CN209978741U - Automatic rocket projectile propellant pouring device and rocket projectile decomposing equipment - Google Patents
Automatic rocket projectile propellant pouring device and rocket projectile decomposing equipment Download PDFInfo
- Publication number
- CN209978741U CN209978741U CN201920740054.XU CN201920740054U CN209978741U CN 209978741 U CN209978741 U CN 209978741U CN 201920740054 U CN201920740054 U CN 201920740054U CN 209978741 U CN209978741 U CN 209978741U
- Authority
- CN
- China
- Prior art keywords
- rocket projectile
- supporting plate
- rocket
- propellant
- clamping
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Abstract
The utility model discloses a rocket shell propellant automatic pouring device and rocket shell decomposition equipment, belonging to the technical field of ammunition destruction, wherein the rocket shell propellant automatic pouring device comprises a lathe bed, a main shaft box, a rotary unloading mechanism and a clamping mechanism, wherein the main shaft box and the rotary unloading mechanism are connected with the lathe bed through a horizontal shifting mechanism; the rotary unloading mechanism is connected with the driving part through the spindle box, and the clamping mechanism is arranged on the opposite side of the rotary unloading mechanism. The utility model clamps the rocket projectile body through the clamping mechanism, and simultaneously clamps the spray pipe of the rocket projectile through the rotary unloading mechanism and carries out rotary unloading on the spray pipe through the driving part, thus the separation of the rocket projectile body and the spray pipe can be easily realized; the rocket projectile decomposing equipment containing the automatic rocket projectile propellant pouring device can realize assembly line operation, and greatly improves the working efficiency. The utility model has the advantages of compact structure, decomposition efficiency are high, can greatly reduce operating personnel's intensity of labour, improve factor of safety and degree of automation.
Description
Technical Field
The utility model belongs to the technical field of the ammunition is destroyed, especially, relate to an automatic device and rocket shell decomposition equipment of pouring out of rocket shell propellant.
Background
The dumping of the propellant of the scrapped rocket projectile is an important process for realizing the emptying separation of energetic materials and projectile inert materials, and is still in the manual operation stage at present. Because the propellant has the characteristics of explosion and explosion, the sensitivity is high, great potential safety hazards exist in manual emptying operation, safety accidents are easy to happen, manual operation is high in operation intensity and low in operation efficiency, personnel can contact the propellant in a short distance for a long time, toxic and harmful gases volatilize, and the occupational safety and health of the operating personnel are not facilitated.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an automatic device and rocket shell decomposition equipment of pouring of rocket shell propellant aims at solving among the above-mentioned prior art the artifical technical problem who pours the existence very big potential safety hazard of propellant in the shell, and the operating strength inefficiency greatly.
In order to solve the technical problem, the utility model discloses the technical scheme who takes is:
a rocket projectile propellant automatic pouring device comprises a machine frame, a supporting plate, a turnover mechanism and a clamping mechanism for clamping rocket projectile bodies, wherein the rocket projectile bodies are placed on the supporting plate, and the clamping mechanism and the turnover mechanism are connected with the machine frame; the supporting plate is arranged at the top of the rack, one end of the supporting plate is rotatably connected with the top of the rack, and the turnover mechanism is arranged at the bottom of the supporting plate; a collecting component for recovering the propellant is arranged on one side of the rack and is arranged at one end, connected with the supporting plate, of the rack; the turnover mechanism and the clamping mechanism are electrically connected with a control cabinet in the central control room.
Preferably, the clamping mechanism comprises a pressing plate for pressing the rocket projectile body and a lifting mechanism for driving the pressing plate to lift, and the pressing plate is arranged above the supporting plate; the pressing plate is arranged at the top of the movable end of the lifting mechanism, the movable end of the lifting mechanism penetrates through the supporting plate, and the lifting mechanism is arranged below the supporting plate; the lifting mechanism is electrically connected with the control cabinet.
Preferably, the lifting mechanism and the turnover mechanism are air cylinders or hydraulic cylinders; the lower surface of the supporting plate is rotatably connected with the top of the movable end of the turnover mechanism, the movable end of the turnover mechanism penetrates through the supporting plate, and the cylinder body of the turnover mechanism is rotatably connected with the rack.
Preferably, be equipped with on the layer board and be used for spacing a pair of draw-in groove to the rocket projectile body, two draw-in grooves interval sets up for it is spacing simultaneously to rocket projectile body front and back portion.
Preferably, two pairs of clamping grooves which are arranged in parallel are arranged on the supporting plate and used for limiting two rocket projectile bodies which are arranged in parallel; the pressing plate is arranged in the middle of the two pairs of clamping grooves.
Preferably, the pressing plate is connected with the movable end of the lifting mechanism through a rotating mechanism, the rotating mechanism comprises a rotating motor and a rotating shaft, the pressing plate is fixed at the tail end of the rotating shaft, an output shaft of the rotating motor is coaxially fixed with the rotating shaft, and the rotating motor is fixed at the movable end of the lifting mechanism; the rotating motor is electrically connected with the control cabinet.
The utility model also provides a rocket shell decomposition equipment who contains the automatic device of pouring out of above-mentioned rocket shell propellant.
Adopt the produced beneficial effect of above-mentioned technical scheme to lie in: compared with the prior art, the automatic pouring device for the rocket projectile propellant clamps the rocket projectile body on the supporting plate through the clamping mechanism, and meanwhile, the rocket projectile body can be inclined by a certain angle by utilizing the turnover mechanism, so that the propellant in the projectile body can be conveniently poured into a collecting part on one side; the rocket projectile decomposition equipment comprising the rocket projectile propellant automatic pouring device can realize assembly line production, and greatly improves the working efficiency. The utility model has the advantages of compact structure, work factor of safety are high, and the staff can carry out remote control in the central control room, can ensure operating personnel's personal safety, improve work efficiency and degree of automation.
Drawings
The present invention will be described in further detail with reference to the accompanying drawings and specific embodiments.
FIG. 1 is a schematic structural view of an automatic rocket projectile propellant pouring device according to an embodiment of the present invention;
in the figure: 1-a frame, 2-a supporting plate, 3-a turnover mechanism, 4-a rocket projectile body, 5-a pressing plate, 6-a lifting mechanism, 7-a clamping groove and 8-a supporting plate.
Detailed Description
The technical solutions in the embodiments of the present invention are clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
The automatic rocket projectile propellant pouring device shown in fig. 1 comprises a frame 1, a supporting plate 2, a turnover mechanism 3 and a clamping mechanism for clamping a rocket projectile body 4, wherein the rocket projectile body 4 is placed on the supporting plate 2, and the clamping mechanism and the turnover mechanism 3 are both connected with the frame 1; the supporting plate 2 is arranged at the top of the rack 1, one end of the supporting plate 2 is rotatably connected with the top of the rack 1, and the turnover mechanism 3 is arranged at the bottom of the supporting plate 2; a collecting component for recovering the propellant is arranged on one side of the machine frame 1, and the collecting component is arranged at one end of the machine frame 1 connected with the supporting plate 2; the turnover mechanism 3 and the clamping mechanism are electrically connected with a control cabinet in the central control room. The collecting component adopts a collecting box or a conveying belt, so that the propellant can be conveniently and timely recovered. The rocket projectile body is placed on the supporting plate and is firmly clamped by the clamping mechanism, the propelling agent in the rocket projectile body is poured into the collecting box or the conveying belt on one side by the driving turnover mechanism, and the propelling agent is automatically poured out. Utilize this technical scheme to replace manual operation, operating personnel can be operated promptly in the central control room, has guaranteed staff's personal safety, has also improved degree of automation and work efficiency simultaneously.
As a preferable technical solution, the clamping mechanism comprises a pressing plate 5 for pressing the rocket projectile body 4 and a lifting mechanism 6 for driving the pressing plate 5 to lift, wherein the pressing plate 5 is arranged above the supporting plate 2; the pressing plate 5 is arranged at the top of the movable end of the lifting mechanism 6, the movable end of the lifting mechanism 6 penetrates through the supporting plate 2, and the lifting mechanism 6 is arranged below the supporting plate 2; the lifting mechanism 6 is electrically connected with the control cabinet. The clamp plate passes through elevating system and risees, and when the rocket projectile body that has dismantled warhead and spray tube was arranged in on the layer board, the clamp plate can compress tightly the rocket projectile body along with elevating system whereabouts and fix on the clamp plate, makes things convenient for the fixed upset of rocket projectile body to empty the propellant after firm.
In a specific embodiment of the present invention, the lifting mechanism 6 and the turning mechanism 3 are cylinders or hydraulic cylinders; the lower surface of the supporting plate 2 is rotatably connected with the top of the movable end of the turnover mechanism 3, the movable end of the turnover mechanism 3 penetrates through the supporting plate 2, and the cylinder body of the turnover mechanism 3 is rotatably connected with the rack 1.
In order to conveniently carry out spacingly to the rocket projectile body, be equipped with on layer board 2 and be used for a pair of draw-in groove 7 spacing to rocket projectile body 4, two draw-in grooves 7 interval settings are used for spacing simultaneously to rocket projectile body 4 front and back portion. Utilize two draw-in grooves to fix the front and back portion of rocket projectile body simultaneously, avoid rocket projectile body to take place to twist reverse at the upset in-process, guarantee empting smoothly of propellant.
In order to further improve the working efficiency, two pairs of clamping grooves 7 which are arranged in parallel are arranged on the supporting plate 2 and used for limiting the two rocket projectile bodies 4 which are arranged in parallel; the pressing plate 5 is arranged in the middle of the two pairs of clamping grooves 7. Two pairs of draw-in grooves carry on spacingly to two rocket projectile bodies simultaneously to utilize the clamp plate both ends to fix simultaneously, can once only realize empting of two rocket projectile propellants, improved work efficiency.
Wherein, a horizontal shaft is arranged at one end of a top supporting plate 8 of the frame 1, a notch is processed at the middle part of the other end, the end parts at two sides of the supporting plate 2 are rotationally connected with the horizontal shaft through two connecting lugs, a supporting seat is arranged at the bottom surface of the supporting plate, and the end part of a piston rod of the turnover mechanism is rotationally connected with the supporting seat; the piston rod of the turnover mechanism can move in the opening of the supporting plate, so that the supporting plate can be lifted. The stability of the supporting plate in the overturning process can be ensured by the structure.
Further optimizing the technical scheme, the pressing plate 5 is connected with the movable end of the lifting mechanism 6 through a rotating mechanism, the rotating mechanism comprises a rotating motor and a rotating shaft, the pressing plate 5 is fixed at the tail end of the rotating shaft, an output shaft of the rotating motor is coaxially fixed with the rotating shaft, and the rotating motor is fixed at the movable end of the lifting mechanism 6; the rotating motor is electrically connected with the control cabinet. When the propellant in the rocket projectile body is poured, the pressing plate is rotated to be vertical to the length direction of the rocket projectile body, so that two rocket projectile bodies can be conveniently and simultaneously pressed; after the propellant is poured, the pressing plate is rotated to be consistent with the length direction of the rocket projectile body, so that the rocket projectile is convenient to load and unload.
The utility model also provides a rocket shell decomposition equipment who contains the automatic device of pouring of above-mentioned structure rocket shell propellant. All rocket projectile decomposing equipment containing the rocket projectile propellant automatic pouring device with the structure is within the protection scope of the utility model. The rocket projectile decomposing equipment comprises two conveying belts driven by a power mechanism, and paired clamping grooves for bearing rocket projectile bodies are arranged on the two conveying belts at intervals; the support plate of frame is fixed in hydraulic cylinder's piston rod tip, and hydraulic cylinder is fixed in on the base through the support frame, and the base passes through the bolt fastening subaerial. When the rocket projectile body is conveyed forwards along with the conveying belt, the piston rod of the lifting hydraulic cylinder retracts to drive the rack and the pressing plate on the rack to descend, so that the pressing plate and the supporting plate are lower than the conveying belt; when the rocket projectile body moves to the station of falling the medicine, hydraulic cylinder's piston rod stretches out, and the layer board rises to hold up the rocket projectile body with the help of the draw-in groove above it, and the clamp plate risees and rotates to perpendicular with the rocket projectile body after that, and the clamp plate descends to compress tightly the rocket projectile body in the draw-in groove and upset afterwards, conveniently emptys the collection part of rocket projectile body internal propellant to the side in.
To sum up, the utility model has the advantages of simple structure is compact, convenient operation is swift, can improve rocket projectile's decomposition efficiency greatly, borrow this rocket shell propellant automatic pouring device can easily empty out the propellant in the rocket projectile, the staff only needs to operate in the central control room and can accomplish rocket projectile's decomposition and pouring medicine, has reduced operating personnel's intensity of labour, has improved the spray tube and has unloaded work efficiency soon, has improved the degree of automation of work safety factor and equipment simultaneously, convenient popularization and application.
In the above description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, but the present invention may be implemented in other ways different from the one described herein, and those skilled in the art may similarly generalize the present invention without departing from the spirit of the present invention, and therefore the present invention is not limited to the specific embodiments disclosed above.
Claims (7)
1. A rocket shell propellant automatic pouring device is characterized in that: the rocket projectile body clamping device comprises a rack, a supporting plate, a turnover mechanism and a clamping mechanism for clamping the rocket projectile body, wherein the rocket projectile body is placed on the supporting plate, and the clamping mechanism and the turnover mechanism are both connected with the rack; the supporting plate is arranged at the top of the rack, one end of the supporting plate is rotatably connected with the top of the rack, and the turnover mechanism is arranged at the bottom of the supporting plate; a collecting component for recovering the propellant is arranged on one side of the rack and is arranged at one end, connected with the supporting plate, of the rack; the turnover mechanism and the clamping mechanism are electrically connected with a control cabinet in the central control room.
2. A rocket projectile propellant automatic dumping apparatus as claimed in claim 1, wherein: the clamping mechanism comprises a pressing plate for pressing the rocket projectile body and a lifting mechanism for driving the pressing plate to lift, and the pressing plate is arranged above the supporting plate; the pressing plate is arranged at the top of the movable end of the lifting mechanism, the movable end of the lifting mechanism penetrates through the supporting plate, and the lifting mechanism is arranged below the supporting plate; the lifting mechanism is electrically connected with the control cabinet.
3. A rocket projectile propellant automatic dumping apparatus as claimed in claim 2, wherein: the lifting mechanism and the turnover mechanism are cylinders or hydraulic cylinders; the lower surface of the supporting plate is rotatably connected with the top of the movable end of the turnover mechanism, the movable end of the turnover mechanism penetrates through the supporting plate, and the cylinder body of the turnover mechanism is rotatably connected with the rack.
4. A rocket projectile propellant automatic dumping apparatus as claimed in claim 2, wherein: the supporting plate is provided with a pair of clamping grooves used for limiting the rocket projectile bodies, and the two clamping grooves are arranged at intervals and used for limiting the front and the rear of the rocket projectile bodies.
5. A rocket projectile propellant automatic dumping apparatus as claimed in claim 4, wherein: two pairs of clamping grooves which are arranged in parallel are arranged on the supporting plate and used for limiting two rocket projectile bodies which are arranged in parallel; the pressing plate is arranged in the middle of the two pairs of clamping grooves.
6. A rocket projectile propellant automatic dumping apparatus as claimed in claim 2, wherein: the pressing plate is connected with the movable end of the lifting mechanism through a rotating mechanism, the rotating mechanism comprises a rotating motor and a rotating shaft, the pressing plate is fixed at the tail end of the rotating shaft, an output shaft of the rotating motor is coaxially fixed with the rotating shaft, and the rotating motor is fixed at the movable end of the lifting mechanism; the rotating motor is electrically connected with the control cabinet.
7. A rocket projectile decomposing device including a rocket projectile propellant automatic dumping apparatus as claimed in any one of claims 1 to 6.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920740054.XU CN209978741U (en) | 2019-05-22 | 2019-05-22 | Automatic rocket projectile propellant pouring device and rocket projectile decomposing equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920740054.XU CN209978741U (en) | 2019-05-22 | 2019-05-22 | Automatic rocket projectile propellant pouring device and rocket projectile decomposing equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209978741U true CN209978741U (en) | 2020-01-21 |
Family
ID=69263520
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920740054.XU Active CN209978741U (en) | 2019-05-22 | 2019-05-22 | Automatic rocket projectile propellant pouring device and rocket projectile decomposing equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209978741U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110030886A (en) * | 2019-05-22 | 2019-07-19 | 中国人民解放军32181部队 | Artillery rocket propellant pours out device and artillery rocket resolving device automatically |
| CN111908377A (en) * | 2020-07-06 | 2020-11-10 | 中交武汉港湾工程设计研究院有限公司 | Heavy construction quick assembling and disassembling structure and manufacturing method thereof |
-
2019
- 2019-05-22 CN CN201920740054.XU patent/CN209978741U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110030886A (en) * | 2019-05-22 | 2019-07-19 | 中国人民解放军32181部队 | Artillery rocket propellant pours out device and artillery rocket resolving device automatically |
| CN110030886B (en) * | 2019-05-22 | 2024-03-22 | 中国人民解放军32181部队 | Rocket shell propellant automatic pouring device and rocket shell decomposing equipment |
| CN111908377A (en) * | 2020-07-06 | 2020-11-10 | 中交武汉港湾工程设计研究院有限公司 | Heavy construction quick assembling and disassembling structure and manufacturing method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209978741U (en) | Automatic rocket projectile propellant pouring device and rocket projectile decomposing equipment | |
| CN105905624A (en) | Coarse barium slag dumping overturning platform device | |
| CN106115288A (en) | Thick barium based on toggle is slagged tap roll-over table | |
| CN107877127A (en) | Roller washing machine bearing oil seal pressing all-in-one | |
| CN109261883A (en) | A kind of high performance alloys rod iron continuous forging device | |
| CN110006298B (en) | Automatic decomposing line for rocket shell | |
| CN206142466U (en) | Support of transport material | |
| CN209978740U (en) | Rocket shell automation decomposition line | |
| CN110030886B (en) | Rocket shell propellant automatic pouring device and rocket shell decomposing equipment | |
| CN207986067U (en) | Flat horizontal surface workpiece turning conveying device | |
| CN206689545U (en) | A kind of lightweight cutting workpiece machine | |
| CN210498440U (en) | Slewing bearing oilhole processing positioner | |
| CN209961086U (en) | Rocket shell warhead and rocket part separating device and rocket shell decomposing equipment | |
| CN208037929U (en) | Carry elevator | |
| CN102502252A (en) | Turning carrying device for workpieces | |
| CN212778924U (en) | Grenade decomposition device | |
| CN209927008U (en) | Automatic rotary unloading device for rocket projectile nozzle and rocket projectile decomposition equipment | |
| CN208304819U (en) | The 3D device of falling ball that can be used on roller-way conveying shot-blasting machine | |
| CN2732765Y (en) | Current conducting rod drawing machine for electrolysis | |
| CN213037293U (en) | Paper case assembling equipment for detonating tool | |
| CN207496112U (en) | A kind of packaging bag double-pole cutter device | |
| CN206750974U (en) | Edible mushroom bacterium bag unloading recovery automatic charging machine | |
| CN218855161U (en) | Waste material compression device is used in hardware fitting processing | |
| CN218696446U (en) | Cutting and blanking integrated machine for high-frequency welded steel pipes | |
| CN204817482U (en) | Tubular product automatic discharging frame |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |