CN110030886A - Artillery rocket propellant pours out device and artillery rocket resolving device automatically - Google Patents
Artillery rocket propellant pours out device and artillery rocket resolving device automatically Download PDFInfo
- Publication number
- CN110030886A CN110030886A CN201910428974.2A CN201910428974A CN110030886A CN 110030886 A CN110030886 A CN 110030886A CN 201910428974 A CN201910428974 A CN 201910428974A CN 110030886 A CN110030886 A CN 110030886A
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- China
- Prior art keywords
- supporting plate
- rocket
- artillery
- out device
- device automatically
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- 239000003380 propellant Substances 0.000 title claims abstract description 39
- 230000007246 mechanism Effects 0.000 claims abstract description 65
- 238000003825 pressing Methods 0.000 claims description 35
- 230000007306 turnover Effects 0.000 claims description 29
- 230000003028 elevating effect Effects 0.000 claims description 24
- 238000004064 recycling Methods 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims 1
- 230000008901 benefit Effects 0.000 abstract description 4
- 238000000354 decomposition reaction Methods 0.000 abstract description 4
- 238000000926 separation method Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 2
- 239000003814 drug Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 210000005069 ears Anatomy 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000036541 health Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/06—Dismantling fuzes, cartridges, projectiles, missiles, rockets or bombs
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Processing Of Solid Wastes (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of artillery rocket propellants to pour out device and artillery rocket resolving device automatically, belong to ammunition disposal technical field, it includes lathe bed, spindle box, rotation release mechanism and clamp system that artillery rocket propellant pours out device automatically, and spindle box and rotation release mechanism are connected by horizontal dislodgment feature with lathe bed；Rotation release mechanism is connected by spindle box with driving part, and clamp system is set to the opposite side of rotation release mechanism.The present invention clamps rocket projectile body by clamp system, while clamping the jet pipe of rocket projectile using rotation release mechanism and carrying out rotation to jet pipe by driving part and unloading, and can easily realize the separation of the body and jet pipe of rocket projectile；The artillery rocket resolving device for pouring out device automatically containing the artillery rocket propellant can be realized pipelining, and working efficiency is greatly improved.The present invention has the advantages that compact-sized, decomposition efficiency is high, can greatly reduce the labor intensity of operator, improves safety coefficient and the degree of automation.
Description
Technical field
The invention belongs to ammunition disposal technical fields more particularly to a kind of artillery rocket propellant to pour out device and fire automatically
Arrow shell resolving device.
Background technique
Scrapping artillery rocket propellant and pouring out is the important procedure for realizing that energetic material is isolated with the emptying of body inert material,
It is still within the manpower handwork stage at present.Since propellant has explosive characteristic, sensitivity is big, and there are poles for artificial emptying operation
Big security risk, easily generation safety accident, and manual operation, operation intensity is big, and operating efficiency is low, the long-term short distance of personnel
Propellant is contacted, toxic and harmful gas volatilization is unfavorable for operating personnel's occupational safety and health.
Summary of the invention
The object of the present invention is to provide a kind of artillery rocket propellants to pour out device and artillery rocket resolving device, purport automatically
It is manually poured out there are very big security risk and the big low efficiency of operation intensity solving propellant in above-mentioned body in the prior art
Technical problem.
In order to solve the above technical problems, the technical solution used in the present invention is:
A kind of artillery rocket propellant pours out device automatically, including rack, supporting plate, turnover mechanism and for clamping rocket projectile body
Clamp system, rocket projectile body is placed on supporting plate, and the clamp system and turnover mechanism are connected with rack；The supporting plate
It is set to the top of rack, one end of the supporting plate and frame top are rotatablely connected, and the turnover mechanism is set to the bottom of supporting plate
Portion；The side of the rack is equipped with the collecting part for recycling propellant, and the collecting part is set to rack and supporting plate phase
One end even；The turnover mechanism and clamp system are electrically connected with the control cabinet in Central Control Room.
Preferably, the clamp system includes the pressing plate for pressing rocket projectile body and the liter for driving pressing plate to go up and down
Descending mechanism, the pressing plate are set to the top of supporting plate；The pressing plate is set at the top of the movable end of elevating mechanism, the elevator
The movable end of structure runs through supporting plate, and the elevating mechanism is set to the lower section of supporting plate；The elevating mechanism is electrically connected with control cabinet.
Preferably, the elevating mechanism and turnover mechanism are cylinder or hydraulic cylinder；The lower surface of the supporting plate and tipper
The movable end of rotation connection at the top of the movable end of structure, the turnover mechanism runs through supporting plate, the cylinder body and rack of the turnover mechanism
Rotation connection.
Preferably, the supporting plate is equipped with a pair of of card slot for limiting to rocket projectile body, and two card slot intervals are arranged,
For being limited simultaneously to rocket projectile body front and rear part.
Preferably, the supporting plate is equipped with two pairs of card slots placed side by side, for two rocket projectile bullets placed side by side
Body limit；The pressing plate is set to the middle part of two pairs of card slots.
Preferably, the pressing plate is connected by rotating mechanism with the movable end of elevating mechanism, and the rotating mechanism includes rotation
Rotating motor and shaft, the pressing plate, which is fixed on, turns the tip of the axis, and the output shaft of the rotating electric machine is coaxially fixed with shaft, described
Rotating electric machine is fixed on the movable end of elevating mechanism；The rotating electric machine is electrically connected with control cabinet.
The present invention also provides a kind of artillery rocket resolving devices for pouring out device automatically containing above-mentioned artillery rocket propellant.
The beneficial effects of adopting the technical scheme are that compared with prior art, artillery rocket of the present invention pushes away
It pours out device automatically into agent and rocket projectile body is clamped on supporting plate by clamp system, while can be by rocket using turnover mechanism
It plays body to be tilted a certain angle, facilitates and propellant in body is poured onto the collecting part of side；It is pushed away containing the artillery rocket
The rocket projectile resolving device for pouring out device automatically into agent can be realized flow line production, and working efficiency is greatly improved.Present invention tool
Have the advantages that compact-sized, operating safety factor is high, staff can remotely be controlled in Central Control Room, it can be ensured that operation
The personal safety of personnel improves working efficiency and the degree of automation.
Detailed description of the invention
The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments.
Fig. 1 is the structural schematic diagram that a kind of artillery rocket propellant provided in an embodiment of the present invention pours out device automatically；
In figure: 1- rack, 2- supporting plate, 3- turnover mechanism, 4- rocket projectile body, 5- pressing plate, 6- elevating mechanism, 7- card slot, 8- branch
Fagging.
Specific embodiment
With reference to the attached drawing in the embodiment of the present invention, technical solution in the embodiment of the present invention carries out clear, complete
Ground description, it is clear that described embodiment is only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
A kind of artillery rocket propellant as shown in Figure 1 pours out device, including rack 1, supporting plate 2,3 and of turnover mechanism automatically
For clamping the clamp system of rocket projectile body 4, rocket projectile body 4 is placed on supporting plate 2, the clamp system and turnover mechanism
3 are connected with rack 1；The supporting plate 2 is set to the top of rack 1, is rotatablely connected at the top of one end of the supporting plate 2 and rack 1,
The turnover mechanism 3 is set to the bottom of supporting plate 2；The side of the rack 1 is equipped with the collecting part for recycling propellant, institute
It states collecting part and is set to one end that rack 1 is connected with supporting plate 2；The turnover mechanism 3 and clamp system are and in Central Control Room
Control cabinet electrical connection.Collecting part uses collecting box or conveyer belt, convenient recycling propellant in time.Rocket projectile body is placed on
On supporting plate, and clamp system firm grip is utilized, drives turnover mechanism that the intracorporal propellant of rocket projectile bullet is poured onto side
In collecting box or on conveyer belt, pouring out automatically for propellant is completed.Manual operation is replaced using the technical solution, operator exists
It can be operated in Central Control Room, ensure that the personal safety of staff, while also improving the degree of automation and working efficiency.
As a kind of optimal technical scheme, the clamp system includes pressing plate 5 for pressing rocket projectile body 4 and is used for
The elevating mechanism 6 for driving pressing plate 5 to go up and down, the pressing plate 5 are set to the top of supporting plate 2；The pressing plate 5 is set to elevating mechanism 6
Movable end at the top of, the movable end of the elevating mechanism 6 runs through supporting plate 2, and the elevating mechanism 6 is set to the lower section of supporting plate 2；Institute
Elevating mechanism 6 is stated to be electrically connected with control cabinet.Pressing plate is increased by elevating mechanism, when the rocket projectile bullet for having dismantled warhead and jet pipe
When body is placed on supporting plate, rocket projectile body can be pressed abd fixed on pressing plate by pressing plate with elevating mechanism whereabouts, facilitate rocket projectile bullet
Turnover falls propellant after body fixation.
In one particular embodiment of the present invention, the elevating mechanism 6 and turnover mechanism 3 are cylinder or hydraulic cylinder；Institute
It states and is rotatablely connected at the top of the lower surface of supporting plate 2 and the movable end of turnover mechanism 3, the movable end of the turnover mechanism 3 runs through supporting plate
2, the cylinder body and rack 1 of the turnover mechanism 3 are rotatablely connected.
Rocket projectile body is limited for convenience, the supporting plate 2 is equipped with one for limiting to rocket projectile body 4
To card slot 7, two interval of card slot 7 settings, for being limited simultaneously to 4 front and rear part of rocket projectile body.It is right simultaneously using two card slots
The front and rear part of rocket projectile body is fixed, and rocket projectile body is avoided to twist in switching process, guarantees the suitable of propellant
Benefit is toppled over.
In order to further increase working efficiency, the supporting plate 2 is equipped with two pairs of card slots 7 placed side by side, for two
Rocket projectile body 4 placed side by side limits；The pressing plate 5 is set to the middle part of two pairs of card slots 7.Two pairs of card slots are simultaneously to two fire
Arrow bullet body is limited, and fixed simultaneously using pressing plate both ends, can disposably be realized toppling over for two rocket projectile propellants, be mentioned
High working efficiency.
Wherein, gap, supporting plate are processed in the middle part of a piece trunnion axis of 8 one end of top support plate of rack 1 installation, the other end
2 both side ends are rotatedly connected by connection ears with trunnion axis, install support base, the work of turnover mechanism in the bottom surface of support plate
Stopper rod end and support base are rotatablely connected；The piston rod of turnover mechanism can move in the gap of supporting plate, realize the liter of supporting plate
Drop.It can guarantee stability of the supporting plate in switching process by this structure.
Above-mentioned technical proposal is advanced optimized, the pressing plate 5 is connected by rotating mechanism with the movable end of elevating mechanism 6,
The rotating mechanism includes rotating electric machine and shaft, and the pressing plate 5, which is fixed on, turns the tip of the axis, the output shaft of the rotating electric machine
It is coaxially fixed with shaft, the rotating electric machine is fixed on the movable end of elevating mechanism 6；The rotating electric machine is electrically connected with control cabinet
It connects.When toppling over propellant in rocket projectile body, pressing plate is rotated to vertical with rocket projectile body length direction, it is convenient while pressing
Firmly two rocket projectile bodies；After having toppled over propellant, pressing plate is rotated to consistent with rocket projectile body length direction, dress is facilitated
Unload rocket projectile.
The present invention also provides a kind of artillery rocket decomposition for pouring out device automatically containing above structure artillery rocket propellant
Equipment.All artillery rocket resolving devices for pouring out device automatically containing above structure artillery rocket propellant, in the present invention
Protection scope within.Artillery rocket resolving device includes two and drives conveyer belt by power mechanism, on two conveyer belts between
Every equipped with the pairs of card slot for support rocket projectile body；The support plate of rack is fixed on the piston rod end of lifting hydraulic cylinder,
Lifting hydraulic cylinder is fixed on pedestal by support frame, and pedestal is fixed by bolts on ground.When rocket projectile body is with defeated
When band being sent to be fed forward, the piston rod of lifting hydraulic cylinder bounces back, and drives rack and its pressing plate decline above, makes pressing plate and supporting plate
It is below conveyer belt；When rocket projectile body is run to the station of falling medicine, the piston rod of lifting hydraulic cylinder stretches out, supporting plate rise by
Card slot above it holds up rocket projectile body, and then pressing plate is increased and rotated to vertical with rocket projectile body, under rear fender
General who has surrendered's rocket projectile body is pressed in card slot and overturns, and facilitates the collecting part that propellant in rocket projectile body is poured onto side
It is interior.
In conclusion the present invention has the advantages that simple and compact for structure, easy to operate, rocket projectile can be greatly improved
Decomposition efficiency, borrowing the artillery rocket propellant and pouring out device automatically easily the propellant in rocket projectile to be poured out
Come, staff need to only carry out operating the decomposition that rocket projectile can be completed and medicine in Central Control Room, reduce the labor of operator
Fatigue resistance improves jet pipe rotation and unloads working efficiency, while improving the degree of automation of operating safety factor and equipment, conveniently pushes away
Wide application.
Many details are elaborated in the above description to facilitate a thorough understanding of the present invention, still the present invention can be with
Implemented using other than the one described here other way, those skilled in the art can be without prejudice to intension of the present invention
In the case of do similar popularization, therefore the present invention is not limited by particular embodiments disclosed above.
Claims (7)
1. a kind of artillery rocket propellant pours out device automatically, it is characterised in that: including rack, supporting plate, turnover mechanism and be used for
The clamp system of rocket projectile body is clamped, rocket projectile body is placed on supporting plate, and the clamp system and turnover mechanism are and machine
Frame is connected；The supporting plate is set to the top of rack, and one end of the supporting plate and frame top are rotatablely connected, the turnover mechanism
It is set to the bottom of supporting plate；The side of the rack is equipped with the collecting part for recycling propellant, the collecting part setting
In one end that rack is connected with supporting plate；The turnover mechanism and clamp system are electrically connected with the control cabinet in Central Control Room.
2. artillery rocket propellant according to claim 1 pours out device automatically, it is characterised in that: the clamp system packet
The pressing plate for pressing rocket projectile body and the elevating mechanism for driving pressing plate to go up and down are included, the pressing plate is set to the upper of supporting plate
Side；The pressing plate is set at the top of the movable end of elevating mechanism, and the movable end of the elevating mechanism runs through supporting plate, the elevator
Structure is set to the lower section of supporting plate；The elevating mechanism is electrically connected with control cabinet.
3. artillery rocket propellant according to claim 2 pours out device automatically, it is characterised in that: the elevating mechanism and
Turnover mechanism is cylinder or hydraulic cylinder；It is rotatablely connected at the top of the lower surface of the supporting plate and the movable end of turnover mechanism, it is described to turn over
The movable end of rotation mechanism runs through supporting plate, and the cylinder body of the turnover mechanism is connect with gantry rotation.
4. artillery rocket propellant according to claim 1 pours out device automatically, it is characterised in that: the supporting plate is equipped with
A pair of of card slot for being limited to rocket projectile body, two card slot interval settings, for the rocket projectile body front and rear part same time limit
Position.
5. artillery rocket propellant according to claim 4 pours out device automatically, it is characterised in that: the supporting plate is equipped with
Two pairs of card slots placed side by side, for being limited to two rocket projectile bodies placed side by side；The pressing plate is set to two pairs of card slots
Middle part.
6. artillery rocket propellant according to claim 2 pours out device automatically, it is characterised in that: the pressing plate passes through rotation
Rotation mechanism is connected with the movable end of elevating mechanism, and the rotating mechanism includes rotating electric machine and shaft, and the pressing plate, which is fixed on, to be turned
The output shaft of the tip of the axis, the rotating electric machine is coaxially fixed with shaft, and the rotating electric machine is fixed on the activity of elevating mechanism
End；The rotating electric machine is electrically connected with control cabinet.
7. containing the artillery rocket resolving device for pouring out device automatically such as any one of claim 1-6 artillery rocket propellant.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910428974.2A CN110030886B (en) | 2019-05-22 | 2019-05-22 | Rocket shell propellant automatic pouring device and rocket shell decomposing equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910428974.2A CN110030886B (en) | 2019-05-22 | 2019-05-22 | Rocket shell propellant automatic pouring device and rocket shell decomposing equipment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110030886A true CN110030886A (en) | 2019-07-19 |
| CN110030886B CN110030886B (en) | 2024-03-22 |
Family
ID=67243047
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910428974.2A Active CN110030886B (en) | 2019-05-22 | 2019-05-22 | Rocket shell propellant automatic pouring device and rocket shell decomposing equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110030886B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114383466A (en) * | 2022-01-27 | 2022-04-22 | 唐山市安航电子科技有限公司 | Automatic bird-repelling bullet control system |
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| DE19916751A1 (en) * | 1999-04-14 | 2000-10-19 | Fac Frank Abels Consult & Tech | Equipment for dismantling artillery and mortar ammunition filled with explosive material involves closed chamber in which is a rotary machine with rotatable clamp chuck for retention of ammunition |
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| Publication number | Priority date | Publication date | Assignee | Title |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN110030886B (en) | 2024-03-22 |
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