc-shaped electromagnets 125 are circumferentially arrayed and fixedly arranged in the annular chamber of the annular sliding seat 105. The arc-shaped electromagnets 125 are used to adjust the position of the corresponding limiting sliding plate 118. The outer side of the launch cylinder 101 is also fixedly installed with an annular limiting plate 119. The annular limiting plate 119 is used to limit the movement position of the annular sliding seat 105.
[0032] In the initial position, the annular sliding seat 105 is not in contact with the annular limiting plate 119. The limiting sliding plate 118 is located at the position closest to the axis of the launch cylinder 101. At this time, the limiting spring 124 is not compressed. The inner circumferential surface of the annular sliding seat 105 is in contact with the end surface of the limiting sliding plate 118 farthest from the axis of the launch cylinder 101. Under the action of the annular sliding seat 105, the limiting sliding plate 118 cannot move away from the axis of the launch cylinder 101. At this time, the end of the limiting sliding plate 118 closest to the axis of the launch cylinder 101 is located on the inner side of the launch cylinder 115. At this time, the rubber ball block is located between the limiting sliding plate 118 and the separation circular plate 114. Under the action of the limiting sliding plate 118, the position of the rubber ball block in the launch cylinder 115 is limited, that is, the positions of the four rubber ball blocks in the respective launch cylinders 115 are the same.
[0033] The pushing ring-shaped sliding seat 105 is moved towards the direction close to the ring-shaped limiting plate 119, that is, the ring-shaped sliding seat 105 is gradually separated from the contact with the limiting sliding plate 118, and finally the ring-shaped sliding seat 105 is moved to contact the ring-shaped limiting plate 119, at this time, the ring-shaped cavity of the ring-shaped sliding seat 105 is not directly above the limiting sliding plate 118, that is, at this time, the limiting spring 124 is directly above the corresponding limiting sliding plate 118, and then the arc-shaped electromagnet 125 is started to adsorb the limiting sliding plate 118, that is, the limiting sliding plate 118 is moved towards the direction close to the corresponding limiting sliding plate 118, and finally the limiting sliding plate 118 is moved to the position farthest from the axis of the launching cylinder 101, the limiting spring 124 is compressed, at this time, the position adjusting block two 122 is in contact with the corresponding limiting block two 123, at this time, the surface of the limiting sliding plate 118 closest to the axis of the launching cylinder 101 and the inner circumferential surface of the launching circular pipe 115 are on the same circumferential surface, at this time, the rubber ball block can move freely in the launching circular pipe 115, that is, the limiting sliding plate 118 contacts the limiting position of the rubber ball block.
[0034] The launching cylinder 101 is also provided with a separation unit, the separation unit includes four separation sliding plates 111, the four separation sliding plates 111 are circumferentially arrayed and slidingly installed on the launching cylinder 101, the separation sliding plate 111 and the launching cylinder 101 are both provided with a separation spring 113, the end of the separation sliding plate 111 closest to the axis of the separation circular plate 114 is fixedly provided with a separation circular block 117, the separation circular block 117 is used to block the communication between the corresponding launching circular pipe 115 and the high-explosive chamber 126, the side of the separation sliding plate 111 is also fixedly provided with a position adjusting block one 120, the side of the separation sliding plate 111 is also provided with two limiting blocks one 121, the limiting blocks one 121 are fixedly installed on the separation circular plate 114, the position adjusting block one 120 is located between the corresponding two limiting blocks one 121, and the limiting blocks one 121 are used to limit the movement position of the position adjusting block one 120.
[0035] In the initial position, the separation springs 113 are not compressed, and the separation sliding plates 111 are located closest to the axis of the launching cylinder 101, that is, the separation circular blocks 117 are located closest to the axis of the launching cylinder 101, the separation circular blocks 117 cover the connection between the corresponding launching circular pipe 115 and the high-explosive chamber 126, and at this time, the position adjusting block one 120 is in contact with the limiting block one 121 closest to the axis of the launching cylinder 101 among the corresponding two limiting blocks one 121.
[0036] The separation slide plate 111 is pushed to move away from the axis of the launching cylinder 101, the separation spring 113 is stretched, i.e. the separation circular block 117 is moved away from the axis of the launching cylinder 101, i.e. the positioning block 120 is moved away from the limiting block 121 closest to the axis of the launching cylinder 101, and finally the positioning block 120 contacts the limiting block 121 farthest from the axis of the launching cylinder 101 among the two corresponding limiting blocks 121, at this time the separation circular block 117 completely removes the shielding of the connecting part between the high-explosive chamber 126 and the launching cylinder 115.
[0037] The annular slide plate 106 is also slidingly installed on the launching cylinder 101, the annular slide plate 106 and the annular slide seat 105 are slidingly matched, springs are arranged between the annular slide plate 106 and the annular slide seat 105, four right-angle push plates 109 are fixedly arranged in a circumferential array on the annular slide plate 106, and the side surface of the separation slide plate 111 is also fixedly installed with a deployment short column 110, the right-angle push plate 109 is used for pushing the corresponding deployment short column 110 to move, and four limiting plates 112 are also fixedly arranged in a circumferential array on the annular slide seat 105, and the limiting plate 112 is used for limiting the position of the corresponding separation slide plate 111.
[0038] In the initial position, the annular slide plate 106 is located at the position farthest from the annular limiting plate 119, the springs between the annular slide plate 106 and the annular slide seat 105 are not compressed, i.e. the annular slide plate 106 is located at the position farthest from the annular slide seat 105, at this time the surface of the limiting plate 112 closest to the axis of the launching cylinder 101 and the surface of the separation slide plate 111 farthest from the axis of the launching cylinder 101, under the action of the limiting plate 112, the separation slide plate 111 cannot move away from the axis of the launching cylinder 101, i.e. the position of the separation slide plate 111 is locked, thereby preventing the position of the separation circular block 117 from moving, and at this time the right-angle push plate 109 does not contact the corresponding deployment short column 110.
[0039] The annular slide plate 106 is pushed to move, under the action of the springs between the annular slide plate 106 and the annular slide seat 105, the annular slide seat 105 moves synchronously, so that the annular slide seat 105 contacts the annular limiting plate 119, under the action of the annular limiting plate 119, the annular slide seat 105 cannot continue to move, at this time the inclined surface of the right-angle push plate 109 contacts the corresponding deployment short column 110, and at this time the limiting plate 112 is separated from the corresponding separation slide plate 111, the annular slide plate 106 continues to move, the springs between the annular slide plate 106 and the annular slide seat 105 are compressed, under the action of the right-angle push plate 109, the deployment short column 110 moves away from the axis of the launching cylinder 101, i.e. the separation slide plate 111 moves away from the axis of the launching cylinder 101, i.e. under the action of the right-angle push plate 109 and the deployment short column 110, the movement of the separation slide plate 111 is realized.
[0040] The annular electromagnetic iron two 108 is fixedly installed on the launching cylinder 101, the annular electromagnetic iron one 107 is fixedly installed on the surface of the annular electromagnetic iron two 108 closest to the annular electromagnetic iron one 107, the annular electromagnetic iron two 108 is used for pushing the annular electromagnetic iron one 107 to move, and the annular protective cover 102 is further fixedly installed on the launching cylinder 101, and the annular protective cover 102 is used for protecting parts outside the launching cylinder 101.
[0041] When the initial position is, the annular electromagnetic iron one 107 is located at the position closest to the annular electromagnetic iron two 108, at this time, the separation round block 117 and the limiting slide plate 118 are all in the output position, the annular electromagnetic iron one 107 is controlled to move away from the annular electromagnetic iron two 108, so that the annular slide plate 106 moves.
[0042] Working principle: after the controller 104 receives the firing signal, the annular electromagnetic iron one 107 and the annular electromagnetic iron two 108 are started, the annular slide plate 106 moves away from the annular electromagnetic iron two 108, the limiting slide plate 118 is first moved to the position farthest from the axis of the launching cylinder 101, that is, the limiting unit releases the limitation on the position of the rubber ball block, then the separation round block 117 is moved to the position farthest from the axis of the launching cylinder 101, that is, the separation unit releases the blockage of the connecting part between the launching cylinder 115 and the high-explosive chamber 126, then the trigger 116 is started to detonate the gas generating agent in the high-explosive chamber 126, under the action of the high-pressure gas, the rubber ball block in the launching cylinder 115 flies out under the action of the high-pressure gas, the rubber ball block breaks the sheet 103 and flies out, and the capture net in the launching chamber 127 is unfolded and flies out under the action of the rubber ball block.
[0043] The utility model is not limited to the above-mentioned specific implementation, and various transformations made by the skilled in the art without creative labor, based on the above-mentioned concept, all fall within the protection scope of the utility model.
Claims
1. An airborne high-explosive gas type anti-UAV capture net launcher device, comprising a launching cylinder (101), characterized in that: a separation disc (114) is arranged inside the launching cylinder (101), the separation disc (114) separates the inside of the launching cylinder (101) into a high-explosive chamber (126) and a launching chamber (127), the high-explosive chamber (126) is used for storing a gas generating agent, and the launching chamber (127) is used for placing a capture net; the separation disc (114) is fixedly provided with a circumferential array of launching cylinders (115) on the separation disc (114), the launching cylinders (115) are respectively used for placing rubber ball blocks at four corners of the capture net, and the ends of the launching cylinders (115) closest to the high-explosive chamber (126) are all in communication with the high-explosive chamber (126); a limiting unit and a separation unit are further arranged on the launching cylinder (101), the limiting unit comprises four limiting slides (118) which are in sliding fit with the corresponding launching cylinders (115), the limiting slides (118) are used for limiting the positions of the rubber ball blocks on the launching cylinders (115), and the separation unit comprises four separation slides (111), the ends of the separation slides (111) closest to the axis of the separation disc (114) are all fixedly provided with separation blocks (117), and the separation blocks (117) are respectively used for blocking the communication between the corresponding launching cylinders (115) and the high-explosive chamber (126). A controller (104) is fixedly installed on the end face of the launching cylinder (101) farthest from the launching chamber (127), a firing device (116) is further fixedly installed in the high-explosive chamber (126), the controller (104) is used for controlling the firing device (116), and the firing device (116) is used for detonating the gas in the high-explosive chamber (126); and a thin plate (103) is fixedly arranged on the end of the launching cylinder (101) farthest from the high-explosive chamber (126).
2. The airborne high-explosive-gas anti-UAV capture net launcher according to claim 1, characterized in that: The four limiting slides (118) are circumferentially and slidably installed on the launching cylinder (101), limiting springs (124) are arranged between the limiting slides (118) and the launching cylinder (101), side faces of the limiting slides (118) are all fixedly provided with position adjusting blocks two (122), and four limiting blocks two (123) are circumferentially and fixedly arranged on the separation disc (114), the limiting blocks two (123) are used for limiting the movement positions of the corresponding position adjusting blocks two (122).
3. The airborne high-explosive-gas anti-UAV capture net launcher according to claim 2, characterized in that: An annular slide (105) is further slidably installed on the outside of the launching cylinder (101), an annular chamber is arranged inside the annular slide (105), four arc-shaped electromagnets (125) are circumferentially and fixedly arranged in the annular chamber of the annular slide (105), the arc-shaped electromagnets (125) are used for adjusting the positions of the corresponding limiting slides (118), and an annular limiting plate (119) is further fixedly installed on the outside of the launching cylinder (101), the annular limiting plate (119) is used for limiting the movement positions of the annular slide (105).
4. The airborne high-explosive-gas anti-UAV capture net launcher according to claim 3, characterized in that: 5. The airborne high-explosive-gas anti-UAV capture net launcher according to claim 4, characterized in that: The 4 separate slide plates (111) circumferential array is slidably mounted on the launching cylinder (101), and the separate slide plate (111) and the launching cylinder (101) are provided with a separate spring (113), the side of the separate slide plate (111) is further provided with a position adjusting block one (120), the side of the separate slide plate (111) is further provided with two limit blocks one (121), the limit block one (121) is fixedly installed on the separate circular plate (114), the position adjusting block one (120) is located between the corresponding two limit blocks one (121), and the limit block one (121) is used to limit the movement position of the position adjusting block one (120).
6. The airborne high-explosive-gas anti-UAV capture net launcher according to claim 5, characterized in that: The launching cylinder (101) is further provided with an annular slide plate (106), the annular slide plate (106) and the annular slide plate (106) are slidably connected, the annular slide plate (106) and the annular slide plate (106) are provided with a spring, and the annular slide plate (106) is provided with four right angle push plates (109) in circumferential array, the side of the separate slide plate (111) is further provided with an unfolding short column (110), and the right angle push plate (109) is used to push the corresponding unfolding short column (110) to move.
7. The airborne high-explosive-gas anti-UAV capture net launcher according to claim 6, characterized in that: The annular slide plate (105) is further provided with four limit plates (112) in circumferential array, and the limit plate (112) is used to limit the position of the corresponding separate slide plate (111).
8. The airborne high-explosive-gas anti-UAV capture net launcher according to claim 7, characterized in that: The launching cylinder (101) is further provided with an annular electromagnetic iron two (108), the surface of the annular electromagnetic iron one (107) closest to the annular electromagnetic iron two (108) is fixedly installed, the annular electromagnetic iron two (108) is used to push the annular electromagnetic iron one (107) to move.
9. The airborne high-explosive-gas anti-UAV capture net launcher according to claim 8, characterized in that: The launching cylinder (101) is further provided with an annular protective cover (102), and the annular protective cover (102) is used to protect the parts outside the launching cylinder (101).