CN216546775U - Blasting piece individual soldier unmanned aerial vehicle emitter - Google Patents
Blasting piece individual soldier unmanned aerial vehicle emitter Download PDFInfo
- Publication number
- CN216546775U CN216546775U CN202122929417.4U CN202122929417U CN216546775U CN 216546775 U CN216546775 U CN 216546775U CN 202122929417 U CN202122929417 U CN 202122929417U CN 216546775 U CN216546775 U CN 216546775U
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- storage tank
- firing pin
- safety pin
- air storage
- opening mechanism
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Abstract
The utility model relates to the technical field of launching devices, in particular to a rupture disk individual soldier unmanned aerial vehicle launching device which comprises an air storage tank and a launching tube connected with the air storage tank, wherein a rupture disk is arranged between the air storage tank and the launching tube, a firing pin release opening mechanism used for puncturing the rupture disk is arranged in the air storage tank, and a rotatable safety pin is arranged between the firing pin release opening mechanism and the rupture disk.
Description
Technical Field
The utility model relates to the technical field of launching devices, in particular to a single-soldier blasting-piece unmanned aerial vehicle launching device.
Background
Present emitter when the transmission, make release opening mechanism with launch canister and gas holder intercommunication, high-pressure gas in the gas holder enters into the launch canister in, the spheroid in the launch canister is launched away, present emitter's release opening mechanism can not be very fast with launch canister and gas holder intercommunication, can not make the quick launch canister that enters into of high-pressure gas in the gas holder, cause the power of emitter transmission not enough, present emitter is heavier simultaneously, when to single use, be not convenient for carry.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the problems and provides a rupture disc individual unmanned aerial vehicle launching device which is characterized in that the periphery of a rupture disc is tensioned and fixedly connected with a launching tube, the rupture disc is opened instantly when a firing pin release opening mechanism punctures the rupture disc, meanwhile, a rotatable safety pin is arranged, when the rupture disc is not launched, a through hole in the safety pin is rotated to the side surface and does not correspond to the firing pin release opening mechanism, the rupture disc is prevented from being punctured by the firing pin release opening mechanism, when the rupture disc needs to be launched, the safety pin is rotated, the through hole in the safety pin corresponds to the firing pin release opening mechanism, and a firing pin of the firing pin release opening mechanism penetrates through the through hole to puncture the rupture disc.
In order to solve the problems, the technical scheme adopted by the utility model is as follows:
a rupture disk individual soldier unmanned aerial vehicle launching device comprises a gas storage tank and a launching barrel connected with the gas storage tank, wherein a rupture disk is arranged between the gas storage tank and the launching barrel, a firing pin release opening mechanism used for puncturing the rupture disk is arranged in the gas storage tank, a rotatable safety pin is arranged between the firing pin release opening mechanism and the rupture disk, the safety pin is located right ahead of the firing pin release opening mechanism, the upper end of the safety pin is connected with a handle which drives the safety pin to rotate, through holes are transversely arranged at corresponding positions on the safety pin, and the periphery of the rupture disk is tensioned and fixedly connected with the launching barrel.
And a sealing ring is arranged between the safety pin and the launching tube.
And an inflation valve is arranged on the air storage tank.
The gain effect of the utility model is:
the utility model discloses when using, through being tensioning and launching tube fixed connection around with the rupture disk, when firing pin release opening mechanism punctures the rupture disk, the rupture disk is opened in the twinkling of an eye, simultaneously through being provided with rotatable safety pin, when not launching, make the through-hole on the safety pin turn to the side, it is corresponding not giving firing pin release opening mechanism, prevent firing pin release opening mechanism to puncture the rupture disk, when needing the transmission, rotate the safety pin, make the through-hole on the safety pin corresponding with firing pin release opening mechanism, make firing pin release opening mechanism's firing pin pass the rupture disk that the through-hole punctures the rupture disk, even in the quick the entering of the high-pressure gas in the gas holder to the launching tube, the power of launcher transmission has been improved, simultaneously through the setting of safety pin, avoid the mistake to shoot, great improvement the security performance. The utility model has simple structure, reasonable design, light weight, small volume, convenient carrying, large launching power and high safety performance.
Drawings
Fig. 1 is a schematic structural view of the transportation and storage state of the present invention.
Fig. 2 is a structural schematic diagram of the inflated state of the present invention.
Fig. 3 is a schematic diagram of the transmitting state of the present invention.
Detailed Description
The following detailed description of embodiments of the utility model refers to the accompanying drawings.
Referring to fig. 1, 2 and 3, the numbering in the figures: 1 is a gas storage tank, 2 is a spring, 3 is a firing pin, 4 is a safety pin, 5 is a rupture disk, 6 is a positioning spring, 7 is a disposable sleeve, 8 is an inflation valve, 9 is a launching tube, 10 is an electromagnetic valve, 11 is a through hole I, 12 cylinder bodies, 13 is a through hole II and 14 is a needle rod.
The utility model relates to a burst disc individual soldier unmanned aerial vehicle launching device, which comprises a gas storage tank 1 and a launching tube 9 connected with the gas storage tank 1, wherein a burst disc 5 is arranged between the gas storage tank 1 and the launching tube 9, a firing pin release opening mechanism used for puncturing the burst disc 5 is arranged in the gas storage tank 1, the firing pin release opening mechanism comprises a cylinder body 12 arranged in the gas storage tank, a firing pin 3 arranged in the cylinder body 12 in a front-back sliding manner, and a disposable sleeve 7 arranged at the front end of the inner part of the cylinder body 12, a hole used for the front-back sliding of the firing pin is arranged in the middle of the disposable sleeve 7, a spring 2 is arranged between the rear end of the firing pin and the inner wall of the gas storage tank 1, the rear end of the spring 2 is fixedly connected with the inner wall of the cylinder body 12, the front end of the spring 2 is fixedly connected with the firing pin, the diameter of the hole used for the front-back sliding of the firing pin arranged in the middle of the disposable sleeve 7 is larger than the diameter of a needle rod of the firing pin, a through hole II 13 is transversely arranged in the middle of the firing pin, a positioning spring 6 is arranged in the through hole II 13, positioning balls are fixedly connected with two ends of the positioning spring 6, a circle of baffle ring is inwards arranged at two ends of the through hole II 13, the diameter of a middle hole of the baffle ring is smaller than that of the positioning ball, the diameter of the through hole II 13 is larger than that of the positioning ball, a circle of pit is arranged at a corresponding position on the inner wall of the cylinder body 12, the positioning spring 6 is in a compressed rotating state, a circle of concave ring is arranged on the outer wall of the disposable sleeve 7, an exhaust hole is arranged on the side wall of the front end of the cylinder body 12, an electromagnetic valve 10 is arranged on the exhaust hole, a gap is arranged between the side wall of the cylinder body 12, which is provided with the exhaust hole, and the outer wall of the disposable sleeve 7 at the corresponding position, a boss is arranged on the inner wall of the cylinder body 12 at the rear end of the disposable sleeve 7, the boss prevents the disposable sleeve 7 from moving backwards, and is arranged in a staggered manner, a gap is arranged between the side wall of the cylinder body 12 provided with the exhaust hole and the outer wall of the disposable sleeve 7 at the corresponding position, so that high-pressure gas in the gas storage tank 1 can enter the exhaust hole through the gap arranged between the side wall of the cylinder body 12 provided with the exhaust hole and the outer wall of the disposable sleeve 7 at the corresponding position and then is released through the exhaust hole. A rotatable safety pin 4 is arranged between the firing pin release opening mechanism and the rupture disk 5, the safety pin 4 is located right ahead of a firing pin 3 of the firing pin release opening mechanism, the upper end of the safety pin 4 is connected with a handle which drives the safety pin 4 to rotate, a first through hole 11 is transversely arranged at a corresponding position on the safety pin, the firing pin 3 penetrates through the safety pin 4 when the through hole 11 is fired, the rupture disk 5 is punctured, the periphery of the rupture disk 5 is tensioned, the periphery of the rupture disk 5 is fixedly connected with a firing tube 9, a sealing ring is arranged between the safety pin 4 and the firing tube 9, and an inflation valve 8 is installed on the gas storage tank.
The utility model discloses in the state of transportation, the location ball is located the pit of matching the card house in corresponding side, effectually avoid under the transportation effect, because under the effect of external force, make for firing pin 3 and add external force, make firing pin 3 mistake forward motion, pierce rupture disk 5, make launch canister and gas holder intercommunication, cause the mistake to penetrate, simultaneously when not launching, rotate safety pin 4, make through-hole 11 on the safety pin 4 stagger with firing pin 3, the safety pin is owing to blockking that the firing pin moves forward. When the firing is needed, the safety pin is rotated to enable the first through hole 11 on the safety pin 4 to be opposite to the firing pin 3, the gas storage tank 1 is inflated through the inflation valve 8 at this time, the high-pressure gas in the gas storage tank 1 firstly enters the disposable sleeve 7 and then enters the front end of the cylinder body 12 through a gap between a hole arranged in the middle of the disposable sleeve 7 and a needle rod of the firing pin 3, the high-pressure gas at the front end of the cylinder body 12 pushes the firing pin 3 to move backwards, the spring 2 at the rear end of the firing pin 3 is compressed, meanwhile, the gas pressure in the cylinder body 12 at the rear end of the firing pin 3 is compressed, when the gas pressure is compressed to a certain degree, the electromagnetic valve 10 at the front end of the cylinder body 12 is opened, so that the high-pressure gas in the cylinder body 12 at the front end of the firing pin enters the vent hole through a gap arranged between the side wall, provided with the vent hole, of the cylinder body 12 and the outer wall of the disposable sleeve 7 at the corresponding position, the vent hole is released, under the action of the elastic force of the spring 2 and the acting force of air pressure in a cylinder body 12 at the rear end of the firing pin 3, the firing pin 3 is pushed to move forwards, the firing pin 3 penetrates through the safety pin through a through hole I11 in the safety pin 4, the rupture disc 5 at the joint of the air storage tank 1 and the launching tube 9 is punctured, and the rupture disc 5 can be rapidly torn due to the fact that the periphery of the rupture disc is tensioned, so that the joint of the air storage tank 1 and the launching tube 9 is rapidly opened, high-pressure air in the air storage tank 9 rapidly enters the launching tube 9, and the launching power of the launching device is greatly provided; the utility model adopts the firing pin and the rupture disk, and integrates the gas storage tank and the launching tube into a whole, thereby greatly reducing the weight of the utility model and facilitating the carrying of the utility model when a single person fights.
The foregoing shows and describes the general principles, essential features, and advantages of the utility model. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are merely illustrative of the principles of the utility model, but that various changes and modifications may be made without departing from the spirit and scope of the utility model, which fall within the scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (3)
1. The utility model provides a rupture disc individual soldier unmanned aerial vehicle emitter which characterized in that: the high-speed explosive-proof launching device comprises an air storage tank and a launching tube connected with the air storage tank, wherein a rupture disc is arranged between the air storage tank and the launching tube, a firing pin release opening mechanism used for puncturing the rupture disc is arranged in the air storage tank, a rotatable safety pin is arranged between the firing pin release opening mechanism and the rupture disc, the safety pin is positioned right ahead of the firing pin release opening mechanism, the upper end of the safety pin is connected with a handle which drives the safety pin to rotate, through holes are transversely formed in the corresponding positions of the safety pin, and the periphery of the rupture disc is tensioned and fixedly connected with the launching tube.
2. The rupture disk individual soldier unmanned aerial vehicle launcher of claim 1, characterized in that: and a sealing ring is arranged between the safety pin and the launching tube.
3. The rupture disk individual soldier unmanned aerial vehicle launcher of claim 1, characterized in that: and an inflation valve is arranged on the air storage tank.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122929417.4U CN216546775U (en) | 2021-11-26 | 2021-11-26 | Blasting piece individual soldier unmanned aerial vehicle emitter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122929417.4U CN216546775U (en) | 2021-11-26 | 2021-11-26 | Blasting piece individual soldier unmanned aerial vehicle emitter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216546775U true CN216546775U (en) | 2022-05-17 |
Family
ID=81575911
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122929417.4U Active CN216546775U (en) | 2021-11-26 | 2021-11-26 | Blasting piece individual soldier unmanned aerial vehicle emitter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216546775U (en) |
-
2021
- 2021-11-26 CN CN202122929417.4U patent/CN216546775U/en active Active
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