CN112484592B - Guided missile ammunition recovery device - Google Patents
Guided missile ammunition recovery device Download PDFInfo
- Publication number
- CN112484592B CN112484592B CN202011298164.9A CN202011298164A CN112484592B CN 112484592 B CN112484592 B CN 112484592B CN 202011298164 A CN202011298164 A CN 202011298164A CN 112484592 B CN112484592 B CN 112484592B
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- shot
- ammunition
- box
- recovery
- air
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- 238000011084 recovery Methods 0.000 title claims abstract description 64
- 238000007664 blowing Methods 0.000 claims abstract description 28
- 230000007246 mechanism Effects 0.000 claims abstract description 19
- 238000004064 recycling Methods 0.000 claims abstract description 19
- 229920000742 Cotton Polymers 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000010926 purge Methods 0.000 claims 1
- 230000006378 damage Effects 0.000 abstract 1
- 239000008188 pellet Substances 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- 238000001914 filtration Methods 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000006187 pill Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42D—BLASTING
- F42D5/00—Safety arrangements
- F42D5/04—Rendering explosive charges harmless, e.g. destroying ammunition; Rendering detonation of explosive charges harmless
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Elimination Of Static Electricity (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention provides a guided missile ammunition recovery device, which belongs to the technical field of scrapped ammunition destruction equipment and comprises a recovery box, an air blow pipe, an air compressor, a linear driver and a rotating mechanism, wherein the air blow pipe is arranged on the recovery box; the recycling box is provided with a feeding hole and an exhaust pipe; the projectile is placed on the recovery box, and an ammunition outlet of the projectile is communicated with the feeding hole; one end of the air blowing pipe penetrates through the feeding hole and is used for extending into the shot, and the other end of the air blowing pipe penetrates through the side wall of the recycling box and is positioned outside the recycling box; the air compressor is positioned outside the recovery box and connected with the other end of the air blowing pipe; the fixed end of the linear driver is fixedly arranged on the upper end surface of the recovery box; the rotating mechanism is positioned above the feed inlet; is fixedly arranged on the movable end of the linear driver; according to the guided missile ammunition recovery device provided by the invention, high-pressure air is blown into the inside of the shot to blow down ammunition adhered to the inner wall of the shot, the shot is rotated to different angles, and the ammunition adhered to different positions in the shot is blown and washed, so that the ammunition falls into the recovery box, and the ammunition recovery becomes simple and safe.
Description
Technical Field
The invention belongs to the technical field of scrapped ammunition destroying equipment, and particularly relates to a guided missile ammunition recovery device.
Background
In the process of manufacturing ammunition and destroying waste ammunition, various types of ammunition are required to be poured frequently. Because the ammunition is stored for a long time, the ammunition is easy to bond on the metal inner wall of the bullet, and the ammunition is stored and piled into blocks for a long time due to the self gravity, so that the ammunition bonded on the inner wall of the bullet is not easy to fall off. The difficulty of manual medicine pouring is high, certain risk still exists when the operation is improper, and once ignition occurs, the consequence is not imaginable.
Disclosure of Invention
The invention aims to provide a guided missile ammunition recovery device, and aims to solve the technical problems that manual cleaning of ammunition adhered to the inner wall of a projectile is difficult and certain risks exist in the prior art.
In order to achieve the purpose, the invention adopts the technical scheme that: there is provided a missile ammunition recovery device comprising:
the recycling box is provided with a feeding hole and an exhaust pipe; the shot is placed on the recovery box, and an ammunition outlet of the shot is communicated with the feed inlet;
one end of the air blowing pipe penetrates through the feeding hole and is used for extending into the shot, and the other end of the air blowing pipe penetrates through the side wall of the recovery box and is positioned outside the recovery box;
the air compressor is positioned outside the recovery box and connected with the other end of the air blowing pipe;
the fixed end of the linear driver is fixedly arranged on the upper end surface of the recycling box and is positioned on one side of the feeding hole;
the rotating mechanism is positioned above the feed inlet and is used for being connected with the shot and driving the shot to rotate; the rotating mechanism is fixedly arranged on the movable end of the linear driver
As another embodiment of the present application, the rotation mechanism includes:
the supporting plate is fixedly connected with the movable end of the linear driver, and a through hole for the shot to pass through is formed in the supporting plate;
the first gear is provided with a limiting hole for the shot to pass through and a locking piece for fixing the shot; the first gear is rotationally connected to the supporting plate;
the second gear is rotationally connected to the supporting plate and meshed with the first gear;
the driving motor is arranged on the supporting plate and is in transmission connection with the second gear;
as another embodiment of this application, the retaining member is locating pin or positioning bolt, be equipped with pinhole or screw on the first gear.
As another embodiment of the application, the inner side surface of the feeding hole is a conical surface which is used for being matched with the head of the shot.
As another embodiment of the application, an included angle is formed between a section of the air blowing pipe extending into the projectile and the central line of the projectile.
As another embodiment of this application, the collection box is equipped with the drainage plate that the slope set up, the drainage plate is located the feed inlet below for the ammunition that the ammunition export of guide from the shot flows out.
As another embodiment of this application, still be equipped with the relief valve on the collection box, be equipped with the flitch that gathers that the slope set up in the collection box, it is located to gather the flitch drainage plate below, and be located and keep away from one side of relief valve.
As another embodiment of the present application, the exhaust pipe is disposed on an upper end surface of the recycling bin, the exhaust pipe is a tapered pipe, and a cross section of the tapered pipe gradually increases from top to bottom; the air blowing pipe is obliquely arranged in the shot.
As another embodiment of this application, the top of blast pipe is equipped with the filter pulp.
The guided missile ammunition recovery device provided by the invention has the beneficial effects that: placing the shot on a rotating mechanism, starting a linear driver to enable an ammunition outlet of the shot to be communicated with a feeding hole of a recovery box, starting an air compressor, enabling high-pressure air to enter the shot through an air blowing pipe to blow off ammunition adhered to the inner wall of the shot and then fall into the recovery box; stopping the air compressor, starting the linear actuator, making the shot keep away from the recycling bin, the slewing mechanism drives the shot to rotate a certain angle, the restart linear actuator makes the ammunition export of shot communicate with each other with the feed inlet of recycling bin, starts the air compressor, and highly-compressed air gets into the inside ammunition with the inner wall of shot again and blows off to the recycling bin in. Blow in the shot through highly-compressed air inside, will paste the ammunition of falling at the shot inner wall, rotate the shot to different angles, will paste the ammunition at the inside different positions of shot and blast, make the ammunition fall into the collection box in, make the ammunition retrieve and become simple safety.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings required to be used in the embodiments or the prior art description will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings may be obtained according to these drawings without inventive labor.
Fig. 1 is a schematic structural diagram of a missile ammunition recovery device provided by the embodiment of the invention.
Wherein, in the figures, the respective reference numerals:
1. a recycling bin; 11. a feed inlet; 111. a conical surface; 12. an exhaust pipe; 121. filtering cotton; 13. a drainage plate; 14. a material gathering plate; 15. a discharge valve; 2. an air blowing pipe; 3. an air compressor; 4. a rotating mechanism; 41. a support plate; 42. a first gear; 43. a second gear; 44. a drive motor; 45. a locking member; 5. a linear actuator; 6. and (6) making pills.
Detailed Description
In order to make the technical problems, technical solutions and advantageous effects of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
It will be understood that when an element is referred to as being "secured to" or "disposed on" another element, it can be directly on the other element or be indirectly on the other element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or be indirectly connected to the other element.
It will be understood that the terms "length," "width," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like, as used herein, refer to an orientation or positional relationship indicated in the drawings, which is solely for the purpose of facilitating the description and simplifying the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and is therefore not to be construed as limiting the invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or to implicitly indicate the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
Referring to fig. 1, the missile ammunition recovery apparatus provided by the present invention will now be described. The guided missile ammunition recovery device comprises a recovery box 1, an air blow pipe 2, an air compressor 3, a linear driver 5 and a rotating mechanism 4; the recycling box 1 is provided with a feed inlet 11 and an exhaust pipe 12; the shot 6 is placed on the recovery box 1, and an ammunition outlet of the shot 6 is communicated with the feed inlet 11; one end of the air blowing pipe 2 penetrates through the feeding hole 11 and is used for extending into the shot 6, and the other end of the air blowing pipe penetrates through the side wall of the recycling box 1 and is positioned outside the recycling box 1; the air compressor 3 is positioned outside the recovery box 1 and is connected with the other end of the air blowing pipe 2; the fixed end of the linear driver 5 is fixedly arranged on the upper end surface of the recovery box 1 and is positioned on one side of the feed port 11; the rotating mechanism 4 is positioned above the feeding hole 11 and is used for connecting with the shot 6 and driving the shot 6 to rotate; the rotating mechanism 4 is fixedly arranged on the movable end of the linear driver 5.
Compared with the prior art, the guided missile ammunition recovery device provided by the invention has the advantages that the projectile 6 is placed on the rotating mechanism 4, the linear driver 5 is started to enable the ammunition outlet of the projectile 6 to be communicated with the feed inlet 11 of the recovery box 1, the air compressor 3 is started, and high-pressure air enters the projectile 6 through the air blowing pipe 2 to blow off the ammunition adhered to the inner wall of the projectile 6 and then falls into the recovery box 1; stopping air compressor machine 3, starting linear actuator 5, making 6 keeping away from collection box 1 of pellet, slewing mechanism 4 drive 6 certain angles of rotation of pellet, restart linear actuator 5 makes 6 ammunition export of pellet communicate with each other with the feed inlet 11 of collection box 1, start air compressor machine 3, high-pressure air gets into 6 insidely of pellet again and blows off the ammunition of inner wall to in collection box 1. Blow in 6 insides of shot through highly-compressed air, will paste the ammunition of 6 inner walls of shot and blow down, rotate 6 to different angles of shot, will paste the ammunition of 6 inside different positions of shot and blast, make the ammunition fall into collection box 1 in, make the ammunition retrieve and become simple safety.
Referring to fig. 1, as a specific embodiment of the missile ammunition recovery device provided by the present invention, the rotating mechanism 4 includes a support plate 41, a first gear 42, a second gear 43, and a driving motor 44; the support plate 41 is fixedly connected with the movable end of the linear driver 5, and a through hole for the bullet 6 to pass through is arranged on the support plate 41; the first gear 42 is provided with a limiting hole for the projectile 6 to pass through and a locking piece 45 for fixing the projectile 6; the first gear 42 is rotatably connected to the support plate 41; the second gear 43 is rotatably connected to the support plate 41 and meshed with the first gear 42; the driving motor 44 is arranged on the supporting plate 41 and is in transmission connection with the second gear 43; putting the shot 6 on the first gear 42 and locking, starting the linear driver 5, driving an ammunition outlet of the shot 6 to be communicated with the feeding hole 11 by the linear driver 5, starting the air compressor 3, and allowing high-pressure air to enter the shot 6 through the air blowing pipe 2 to blow off the ammunition on one side of the inner wall of the shot 6; starting the linear driver 5 to enable the shot 6 to be far away from the recycling box 1, starting the driving motor 44 to drive the second gear 43 to rotate, driving the shot 6 to rotate along with the rotation of the first gear 42 by a certain angle to stop, starting the linear driver 5 again, driving the ammunition outlet of the shot 6 to be communicated with the feeding hole 11 by the linear driver 5, starting the air compressor 3 again, enabling high-pressure air to enter the shot 6 to blow off ammunition on one side of the inner wall of the shot 6, and then enabling the high-pressure air to fall into the recycling box 1; repeating the steps, blowing all the ammunition adhered to the periphery of the inner wall of the projectile 6, and collecting the ammunition into the recovery box 1. The sleeve of the first gear wheel 42 is provided with a locking element 45, which locking element 45 locks the projectile 6 and rotates with the first gear wheel 42.
Referring to fig. 1, as a specific embodiment of the missile ammunition recovery device provided by the present invention, the locking member 45 is a positioning pin or a positioning bolt, and the first gear 42 is provided with a pin hole or a screw hole. The shot 6 is fixed through a positioning pin or a positioning bolt, the driving motor 44 is started, the driving motor 44 drives the second gear 43 to rotate, the second gear 43 drives the first gear 42 to rotate, and the shot 6 rotates along with the first gear 42.
Referring to fig. 1, as an embodiment of the missile ammunition recovery device provided by the present invention, the inner side surface of the feed port 11 is a conical surface 111 for fitting the head of the projectile 6. The pellets 6 are fitted with the tapered surface 111, ensuring that the pellets 6 are more stably placed on the feed port 11.
Referring to fig. 1, as a specific embodiment of the missile ammunition recovery device provided by the invention, an included angle is formed between a section of the gas blowing pipe 2 extending into the projectile 6 and the center line of the projectile 6. High-pressure air enters the inside of the shot 6 through the air blowing pipe 2, the air blowing pipe 2 is obliquely arranged, the high-pressure air is directly blown to one side of the inner wall of the shot 6, then the high-pressure air upwards reaches the top of the shot 6 along the inner wall of the shot 6 and then turns back, and ammunition adhered to the inner wall of the shot 6 is blown down through the side, directly blown by the high-pressure air, of the inside of the shot 6; the projectile 6 rotates for a certain angle and then is blown again, and after multiple times of blowing, ammunition bonded to the inner wall of the projectile 6 is blown down.
Referring to fig. 1, as a specific embodiment of the missile ammunition recovery device provided by the present invention, the recovery box 1 is provided with an obliquely arranged flow guide plate 13, and the flow guide plate 13 is located below the feed port 11 and is used for guiding the ammunition flowing out from the ammunition outlet of the projectile 6. The drainage plate 13 inclines to set up, and the ammunition that flows out leans on self gravity to pass through drainage plate 13 landing to gathering flitch 14, has avoided the ammunition to pile up at drainage plate 13. If the ammunition is excessively high accumulated on the flow guide plate 13, the effect of discharging the ammunition is affected
Referring to fig. 1, as a specific embodiment of the missile ammunition recovery device provided by the present invention, a discharge valve 15 is further disposed on the recovery box 1, an obliquely disposed material collecting plate 14 is disposed in the recovery box 1, and the material collecting plate 14 is located below the drainage plate 13 and on a side away from the discharge valve 15. On the ammunition that slides down from drainage plate 13 fell to gathering flitch 14, gather flitch 14 slope setting, the ammunition that falls to gathering flitch 14 leans on self gravity to slide gradually to the bottommost of collection box 1, and discharge valve 15 locates the collection box 1 bottommost, can make the ammunition of storage in collection box 1 discharge through discharge valve 15. The ammunition dropped on the gathering plate 14 gradually slides down to the discharge valve 15, avoiding long-term extrusion without discharge of the ammunition dropped on the gathering plate 14.
Referring to fig. 1, as a specific embodiment of the missile ammunition recovery device provided by the present invention, an exhaust pipe 12 is provided on an upper end surface of the recovery box 1, the exhaust pipe 12 is a tapered pipe, and a cross section of the tapered pipe gradually increases from top to bottom. High-pressure air discharged from the air compressor 3 enters the shot 6 through the air blowing pipe 2 to impact upwards, then the high-pressure air is discharged through a gap between the air blowing pipe 2 and an ammunition outlet, and then the high-pressure air is discharged out of the recycling box 1 through the exhaust pipe 12. The balance of the air pressure inside and outside the recycling box 1 is realized in the whole air intake and exhaust process. The exhaust pipe 12 is higher than the recovery tank 1, and when the high-pressure air goes upward through the exhaust pipe 12, the ammunition mixed in the high-pressure air is further precipitated into the recovery tank 1. The higher the exhaust pipe 12, the smaller the amount of ammunition mixed in the high-pressure air; the size of the top of the exhaust pipe 12 is smaller than that of the bottom, and the exhaust pipe is in a necking shape, so that more ammunitions are collided with the inner wall of the exhaust pipe 12 and subsided to the recovery box 1 in the ascending process of the ammunition mixed in high-pressure air, the content of the ammunition in the high-pressure air is reduced, and the influence on the external environment is reduced
Referring to fig. 1, as an embodiment of the missile ammunition recovery device provided by the present invention, a filter cotton 121 is disposed on the top of the exhaust pipe 12. High-pressure air discharged from the air compressor 3 enters the shot 6 through the blowpipe 2 and impacts upwards, then the high-pressure air is discharged through a gap between the blowpipe 2 and an ammunition outlet, and then the high-pressure air is discharged out of the recovery box 1 through the exhaust pipe 12. The balance of the air pressure inside and outside the recycling box 1 is realized in the whole air intake and exhaust process. The high pressure air discharged from the air compressor 3 is mixed with the ammunition after passing through the projectile 6, and the ammunition is gradually precipitated along with the flow of the high pressure air, but a small amount of ammunition still exists when the high pressure air is discharged through the exhaust pipe 12. The existence of the filter cotton 121 makes the ammunition in the high-pressure air be thoroughly separated from the high-pressure air, and the filter cotton 121 is replaced or cleaned after a certain time, so that the filtering effect is better.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (7)
1. A missile ammunition recovery device, comprising:
the recycling box is provided with a feeding hole and an exhaust pipe; the shot is placed on the recovery box, and an ammunition outlet of the shot is communicated with the feed inlet;
one end of the air blowing pipe penetrates through the feeding hole and is used for extending into the shot, the other end of the air blowing pipe penetrates through the side wall of the recovery box and is located outside the recovery box, an included angle is formed between one section of the air blowing pipe extending into the shot and the central line of the shot, high-pressure air enters the shot through the air blowing pipe, the air blowing pipe is obliquely arranged inside the shot, the high-pressure air is directly blown to one side of the inner wall of the shot, and then the high-pressure air upwards reaches the top of the shot along the inner wall of the shot and then turns back;
the air compressor is positioned outside the recovery box and connected with the other end of the air blowing pipe;
the fixed end of the linear driver is fixedly arranged on the upper end surface of the recovery box and is positioned on one side of the feed port;
the rotating mechanism is positioned above the feed inlet and is used for being connected with the shot and driving the shot to rotate; the rotating mechanism is fixedly arranged on the movable end of the linear driver and used for rotating the shot to different angles and purging ammunition stuck to different positions in the shot;
the exhaust pipe is arranged on the upper end surface of the recovery box and is a conical pipe, and the cross section of the conical pipe is gradually increased from top to bottom;
place the shot on slewing mechanism, start the ammunition export that linear actuator made the shot with the collection box the feed inlet communicates with each other, starts the air compressor machine, high-pressure air passes through the gas blow pipe enters into inside the shot and blows off and then fall into the ammunition of shot inner wall the collection box is internal, stops the air compressor machine starts linear actuator makes the shot keep away from the collection box, slewing mechanism drive shot rotates certain angle, restarts linear actuator makes the ammunition export of shot with the collection box the feed inlet communicates with each other, starts the air compressor machine, high-pressure air again get into inside the shot blow off the ammunition of inner wall extremely in the collection box, blow in the shot through high-pressure air, will paste the ammunition of shot inner wall and blow off, rotate shot to different angles, will paste the inside different positions of shot blow wash and go on, make the messenger fall into in the collection box.
2. The missile ammunition recovery device of claim 1, wherein the rotation mechanism comprises:
the supporting plate is fixedly connected with the movable end of the linear driver, and a through hole for the shot to pass through is formed in the supporting plate;
the first gear is provided with a limiting hole for the projectile to pass through and a locking piece for fixing the projectile; the first gear is rotationally connected to the supporting plate;
the second gear is rotationally connected to the supporting plate and meshed with the first gear;
and the driving motor is arranged on the supporting plate and is in transmission connection with the second gear.
3. The missile ammunition recovery device of claim 2, wherein the locking member is a positioning pin or a positioning bolt, and the first gear is provided with a pin hole or a screw hole.
4. The missile ammunition recovery device of claim 1, wherein the inner side surface of the feed port is a conical surface adapted to the head of the projectile.
5. The missile ammunition recovery device of claim 1, wherein the recovery box is provided with an obliquely arranged flow guide plate which is positioned below the feed port and is used for guiding the ammunition flowing out of the ammunition outlet of the projectiles.
6. The missile ammunition recovery device of claim 5, wherein the recovery box is further provided with a discharge valve, and an obliquely arranged material gathering plate is arranged in the recovery box and is positioned below the drainage plate and on the side far away from the discharge valve.
7. The missile ammunition recovery device of claim 1, wherein the top of the exhaust pipe is provided with filter cotton.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011298164.9A CN112484592B (en) | 2020-11-18 | 2020-11-18 | Guided missile ammunition recovery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011298164.9A CN112484592B (en) | 2020-11-18 | 2020-11-18 | Guided missile ammunition recovery device |
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| Publication Number | Publication Date |
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| CN112484592A CN112484592A (en) | 2021-03-12 |
| CN112484592B true CN112484592B (en) | 2023-01-13 |
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| CN202011298164.9A Active CN112484592B (en) | 2020-11-18 | 2020-11-18 | Guided missile ammunition recovery device |
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| WO1999034165A1 (en) * | 1997-12-17 | 1999-07-08 | Jansson Claes Haakan | A method and a device for destroying military explosives |
| CN106091855A (en) * | 2016-06-21 | 2016-11-09 | 中国人民解放军军械工程学院 | A kind of bullet explosive emptier and turned letter method |
| CN109084644A (en) * | 2018-08-30 | 2018-12-25 | 中国兵器装备集团自动化研究所 | A kind of energetic material automatic emptying device and its operating method |
| CN110411290A (en) * | 2019-08-28 | 2019-11-05 | 西安近代化学研究所 | It is a kind of for emptying the cavitation spray head of Charge of ammunitions |
| CN110425201A (en) * | 2019-07-11 | 2019-11-08 | 广东宏大民爆集团有限公司 | A kind of blasting agent mixing vehicle safe locking device and method |
| CN110879021A (en) * | 2019-12-19 | 2020-03-13 | 中国人民解放军陆军工程大学 | Shell decomposition line and decomposition method thereof |
| CN211291207U (en) * | 2019-12-19 | 2020-08-18 | 中国人民解放军32181部队 | Shell decomposes and dials bullet device of pouring medicine |
| CN111551083A (en) * | 2020-05-15 | 2020-08-18 | 刘凤江 | Rotatory ammunition equipment of wasing of high-pressure squirt |
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2020
- 2020-11-18 CN CN202011298164.9A patent/CN112484592B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999034165A1 (en) * | 1997-12-17 | 1999-07-08 | Jansson Claes Haakan | A method and a device for destroying military explosives |
| CN106091855A (en) * | 2016-06-21 | 2016-11-09 | 中国人民解放军军械工程学院 | A kind of bullet explosive emptier and turned letter method |
| CN109084644A (en) * | 2018-08-30 | 2018-12-25 | 中国兵器装备集团自动化研究所 | A kind of energetic material automatic emptying device and its operating method |
| CN110425201A (en) * | 2019-07-11 | 2019-11-08 | 广东宏大民爆集团有限公司 | A kind of blasting agent mixing vehicle safe locking device and method |
| CN110411290A (en) * | 2019-08-28 | 2019-11-05 | 西安近代化学研究所 | It is a kind of for emptying the cavitation spray head of Charge of ammunitions |
| CN110879021A (en) * | 2019-12-19 | 2020-03-13 | 中国人民解放军陆军工程大学 | Shell decomposition line and decomposition method thereof |
| CN211291207U (en) * | 2019-12-19 | 2020-08-18 | 中国人民解放军32181部队 | Shell decomposes and dials bullet device of pouring medicine |
| CN111551083A (en) * | 2020-05-15 | 2020-08-18 | 刘凤江 | Rotatory ammunition equipment of wasing of high-pressure squirt |
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| CN112484592A (en) | 2021-03-12 |
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