CN210549451U - Flexible general installation mechanism of solid rocket projectile - Google Patents
Flexible general installation mechanism of solid rocket projectile Download PDFInfo
- Publication number
- CN210549451U CN210549451U CN201921347670.5U CN201921347670U CN210549451U CN 210549451 U CN210549451 U CN 210549451U CN 201921347670 U CN201921347670 U CN 201921347670U CN 210549451 U CN210549451 U CN 210549451U
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- motor
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- solid rocket
- rocket projectile
- frock
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- 230000007246 mechanism Effects 0.000 title claims abstract description 34
- 239000007787 solid Substances 0.000 title claims abstract description 16
- 238000009434 installation Methods 0.000 title abstract description 4
- 238000001514 detection method Methods 0.000 claims abstract description 8
- 238000003825 pressing Methods 0.000 claims description 6
- 230000008878 coupling Effects 0.000 claims description 5
- 238000010168 coupling process Methods 0.000 claims description 5
- 238000005859 coupling reaction Methods 0.000 claims description 5
- 210000001503 joint Anatomy 0.000 claims description 5
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a flexible assembly mechanism of solid rocket projectile, the on-line screen storage device comprises a base, base upper surface front side is provided with the slip table, sliding connection has the last frock on the slip table, base top rear side is provided with actuating mechanism, actuating mechanism's removal end openly is provided with O type circle frock and top cap tightening frock respectively. This flexible final assembly mechanism of solid rocket projectile adopts the cooperation of frock of screwing up of piece frock, slip table, O type circle frock and top cap, can carry out automatic installation to O type circle and top cap, reduces personnel's operation, through the accurate detection of sensor, reduces artifical the hourglass and reads, and misreading improves production quality and efficiency, guarantees personnel's safety.
Description
Technical Field
The utility model relates to a guided missile assembly technical field specifically is a flexible assembly mechanism of solid rocket projectile.
Background
When the shell and the top cover of the solid rocket projectile are assembled, the solid rocket projectile is still manually transported for multiple times at the present stage, and manually knocked by a hammer and installed by a simple tool, so that the efficiency is low, and the problem caused by centralized personnel working places exists, and potential safety hazards exist.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a flexible assembly mechanism of solid rocket projectile to solve the problem of proposition among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a flexible assembly mechanism of a solid rocket projectile comprises a base, wherein a sliding table is arranged on the front side of the upper surface of the base, an upper workpiece tool is connected to the sliding table in a sliding mode, a driving mechanism is arranged on the rear side of the top of the base, and an O-shaped ring tool and a top cover screwing tool are respectively arranged on the front face of the moving end of the driving mechanism;
the workpiece loading tool comprises a clamping table in sliding connection with the sliding table, and one side of the top of the clamping table is provided with a clamping hand;
the O-shaped ring tool comprises a support A, wherein the top of the support A is fixedly connected with a motor A, the output end of the motor A penetrates through the support A and is connected with a flange, and a butt joint pressing flange is fixedly connected onto the flange;
the top cover screwing tool comprises a support B, a motor B is fixedly connected to the top of the support B, and the output end of the motor B penetrates through the support B and is connected with a hand grab in a matching mode.
Preferably, actuating mechanism includes a backplate, the positive both sides of backplate are provided with two guide rails, the swing joint has the removal slip table on the guide rail, the positive center department rigid coupling of backplate has support C, it has the screw nut subassembly to connect on the support C, the removal end and the removal slip table bottom rigid coupling of screw nut subassembly, the lead screw input end of screw nut subassembly is connected with motor C.
Preferably, a gap detection sensor is arranged at the bottom of the support B close to the hand grasping part.
Preferably, the motor A and the motor B are both stepping motors, and the motor C is a servo motor.
Compared with the prior art, the beneficial effects of the utility model are that: this flexible final assembly mechanism of solid rocket projectile adopts the cooperation of frock of screwing up of piece frock, slip table, O type circle frock and top cap, can carry out automatic installation to O type circle and top cap, reduces personnel's operation, through the accurate detection of sensor, reduces artifical the hourglass and reads, and misreading improves production quality and efficiency, guarantees personnel's safety.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is the utility model discloses a frock structure schematic diagram is screwed up to O type circle frock and top cap.
In the figure: 1. the base, 2, the slip table, 3, the frock of putting on, 301, the centre gripping platform, 302, press from both sides tight hand and hold, 4, O type circle frock, 401, motor A, 402, support A, 403, the flange, 404, butt joint push down the flange, 5, the frock is screwed up to the top cap, 501, motor B, 502, support B, 503, hold in the hand, 504, clearance detection sensor, 6, actuating mechanism, 601, remove the slip table, 602, lead screw nut subassembly, 603, support C, 604, motor C, 605, guide rail.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying 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.
Referring to fig. 1-2, the present invention provides a technical solution: a flexible assembly mechanism of a solid rocket projectile comprises a base 1, wherein a sliding table 2 is arranged on the front side of the upper surface of the base 1, an upper workpiece tool 3 is connected onto the sliding table 2 in a sliding manner, a driving mechanism 6 is arranged on the rear side of the top of the base 1, an O-shaped ring tool 4 and a top cover screwing tool 5 are respectively arranged on the front side of the moving end of the driving mechanism, and the upper workpiece tool 3 carries a workpiece to move on the sliding table 2 to the bottoms of the O-shaped ring tool 4 and the top cover screwing tool 5 for assembly;
the driving mechanism 6 comprises a back plate, two guide rails are arranged on two sides of the front surface of the back plate, a movable sliding table 601 is movably connected onto the guide rails, an O-shaped ring tool 4 and a top cover screwing tool 5 are fixedly connected onto the movable sliding table 601, a support C603 is fixedly connected to the center of the front surface of the back plate, a lead screw nut assembly 602 is connected onto the support C603, the moving end of the lead screw nut assembly 602 is fixedly connected with the bottom of the movable sliding table 601, the lead screw input end of the lead screw nut assembly 602 is connected with a motor C604, the motor C604 is a servo motor, the motor C604 works to drive the lead screw nut assembly 602 to work and drive the movable sliding table 601 to move up and down on the guide rails, and the O-shaped ring tool 4 and;
the workpiece loading tool 3 comprises a clamping table 301 connected with the sliding table 2 in a sliding mode, a clamping hand grip 302 is arranged on one side of the top of the clamping table 301, a shell and a liner are arranged in the clamping table 301, and the shell and the liner are clamped and fixed through the clamping hand grip 302;
the O-shaped ring tool 4 comprises a support A402, a motor A401 is fixedly connected to the top of the support A402, the motor A401 is a stepping motor, the output end of the motor A401 penetrates through the support A402 and is connected with a flange 403, a butt joint lower pressing flange 404 is fixedly connected to the flange 403, and the motor A401 drives the flange 403 and the butt joint lower pressing flange 404 to rotate;
the top cover screwing tool 5 comprises a support B502, a motor B501 is fixedly connected to the top of the support B502, the motor B501 is a stepping motor, the output end of the motor B501 penetrates through the support B502 and is connected with a hand grab 503 in a matching mode, a gap detection sensor 504 is arranged at the position, close to the hand grab 503, of the bottom of the support B502, the motor B501 drives the hand grab 503 to rotate, the hand grab 503 grabs a clamping top cover, and the gap detection sensor 504 is a laser sensor.
The working principle is as follows:
1. placing the shell and the liner on an upper workpiece tool 3, clamping the workpiece by a clamping gripper 302, and moving the workpiece to a position below an O-shaped ring tool 4 through a sliding table 2;
2. the driving mechanism 6 works to enable the movable sliding table 601 to drive the O-shaped ring tool 4 and the top cover screwing tool 5 to descend, the inner container is pushed into the shell by the O-shaped ring tool 4, and after the completion, the driving mechanism 6 works to enable the movable sliding table 601 to drive the O-shaped ring tool 4 and the top cover screwing tool 5 to ascend;
3. placing an O-shaped ring between the liner and the shell, enabling the movable sliding table 601 to drive the O-shaped ring tool 4 and the top cover screwing tool 5 to descend by the operation of the driving mechanism 6, pressing down the O-shaped ring, enabling the movable sliding table 601 to drive the O-shaped ring tool 4 and the top cover screwing tool 5 to ascend by the operation of the driving mechanism 6, enabling the motor A401 to rotate by 120 degrees, enabling the driving mechanism 6 to drive the O-shaped ring tool 4 to descend twice by the operation of the driving mechanism 6, enabling the O-shaped ring tool 4 to ascend by the driving mechanism 6 after the O-shaped ring tool is completed, repeating the process for three times, pressing down the O-shaped ring by 3mm each time, and moving;
4. with 1 circle of top cap screw in casing, casing and top cap current position person are correct back, actuating mechanism 6 descends the designated height, hold 503 blocks to the top cap on, motor B501 work drives and holds 503 rotatoryly, closes the top cap soon on the casing, detects casing and the current clearance of top cap through clearance detection sensor 504 and continues to compensate and screw up, aligns with the top cap groove when the casing, and stops to screw up when the clearance is less than 0.05 mm.
In the description of the present invention, it is to be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "other end", "upper", "one side", "top", "inner", "front", "center", "both ends", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "disposed," "connected," "fixed," "screwed" and the like are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides a flexible mechanism of always installing of solid rocket projectile which characterized in that: the automatic assembling device comprises a base (1), wherein a sliding table (2) is arranged on the front side of the upper surface of the base (1), an upper tool (3) is connected onto the sliding table (2) in a sliding manner, a driving mechanism (6) is arranged on the rear side of the top of the base (1), and an O-shaped ring tool (4) and a top cover screwing tool (5) are respectively arranged on the front side of the moving end of the driving mechanism;
the workpiece feeding tool (3) comprises a clamping table (301) in sliding connection with the sliding table (2), and a clamping hand grip (302) is arranged on one side of the top of the clamping table (301);
the O-shaped ring tool (4) comprises a support A (402), a motor A (401) is fixedly connected to the top of the support A (402), the output end of the motor A (401) penetrates through the support A (402) and is connected with a flange (403), and a butt joint pressing flange (404) is fixedly connected to the flange (403);
frock (5) is screwed up to top cap includes support B (502), support B (502) top rigid coupling has motor B (501), the output of motor B (501) runs through support B (502) cooperation and is connected with and holds in the palm (503).
2. The flexible final assembly mechanism of a solid rocket projectile according to claim 1, wherein: actuating mechanism (6) are including a backplate, the positive both sides of backplate are provided with two guide rails, it has removal slip table (601) to move on the guide rail to be connected with, the positive center department rigid coupling of backplate has support C (603), it has lead screw nut subassembly (602) to have gone up in support C (603), the removal end and the removal slip table (601) bottom rigid coupling of lead screw nut subassembly (602), the lead screw input end of lead screw nut subassembly (602) is connected with motor C (604).
3. The flexible final assembly mechanism of a solid rocket projectile according to claim 1, wherein: a gap detection sensor (504) is arranged at the bottom of the bracket B (502) close to the hand grab (503).
4. The flexible final assembly mechanism of a solid rocket projectile according to claim 1, wherein: and the motor A (401) and the motor B (501) are both stepping motors.
5. The flexible final assembly mechanism of a solid rocket projectile according to claim 2, wherein: the motor C (604) is a servo motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921347670.5U CN210549451U (en) | 2019-08-20 | 2019-08-20 | Flexible general installation mechanism of solid rocket projectile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921347670.5U CN210549451U (en) | 2019-08-20 | 2019-08-20 | Flexible general installation mechanism of solid rocket projectile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210549451U true CN210549451U (en) | 2020-05-19 |
Family
ID=70667105
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921347670.5U Expired - Fee Related CN210549451U (en) | 2019-08-20 | 2019-08-20 | Flexible general installation mechanism of solid rocket projectile |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210549451U (en) |
-
2019
- 2019-08-20 CN CN201921347670.5U patent/CN210549451U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200519 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |