CN209961086U - Rocket shell warhead and rocket part separating device and rocket shell decomposing equipment - Google Patents
Rocket shell warhead and rocket part separating device and rocket shell decomposing equipment Download PDFInfo
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- CN209961086U CN209961086U CN201920740069.6U CN201920740069U CN209961086U CN 209961086 U CN209961086 U CN 209961086U CN 201920740069 U CN201920740069 U CN 201920740069U CN 209961086 U CN209961086 U CN 209961086U
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- rocket projectile
- rotary unloading
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Abstract
The utility model discloses a rocket shell warhead and rocket part separating device and a rocket shell decomposing device, belonging to the technical field of shell destruction, comprising a lathe bed, a rotary unloading mechanism and a clamping mechanism, wherein the rotary unloading mechanism is connected with the lathe bed through a horizontal shifting mechanism; the clamping mechanism is arranged on the opposite side of the rotary unloading mechanism, and an elastic receiving device is arranged between the rotary unloading mechanism and the clamping mechanism. The rocket projectile body is clamped through the clamping mechanism, the fighting part of the rocket projectile is clamped through the rotary unloading mechanism, the fighting part is rotatably unloaded through the driving part, the rocket projectile body and the fighting part can be easily separated, and the horizontal shifting mechanism is matched with the projectile receiving device to collect the rotatably unloaded fighting part; the rocket shell decomposing equipment containing the rocket shell warhead and rocket part separating device can realize flow line production, 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 shell is destroyed, especially, relate to a rocket shell warhead and rocket portion separator and rocket shell decomposition equipment.
Background
The rotary unloading separation of the warhead part and the rocket part of the scrapped rocket shell is an important process for disassembling and decomposing the scrapped rocket shell and is a necessary link for the subsequent classification treatment of filling emptying of the warhead part and emptying of a propellant of the rocket part. Because the separation of the warhead and the rocket is based on the decomposition of the full ammunition, the ammunition has heavy mass, long structure and large inherent binding force, and adopts manual rotary unloading, so that the device not only uses more personnel, has high operation strength and low operation efficiency, but also has the potential safety hazards of the rotary unloading and falling of the warhead, the occurrence of blasting accidents and the like.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a rocket shell warhead and rocket portion separator and rocket shell decomposition equipment aims at solving among the above-mentioned prior art artifical separation warhead and rocket portion intensity of labour big, the technical problem that work efficiency is low, the potential safety hazard is big.
In order to solve the technical problem, the utility model discloses the technical scheme who takes is:
a device for separating a rocket shell warhead from a rocket comprises a machine body, a rotary unloading mechanism for clamping the rocket shell warhead and a clamping mechanism for clamping a rocket shell body, wherein the rotary unloading mechanism is connected with the machine body through a horizontal displacement mechanism; the clamping mechanism is arranged on the opposite side of the rotary unloading mechanism, and an elastic receiving device is arranged between the rotary unloading mechanism and the clamping mechanism.
Preferably, the rotary unloading mechanism comprises a main shaft box, a chuck and a driving part, a clamping jaw for clamping a rocket projectile warhead is arranged on the front end face of the chuck, the rear part of the chuck is fixed on a horizontal main shaft, and the main shaft is connected with the driving part through the main shaft box; the spindle box is connected with the lathe bed through a horizontal displacement mechanism.
Preferably, the driving part is a hydraulic motor, the chuck is a hydraulic chuck, and the hydraulic chuck and the hydraulic motor are both connected with the hydraulic station.
Preferably, the horizontal displacement mechanism comprises a first telescopic part and a slide rail arranged on the lathe bed, and a slide block matched with the slide rail is arranged at the bottom of the spindle box; the movable end of the first telescopic part is connected with the rear part of the spindle box.
Preferably, the clamping mechanism comprises a bracket for supporting the rocket projectile body and a pressing plate for pressing the rocket projectile body, and the bracket is provided with a clamping groove for limiting the rocket projectile body; the pressing plate is arranged above the bracket and connected with the lifting mechanism.
Preferably, the lifting mechanism is an air cylinder or a hydraulic cylinder, and the pressing plate is arranged at the top of the movable end of the air cylinder or the hydraulic cylinder; the lifting mechanism is arranged below the bracket, and the movable end of the lifting mechanism penetrates through the bracket.
Preferably, the two pairs of clamping grooves are symmetrically arranged below two sides of the pressing plate; the rotary unloading mechanisms are two and respectively correspond to the two pairs of clamping grooves one by one.
Preferably, the bullet receiving device comprises a lifting platform, a lifting mechanism, a pushing mechanism and a conveyor, wherein the lifting platform is arranged between the rotary unloading mechanism and the clamping mechanism and correspondingly arranged below the rocket projectile warhead; the lifting platform is fixed at the top of the movable end of the lifting mechanism, and the lifting mechanism is arranged in the lathe bed; the pushing mechanism is arranged on the side face of the lifting platform, the conveyor is arranged in the machine body below the spindle box, and the warhead of the rocket projectile which is detached in a rotating mode is pushed to the conveying belt of the conveyor through the pushing mechanism.
Preferably, the pushing mechanism comprises a pushing plate and a second telescopic part, and the pushing plate and the conveying belt are respectively arranged on two sides of the lifting platform; the second telescopic part is arranged on the bed body, and the movable end of the second telescopic part is connected with the push plate.
The utility model also provides a rocket shell decomposition equipment that contains above-mentioned rocket shell warhead and rocket part separation device.
Adopt the produced beneficial effect of above-mentioned technical scheme to lie in: compared with the prior art, the rocket shell warhead and rocket head separating device clamps the rocket shell body through the clamping mechanism, simultaneously utilizes the rotary unloading mechanism to clamp the rocket shell warhead and carries out rotary unloading on the rocket shell warhead through the driving part, can easily realize the separation of the rocket shell body and the rocket shell warhead, and the horizontal shifting mechanism is matched with the rocket receiving device to collect the rotary unloaded warhead; the rocket shell decomposing equipment containing the rocket shell warhead and rocket part separating device can realize flow line production, 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.
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 a rocket shell warhead and rocket part separating device provided by the embodiment of the invention;
in the figure: 1-lathe bed, 2-main spindle box, 3-chuck, 4-driving part, 5-clamping jaw, 6-main spindle, 7-first telescopic part, 8-sliding rail, 9-sliding block, 10-pressing plate, 11-clamping groove, 12-lifting mechanism, 13-lifting table, 14-lifting mechanism, 15-conveying belt, 16-push plate, 17-second telescopic part and 18-bracket.
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 rocket shell warhead and rocket part separating device shown in figure 1 comprises a machine body 1, a rotary unloading mechanism for clamping the rocket shell warhead and a clamping mechanism for clamping a rocket shell body, wherein the rotary unloading mechanism is connected with the machine body 1 through a horizontal displacement mechanism; the clamping mechanism is arranged on the opposite side of the rotary unloading mechanism, and an elastic receiving device is arranged between the rotary unloading mechanism and the clamping mechanism. The rocket projectile body is firmly clamped through the clamping mechanism, the fighting part of the rocket projectile is clamped through the rotary unloading mechanism, the fighting part is easily and rotatably unloaded through the rotary unloading mechanism, the rocket projectile body is separated from the fighting part, and the fighting part which is rotatably unloaded is collected through the projectile receiving device. The technical scheme is utilized to replace manual operation, the labor intensity of operators is reduced, and the safety factor and the working efficiency are improved.
As a preferred structure, the rotary unloading mechanism comprises a main spindle box 2, a chuck 3 and a driving part 4, a clamping jaw 5 for clamping a rocket projectile warhead is arranged on the front end surface of the chuck 3, the rear part of the chuck 3 is fixed on a horizontal main spindle 6, and the main spindle 6 is connected with the driving part 4 through the main spindle box 2; the spindle box 2 is connected with the lathe bed 1 through a horizontal displacement mechanism. The driving part 4 is a hydraulic motor, the chuck 3 is a hydraulic chuck, and the hydraulic chuck and the hydraulic motor are both connected with a hydraulic station. Under the control of the hydraulic station, the hydraulic chuck clamps the warhead of the rocket projectile, so that the automation degree is further improved; the hydraulic motor drives the main shaft and the chuck to rotate, and the rotary unloading of the rocket projectile warhead is realized.
Wherein, the jack catch is the extension jack catch of three L shapes, and the long limit portion inboard of jack catch is the cambered surface with warhead external diameter complex, utilizes three extension jack catches can more firmly centre gripping rocket projectile's warhead.
As shown in fig. 1, in a preferred embodiment of the present invention, the horizontal shifting mechanism includes a first telescopic member 7 and a slide rail 8 disposed on the bed 1, and a slide block 9 engaged with the slide rail 8 is disposed at the bottom of the headstock 2; the movable end of the first telescopic part 7 is connected with the rear part of the main spindle box 2. After the rocket projectile is fixed through the clamping mechanism, under the action of the first telescopic part, the spindle box and the clamping jaws at the front end of the spindle box are pushed to be matched with the warhead, the warhead is tightly held under the action of the hydraulic chuck, the warhead can be rotationally detached along with the rotation of the hydraulic motor, the first telescopic part drives the spindle box to retreat, then the hydraulic chuck loosens the warhead, and the warhead which is rotationally detached is collected through the projectile receiving device.
In a preferred embodiment of the present invention, as shown in fig. 1, the clamping mechanism includes a bracket 18 for supporting the rocket projectile body and a pressing plate 10 for pressing the rocket projectile body, and a slot 11 for limiting the rocket projectile body is provided on the bracket 18; the pressing plate 10 is arranged above the bracket 18, and the pressing plate 10 is connected with the lifting mechanism 12. The rocket projectile is placed in the clamping groove, and the pressing plate presses the rocket projectile on the bracket under the action of the lifting mechanism.
The two pairs of clamping grooves 11 are symmetrically arranged below two sides of the pressing plate 10; the number of the rotary unloading mechanisms is two, and the rotary unloading mechanisms are respectively in one-to-one correspondence with the two pairs of clamping grooves 11. The utility model has the advantages of utilize this structure to carry out soon the warhead of two rocket projectiles and unload, can improve work efficiency. Corresponding to the structure, the pressing plate is connected with the movable end of the lifting mechanism through the rotating mechanism, the rotating mechanism comprises a rotating motor and a rotating shaft, the pressing plate is fixed at the upper 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. When the rocket projectile body is loaded and unloaded, the pressing plate is rotated to be consistent with the length direction of the rocket projectile body; in the process of rotating and disassembling the warhead, the pressing plate is rotated to be perpendicular to the rocket projectile bodies, and the two rocket projectile bodies are symmetrically arranged on two sides of the rotating shaft.
In a specific embodiment of the present invention, the lifting mechanism 12 is a cylinder or a hydraulic cylinder, and the pressing plate 10 is disposed on the top of the movable end of the cylinder or the hydraulic cylinder; the lifting mechanism 12 is arranged below the bracket 18, and the movable end of the lifting mechanism 12 penetrates through the bracket 18. The pressing plate can press and release the rocket projectile under the action of the lifting mechanism.
In a preferred embodiment of the present invention, as shown in fig. 1, the projectile receiving device includes a lifting platform 13, a lifting mechanism 14, a pushing mechanism and a conveyor, wherein the lifting platform 13 is disposed between the rotary unloading mechanism and the clamping mechanism and correspondingly disposed below the warhead of the rocket projectile; the lifting table 13 is fixed at the top of the movable end of the lifting mechanism 14, and the lifting mechanism 14 is arranged in the lathe bed 1; the pushing mechanism is arranged on the side surface of the lifting platform 13, and the conveyor is arranged in the lathe bed 1 below the spindle box 2. When the warhead is detached, the lifting platform rises to be in contact with the warhead, the clamping jaws are loosened, the detached warhead falls down along with the lifting platform, the lifting platform is pushed onto a conveying belt 15 of the conveyor through the pushing mechanism, and the warhead can be conveyed to the rear part and falls into a collecting box below along with the transmission of the conveying belt.
In a specific embodiment of the present invention, as shown in fig. 1, the pushing mechanism includes a pushing plate 16 and a second telescopic member 17, the pushing plate 16 and the conveying belt 15 are respectively disposed on two sides of the lifting platform 13; the second telescopic part 17 is arranged on the lathe bed 1, and the movable end of the second telescopic part 17 is connected with the push plate 16. Wherein, the flexible part of second is two, and the symmetry sets up in the both sides of elevating platform, and two flexible parts of second are contract simultaneously, can drive the push pedal and remove towards the conveyer belt to push away the warhead on the elevating platform to the conveyer belt.
The first telescopic component and the second telescopic component are cylinders or hydraulic cylinders, the hydraulic cylinders are connected with the hydraulic station, and the cylinders are connected with the air compressor.
The utility model also provides a rocket shell decomposing equipment containing the rocket shell warhead and rocket part separating device with the structure. All contain the rocket shell decomposition equipment that separates the device from rocket part and the rocket shell warhead of above-mentioned structure, all be in 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 supporting rocket projectile bodies are arranged on the two conveying belts at intervals. When the rocket projectile body is conveyed forwards along with the conveying belt, the bracket descends, and the pressing plate and the bracket are lower than the conveying belt; when the rocket projectile body moves to the rotary unloading station, the bracket rises to the clamping groove on the bracket to support the rocket projectile body, then the pressing plate rises and rotates to be vertical to the rocket projectile body, and then the pressing plate descends to compress the rocket projectile body in the clamping groove, so that the rocket projectile body is conveniently clamped and the warhead of the rocket projectile is quickly and rotatably unloaded.
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 warhead and rocket part from the device can easily unload rocket projectile's warhead fast soon, greatly reduced operating personnel's intensity of labour, improved rocket projectile's decomposition work efficiency, improved the degree of automation of factor of safety 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 (10)
1. A device for separating a rocket shell warhead from a rocket is characterized in that: the device comprises a lathe bed, a rotary unloading mechanism for clamping a warhead of a rotary unloading rocket projectile and a clamping mechanism for clamping a rocket projectile body, wherein the rotary unloading mechanism is connected with the lathe bed through a horizontal displacement mechanism; the clamping mechanism is arranged on the opposite side of the rotary unloading mechanism, and an elastic receiving device is arranged between the rotary unloading mechanism and the clamping mechanism.
2. A rocket projectile warhead and rocket portion detachment apparatus as recited in claim 1, wherein: the rotary unloading mechanism comprises a spindle box, a chuck and a driving part, wherein a clamping jaw for clamping a rocket projectile warhead is arranged on the front end surface of the chuck, the rear part of the chuck is fixed on a horizontal spindle, and the spindle is connected with the driving part through the spindle box; the spindle box is connected with the lathe bed through a horizontal displacement mechanism.
3. A rocket projectile warhead and rocket portion detachment apparatus as recited in claim 2, wherein: the driving part is a hydraulic motor, the chuck is a hydraulic chuck, and the hydraulic chuck and the hydraulic motor are both connected with the hydraulic station.
4. A rocket projectile warhead and rocket portion detachment apparatus as recited in claim 3, wherein: the horizontal displacement mechanism comprises a first telescopic part and a slide rail arranged on the lathe bed, and the bottom of the spindle box is provided with a slide block matched with the slide rail; the movable end of the first telescopic part is connected with the rear part of the spindle box.
5. A rocket projectile warhead and rocket portion detachment apparatus as recited in claim 1, wherein: the clamping mechanism comprises a bracket for bearing the rocket projectile body and a pressing plate for pressing the rocket projectile body, and a clamping groove for limiting the rocket projectile body is formed in the bracket; the pressing plate is arranged above the bracket and connected with the lifting mechanism.
6. A rocket projectile warhead and rocket portion detachment apparatus as recited in claim 5, wherein: the lifting mechanism is an air cylinder or a hydraulic cylinder, and the pressing plate is arranged at the top of the movable end of the air cylinder or the hydraulic cylinder; the lifting mechanism is arranged below the bracket, and the movable end of the lifting mechanism penetrates through the bracket.
7. A rocket projectile warhead and rocket portion detachment apparatus as recited in claim 5, wherein: the two pairs of clamping grooves are symmetrically arranged below two sides of the pressing plate; the rotary unloading mechanisms are two and respectively correspond to the two pairs of clamping grooves one by one.
8. A rocket projectile warhead and rocket portion detachment apparatus as recited in claim 1, wherein: the projectile receiving device comprises a lifting platform, a lifting mechanism, a pushing mechanism and a conveyor, wherein the lifting platform is arranged between the rotary unloading mechanism and the clamping mechanism and correspondingly arranged below the warhead of the rocket projectile; the lifting platform is fixed at the top of the movable end of the lifting mechanism; the pushing mechanism is arranged on the side face of the lifting platform, the conveyor is arranged in the machine body below the spindle box, and the warhead of the rocket projectile which is detached in a rotating mode is pushed to the conveying belt of the conveyor through the pushing mechanism.
9. A rocket projectile warhead and rocket portion detachment apparatus as recited in claim 8, wherein: the pushing mechanism comprises a pushing plate and a second telescopic part, and the pushing plate and the conveying belt are respectively arranged on two sides of the lifting platform; the second telescopic part is arranged on the bed body, and the movable end of the second telescopic part is connected with the push plate.
10. A rocket projectile decomposing device comprising means for detaching a rocket projectile part of the warhead from a rocket portion as claimed in any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920740069.6U CN209961086U (en) | 2019-05-22 | 2019-05-22 | Rocket shell warhead and rocket part separating device and rocket shell decomposing equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920740069.6U CN209961086U (en) | 2019-05-22 | 2019-05-22 | Rocket shell warhead and rocket part separating device and rocket shell decomposing equipment |
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| Publication Number | Publication Date |
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| CN209961086U true CN209961086U (en) | 2020-01-17 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201920740069.6U Active CN209961086U (en) | 2019-05-22 | 2019-05-22 | Rocket shell warhead and rocket part separating device and rocket shell decomposing equipment |
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| CN (1) | CN209961086U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110006297A (en) * | 2019-05-22 | 2019-07-12 | 中国人民解放军32181部队 | Artillery rocket warhead and rocket portion separator and artillery rocket resolving device |
-
2019
- 2019-05-22 CN CN201920740069.6U patent/CN209961086U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110006297A (en) * | 2019-05-22 | 2019-07-12 | 中国人民解放军32181部队 | Artillery rocket warhead and rocket portion separator and artillery rocket resolving device |
| CN110006297B (en) * | 2019-05-22 | 2023-10-13 | 中国人民解放军32181部队 | Rocket shell warhead and rocket part separating device and rocket shell decomposing equipment |
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