CN210258868U - Unmanned aerial vehicle launching tube - Google Patents
Unmanned aerial vehicle launching tube Download PDFInfo
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- CN210258868U CN210258868U CN201920941841.0U CN201920941841U CN210258868U CN 210258868 U CN210258868 U CN 210258868U CN 201920941841 U CN201920941841 U CN 201920941841U CN 210258868 U CN210258868 U CN 210258868U
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Abstract
The utility model belongs to the technical field of the unmanned aerial vehicle transmission, concretely relates to unmanned aerial vehicle launching tube. At present, a single medicine box is used for charging medicine as an energy source, and light, sound, smoke and heat with certain intensity can be generated during emission, so that the medicine box is not beneficial to concealment in a battlefield; simultaneously, this utility model can not adjust the penetrating angle, various penetrating angle's requirement when being unfavorable for various topography. The utility model provides an unmanned aerial vehicle launching tube that can conceal transmission and adjust transmission angle when needs. The cylinder body is sequentially provided with a fixing ring and a shearing cover at an emission opening, a piston is arranged in the cylinder body, and an integrated valve and a protective cover are fixed at the rear seat end of the cylinder body; the main body of the integrated valve is a valve block, a blasting cartridge assembly, a gas cylinder and a gas control valve are installed on the bottom end face of the valve block, and a one-way head is installed on the top end face of the valve block. The structure is simple, the weight is light, and the operation is convenient; can be repeatedly used.
Description
Technical Field
The utility model belongs to the technical field of the unmanned aerial vehicle transmission, concretely relates to unmanned aerial vehicle launching tube.
Background
The invention patent application with the application number of 201710934256.3 relates to an unmanned aerial vehicle launching device, which comprises an inner circle and an outer square launching canister, a high-low pressure launching chamber, a shear pull rod, a front support and a rear support; the inner circle and outer square launching cylinders are fixed with the rear support through bolts, wherein the inner circle and outer square launching cylinders guarantee the pressure bearing and the overall dimension of an inner cylinder during launching; the high-low pressure launching chamber is a power source and provides power for the launching device by utilizing the principle of high-pressure combustion of medicine box charging and low-pressure expansion acting; the shearing pull rod provides a certain pre-tightening force for the launching of the unmanned aerial vehicle, when the pressure of the low-pressure pesticide chamber reaches the shearing force of the shearing pin, the shearing pin is sheared, and the unmanned aerial vehicle starts to move under the action of the launching cylinders which are round inside and square outside; fore-stock and after-poppet provide the support for the unmanned aerial vehicle transmission, and the after-poppet still plays the effect of buffering recoil simultaneously.
The application uses a single medicine box for charging as an energy source, and light, sound, smoke and heat with certain intensity can be generated during emission, so that the application is not beneficial to concealment in a battlefield; simultaneously, this utility model can not adjust the penetrating angle, various penetrating angle's requirement when being unfavorable for various topography.
Unmanned aerial vehicle emitter among the prior art ubiquitous above-mentioned problem.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the technical problem who solves: in order to solve among the prior art the problem that exposes the transmission position easily among the unmanned aerial vehicle transmitting process, can not adjust the transmission shooting angle, the utility model provides a can conceal the unmanned aerial vehicle launch canister who launches and adjust the transmission shooting angle when needs.
An unmanned aerial vehicle launching tube comprises a tube body and a supporting structure, wherein a fixing ring and a shearing cover are sequentially arranged on a launching port of the tube body, a piston is arranged in the tube body, an unmanned aerial vehicle is arranged between the piston and the shearing cover, an integration valve and a protective cover are fixed on the tube body at the end of a rear seat, and an air leakage hole is formed in the tube body at a position close to the launching port; the integrated valve is characterized in that the main body of the integrated valve is a valve block, a blasting cartridge assembly, a gas cylinder and a gas control valve are mounted on the bottom end face of the valve block, a one-way head is mounted on the top end face of the valve block, and the blasting cartridge assembly releases gas to a piston through an airflow channel in the valve block; the gas cylinder is communicated with the gas control valve through a pipeline in the valve block, the outlet of the gas control valve is communicated with the one-way head, and the one-way head is opened under the action of air pressure.
The one-way head comprises a sleeve, a plug, a baffle ring, a spring and a sleeve cover, wherein the spring is arranged in the sleeve cover at the outer end part of the sleeve, the sleeve is provided with a limiting ring in the middle area, the plug and the baffle ring penetrate through the limiting ring through a connecting rod, an air outlet hole is formed in the wall surface of the sleeve, and the spring extrudes the baffle ring so as to seal the air outlet hole through the plug.
The supporting structure comprises a retractable rear support and an angle adjuster, and the angle adjuster comprises an adjusting rod, a transfer block and a supporting rod; the adjusting rod is hinged with a fixing block A on the cylinder and is clamped when the adjusting rod is opened in place; a pair of connecting blocks are positioned in front of and behind the adjusting rod through adjusting pins; the two sides of the switching block are hinged with supporting rods through rotating pins, and the supporting rods are clamped when being opened in place.
The adjusting rod is provided with a plurality of adjusting holes.
And the barrel is also provided with a fixed block B which is fixedly connected with the fixed block B when the rear support is retracted.
The barrel is also provided with a fixing block C which is fixedly connected with the supporting rod when the supporting rod is retracted.
The fixed ring is provided with a plurality of protruding blocks distributed on the periphery of the inner ring, so that the unmanned aerial vehicle can be guided during installation and launching, and the piston is prevented from leaving the cylinder during launching.
The inner end face of the shearing cover is also provided with a structure for providing pretightening force for the unmanned aerial vehicle.
Has the advantages that: adopt the utility model discloses an unmanned aerial vehicle launch canister has following a plurality of advantages:
a) the structure is simple, the weight is light, and the operation is convenient;
b) the storage, transportation and delivery are integrated, and the functions are various;
c) can be repeatedly used;
d) the rear support and the angle regulator can be fixed on the main body, so that the carrying is convenient;
e) the unmanned aerial vehicle can be carried and launched by a single person, so that the labor cost is saved;
f) the shooting angle can be adjusted in multiple gears, so that the requirements of different terrains and unmanned aerial vehicle launching are met;
g) two emission energy sources are provided, and advantages are complementary;
h) the projectile and the gas emission are physically isolated, so that the two energy sources are ensured to be emitted independently;
i) when the unmanned aerial vehicle is launched through gas, the unmanned aerial vehicle has certain launching concealment;
j) when the blasting bomb is used as the launching energy, the portable bomb is convenient to carry.
Drawings
Fig. 1 is an axonometric view of the launch status of a launch canister of an unmanned aerial vehicle.
Fig. 2 is an unmanned aerial vehicle launching tube fold state elevation.
Fig. 3 is a sectional view a-a of fig. 2.
FIG. 4 is a perspective view of the integrated valve shaft.
Fig. 5 is a front view of the integration valve.
Fig. 6 is a sectional view B-B of fig. 5.
Fig. 7 is a schematic view of an angle adjuster.
Fig. 8 is a diagram of a one-way head free state.
Fig. 9 is a diagram of a one-way header compression state.
Wherein, 1, the cylinder body; 2. a piston; 3. a fixing ring; 4. shearing the cover; 5. an integration valve; 6. a protective cover; 7. rear support; 8. an angle adjuster; 9. a valve block; 10. a squib assembly; 11. a gas cylinder; 12. a pneumatic control valve; 13. a one-way head; 14. adjusting a rod; 15. an adjustment pin; 16. a rotation pin; 17. a transfer block; 18. a support bar; 19. a sleeve; 20. a plug; 21. a baffle ring; 22. a spring; 23. a sleeve cover; 24. an unmanned aerial vehicle; 25. a fixed block A; 26. a fixed block B; 27. a fixed block C; 28. an air outlet; 29. an air release hole; 30. a hole A; 31. a pipeline; 32. a hole B; 33. hole C
Detailed Description
As shown in fig. 1, the utility model discloses an unmanned aerial vehicle launch canister mainly comprises barrel 1, piston 2, solid fixed ring 3, shearing lid 4, pile-up valve 5, visor 6, back support 7 and angle regulator 8. Wherein, the integrated valve 5 consists of a valve block 9, a blasting bomb component 10, a gas cylinder 11, a gas control valve 12 and a one-way head 13. The angle adjuster is composed of an adjusting rod 14, an adjusting pin 15, a rotating pin 16, a switching block 17 and a supporting rod 18. The one-way head 13 comprises a sleeve 19, a plug 20, a stop ring 21, a spring 22 and a sleeve cover 23.
A piston 2 is arranged in the cylinder 1; a fixed ring 3 and a shearing cover 4 are sequentially fixed at the emission outlet end of the cylinder body 1, and an unmanned aerial vehicle 24 can be arranged in the cylinder body 1 and between the piston 2 and the shearing cover 4; an integrated valve 5 and a protective cover 6 are fixed at the rear seat end of the cylinder body 1; the rear support 7 is mounted on the protective cover 6. The barrel 1 is provided with a fixing block 25, the angle adjuster 8 is hinged with the fixing block A25 at the top and can rotate back and forth, and the angle adjuster is clamped on the fixing block 25 after rotating forward for a certain angle. The piston 2 is fixed in the cylinder 1 between the integration valve 5 and the fixing ring 3. Solid fixed ring 3 is fixed in 1 unmanned aerial vehicle exit end of barrel, and solid fixed ring 3 inner ring distributes all around has the protruding piece of everywhere for unmanned aerial vehicle 24 provides the direction when installation and transmission, and can block piston 2 and leave barrel 1 when unmanned aerial vehicle 24 transmits. Cut lid 4 and fix on solid fixed ring 3, provide the protection for unmanned aerial vehicle when the transmission. In the integrated valve 5, a blasting bomb component 10, a gas cylinder 11 and a pneumatic control valve 12 are arranged on one side of a valve block 9, and a one-way head 13 is arranged on the other side of the valve block 9. In the one-way head 13, a plug 20 is connected to a stopper ring 21 and is installed in a sleeve 19, a sleeve cover 23 is fixed to one end of the sleeve 19, and a spring 22 is installed between the sleeve cover 23 and the stopper ring 21. The angle regulator 8, the bracing piece 18 is fixed on the switching piece 17 through the swivel pin 16, there are multiple through holes on the regulating lever 14, the regulating pin 15 passes the different holes on switching piece 17 and regulating lever and realizes the angle regulation.
When installing unmanned aerial vehicle 24, with folding unmanned aerial vehicle 24 along solid fixed ring 3 guided into barrel 1, after unmanned aerial vehicle 24 got into barrel 1 completely, will cut lid 4 and install on solid fixed ring 3.
Before launching unmanned aerial vehicle 24, rotatory back support 7 is unscrewed from fixed block B26 on the visor 6, and places it in barrel 1 bottom and the parallel department of ground. Taking the supporting rod 18 out of the fixing block C27 of the protective cover 6, rotating the angle adjuster 8 to a certain angle, and clamping the angle adjuster 8 on the fixing block A25; rotating the support rod 18 to a certain angle, and clamping the support rod 18 on the transfer block 17; the launching angle is adjusted through the adjusting rod 14, and after the angle adjustment is completed, the adjusting pin 15 is clamped between the transfer block 17 and the adjusting rod 14 and is fixed.
When launching unmanned aerial vehicle 24, the unmanned aerial vehicle is launched to two kinds of energy of accessible blasting bomb and gas source system.
When the blasting cartridge is used as a launching energy source, the spring 22 in the one-way head 13 applies pressure to the baffle ring 21 and presses the baffle ring to the limiting ring on the inner side of the sleeve 19, the baffle ring 21 is fixed with the plug 20, the plug 20 isolates the gas outlet 28 from the gas channel, and the one-way head 13 isolates the gas channel from the gunpowder gas to prevent the gunpowder gas from entering the gas channel. Gunpowder gas passes through the passageway in the valve block 9 and reaches piston 2, and along with the increase of gunpowder gas pressure, piston 2 promotes unmanned aerial vehicle 24 to push shear cover 4 open, unmanned aerial vehicle 24 leaves barrel 1 along solid fixed ring 3 direction with certain speed, and after piston 2 arrived the certain distance, atmospheric pressure spilled over from the disappointing hole 29 on the barrel 1, and piston 2 continues the motion, and final jamming is on solid fixed ring 3.
When gas is used as energy, the pneumatic control valve 12 is opened, gas in the gas cylinder 11 continuously enters the pipeline 31 from the hole A30 and flows into the pneumatic control valve 12 from the hole B32, then enters the one-way head 13 from the hole C33, the plug 20 in the one-way head 13 moves along the axial direction of the sleeve 19 to the sleeve cover 23 under the action of air pressure and is blocked by the limiting ring on the inner side of the sleeve 19, the plug 20 does not block the gas outlet 28 any more, and the gas overflows from the gas outlet 28; along with the increase of gas pressure, piston 2 promotes unmanned aerial vehicle 24 to push shear cover 4 open, unmanned aerial vehicle 24 is led along solid fixed ring 3 with certain speed and is left barrel 1, and after piston 2 arrived the certain distance, atmospheric pressure spills over from the disappointing hole 29 on the barrel 1, and piston 2 continues the motion, and the final jamming is on solid fixed ring 3. As the gas pressure decreases, the ring 21 moves in the spring 22, which moves the plug 20, and the plug 20 isolates the gas outlet 28 from the gas channel.
After the unmanned aerial vehicle 24 finishes launching, the angle regulator 8 is retracted and fixed on a fixing block C27 of the protective cover 6; the rear support 6 is retracted and fixed to the protective cover 6 at block B26. The recovery of unmanned aerial vehicle launching canister is accomplished, waits for unmanned aerial vehicle 24 to load next time.
Claims (8)
1. The utility model provides an unmanned aerial vehicle launch canister, includes barrel (1) and bearing structure, its characterized in that: the cylinder body (1) is sequentially provided with a fixing ring (3) and a shearing cover (4) at an emitting opening, a piston (2) is arranged in the cylinder body (1), an unmanned aerial vehicle (24) is arranged between the piston (2) and the shearing cover (4), the cylinder body (1) is fixedly provided with an integrated valve (5) and a protective cover (6) at the rear seat end, and the cylinder body (1) is provided with an air leakage hole (29) at a position close to the emitting opening; the integrated valve (5) is characterized in that a main body is a valve block (9), a blasting cartridge assembly (10), a gas cylinder (11) and a gas control valve (12) are installed on the bottom end face of the valve block (9), a one-way head (13) is installed on the top end face of the valve block, and the blasting cartridge assembly (10) releases gas to a piston (2) through an airflow channel in the valve block (9); the gas bottle (11) and the pneumatic control valve (12) are communicated through a pipeline (31) in the valve block (9), the outlet of the pneumatic control valve (12) is communicated with the one-way head (13), and the one-way head (13) is opened under the action of air pressure.
2. The unmanned aerial vehicle launch canister of claim 1, wherein: the unidirectional head (13) comprises a sleeve (19), a plug (20), a baffle ring (21), a spring (22) and a sleeve cover (23), the spring (22) is arranged in the sleeve cover (23) at the outer end part of the sleeve (19), the sleeve (19) is provided with a limiting ring in the middle area, the plug (20) and the baffle ring (21) penetrate through the limiting ring through a connecting rod, an air outlet hole (28) is formed in the wall surface of the sleeve (19), and the spring (22) extrudes the baffle ring (21) so as to seal the air outlet hole (28) through the plug (20).
3. The unmanned aerial vehicle launch canister of claim 1 or 2, wherein: the supporting structure comprises a retractable rear support (7) and an angle adjuster (8), and the angle adjuster (8) comprises an adjusting rod (14), a switching block (17) and a supporting rod (18); the adjusting rod (14) is hinged with a fixed block A (25) on the barrel (1) and is clamped when being opened in place; a pair of connecting blocks (17) are positioned in front of and behind the adjusting rod (14) through adjusting pins (15); two sides of the switching block (17) are hinged with supporting rods (18) through rotating pins (16), and the supporting rods (18) are clamped when being opened in place.
4. The unmanned aerial vehicle launch canister of claim 3, wherein: the adjusting rod (14) is provided with a plurality of adjusting holes.
5. The unmanned aerial vehicle launch canister of claim 3, wherein: the barrel (1) is also provided with a fixed block B (26), and when the rear support (7) is folded, the fixed block B (26) is fixedly connected with the rear support.
6. The unmanned aerial vehicle launch canister of claim 3, wherein: the barrel (1) is also provided with a fixed block C (27), and when the support rod (18) is folded, the fixed block C (27) is fixedly connected with the support rod.
7. The unmanned aerial vehicle launch canister of claim 1 or 2, wherein: fixed ring (3) distribute all around at the inner ring has a plurality of lugs, for unmanned aerial vehicle (24) provide the direction when installation and transmission to block piston (2) and leave barrel (1) when the transmission.
8. The unmanned aerial vehicle launch canister of claim 1 or 2, wherein: the inner end face of the shearing cover (4) is also provided with a structure for providing pretightening force for the unmanned aerial vehicle (24).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920941841.0U CN210258868U (en) | 2019-06-21 | 2019-06-21 | Unmanned aerial vehicle launching tube |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920941841.0U CN210258868U (en) | 2019-06-21 | 2019-06-21 | Unmanned aerial vehicle launching tube |
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| Publication Number | Publication Date |
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| CN210258868U true CN210258868U (en) | 2020-04-07 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201920941841.0U Active CN210258868U (en) | 2019-06-21 | 2019-06-21 | Unmanned aerial vehicle launching tube |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113044233A (en) * | 2021-04-30 | 2021-06-29 | 河南华讯方舟航空科技有限公司 | Unmanned aerial vehicle emitter |
| CN113998136A (en) * | 2021-12-02 | 2022-02-01 | 北京机电工程研究所 | Miniature aircraft launching device and method |
| CN114115287A (en) * | 2021-12-06 | 2022-03-01 | 西安航空学院 | Unmanned vehicle-unmanned aerial vehicle air-ground cooperative patrol and guidance system |
-
2019
- 2019-06-21 CN CN201920941841.0U patent/CN210258868U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113044233A (en) * | 2021-04-30 | 2021-06-29 | 河南华讯方舟航空科技有限公司 | Unmanned aerial vehicle emitter |
| CN113044233B (en) * | 2021-04-30 | 2022-12-09 | 河南创仕航空科技有限公司 | Unmanned aerial vehicle emitter |
| CN113998136A (en) * | 2021-12-02 | 2022-02-01 | 北京机电工程研究所 | Miniature aircraft launching device and method |
| CN113998136B (en) * | 2021-12-02 | 2024-01-19 | 北京机电工程研究所 | Micro-aircraft transmitting device and method |
| CN114115287A (en) * | 2021-12-06 | 2022-03-01 | 西安航空学院 | Unmanned vehicle-unmanned aerial vehicle air-ground cooperative patrol and guidance system |
| CN114115287B (en) * | 2021-12-06 | 2023-09-22 | 西安航空学院 | Unmanned vehicle-unmanned aerial vehicle air-ground collaborative patrol and guide system |
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