CN218255065U - Rocket assembly is with multi-functional material access arrangement - Google Patents

Rocket assembly is with multi-functional material access arrangement Download PDF

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Publication number
CN218255065U
CN218255065U CN202221754401.2U CN202221754401U CN218255065U CN 218255065 U CN218255065 U CN 218255065U CN 202221754401 U CN202221754401 U CN 202221754401U CN 218255065 U CN218255065 U CN 218255065U
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China
Prior art keywords
pair
multifunctional material
support frame
box
material storing
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CN202221754401.2U
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Chinese (zh)
Inventor
王端志
李少宁
孙伟
董翰林
王成龙
吕泽帅
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Shandong Long March Rocket Co ltd
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Shandong Long March Rocket Co ltd
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Priority to CN202221754401.2U priority Critical patent/CN218255065U/en
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Abstract

The utility model discloses a multifunctional material storing and taking device for rocket assembly, which comprises a base, wherein the base is provided with a multifunctional material storing and taking structure; the multifunctional material storing and taking structure comprises: the support device comprises a pair of support rods, a door-shaped support frame, support rods, a tool box, a consumable box, a plurality of standard component boxes, an adjusting component and a rotating component; a pair of the bracing piece is installed on the wall on the base, door type support frame and a pair of be equipped with adjusting part between the bracing piece, the bracing piece is installed on the door type support frame, the utility model relates to a carrier rocket section assembly operation technical field, the present case mainly adopts material access structure, simple structure, and the simple operation can improve the discernment efficiency of putting up the in-process owing to during the assembly place of design initiating explosive device, conveniently carry out categorised access with standard component, instrument and consumptive material when rocket section assembly operation.

Description

Rocket assembly is with multi-functional material access arrangement
Technical Field
The utility model relates to a carrier rocket section assembly operation technical field specifically is a multi-functional material access arrangement is used to rocket assembly.
Background
At present, in the rocket assembly operation process, the types of materials and auxiliary tools required by assembly operation are various, and particularly, a mechanical device is used as a main part in the field related to initiating explosive devices, so that a multifunctional material access device which is efficient in access and clear in classification and mainly comprises the mechanical device is needed in the assembly field related to initiating explosive devices.
SUMMERY OF THE UTILITY MODEL
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a multifunctional material storing and taking device for rocket assembly comprises a base, wherein a multifunctional material storing and taking structure is arranged on the base;
the multifunctional material storing and taking structure comprises: the pair of supporting rods, the door-shaped supporting frame, the supporting rods, the tool box, the consumable box, the plurality of standard component boxes, the adjusting component and the rotating component are arranged on the box body;
the utility model discloses a door type bracing piece, including base, door type support frame, bracing piece, door type support frame, a plurality of consumable part box, door type support frame, a plurality of the bracing piece is installed on the wall on the base, door type support frame and a pair of be equipped with adjusting part between the bracing piece, the bracing piece is installed on the door type support frame, the tool holder with be equipped with the runner assembly between the bracing piece, the consumable part box is installed on the door type support frame, it is a plurality of the standard part box is located consumable part box right side.
Preferably, the adjusting assembly comprises: the pair of screw rod modules, the pair of moving blocks and the connecting rod;
the pair of lead screw modules are respectively installed on the pair of support rods, the pair of moving blocks are installed on the pair of lead screw module moving ends, the door-shaped support frame is installed on the pair of moving blocks, the connecting rod is installed on the door-shaped support frame, and the connecting rod is located below the consumable box and the plurality of standard component boxes.
Preferably, the rotating assembly comprises: the hinge comprises a hinge seat, a connecting block and a rotating shaft;
the hinge seat is installed on the tool box, the connecting block is installed at the right end of the supporting rod, through holes are formed in the upper wall surface and the lower wall surface of the connecting block, and the rotating shaft is movably installed at the through holes formed in the hinge seat and the upper wall surface of the connecting block.
Preferably, a reinforcing rib for supporting is arranged between the pair of supporting rods and the base.
Preferably, a universal wheel for moving is arranged below the base.
Preferably, a clamp spring for fastening is arranged on the rotating shaft.
Advantageous effects
The utility model provides a rocket assembly is with multi-functional material access arrangement. The method has the following beneficial effects:
the present case mainly adopts material access structure, simple structure, and the simple operation can be when rocket section assembly operation, because during the assembly place of design initiating explosive device, conveniently carries out categorised access with standard component, instrument and consumptive material and improves the discernment efficiency of putting up the in-process.
Drawings
Fig. 1 is a schematic view of a partial three-dimensional structure of a multifunctional material storing and taking device for rocket assembly.
Fig. 2 is a schematic view of a local three-dimensional structure of the multifunctional material storing and taking device for rocket assembly of the present invention.
Fig. 3 is the utility model discloses a rocket assembly is with multi-functional material access arrangement's main view structure schematic diagram.
Fig. 4 is a schematic view of a top view structure of the multifunctional material storing and taking device for rocket assembly of the present invention.
In the figure: 1-a base; 2-a support rod; 3-door type support frame; 4-a support bar; 5-a tool box; 6-consumable box; 7-standard component box; 8-a lead screw module; 9-a moving block; 10-a connecting rod; 11-a hinge mount; 12-connecting blocks; 13-a rotating shaft; 14-reinforcing ribs; 15-universal wheels; 16-clamp spring.
Detailed Description
Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.
Example (b): referring to fig. 1-4, the main components of the present invention are: the multifunctional material storage and taking device comprises a base 1, wherein a multifunctional material storage and taking structure is arranged on the base 1;
it should be noted that, when the rocket is assembled, the multifunctional material storing and taking structure on the base 1 can be used for storing and taking materials.
In the specific implementation process, the multifunctional material storing and taking structure comprises: the device comprises a pair of supporting rods 2, a door-shaped supporting frame 3, the supporting rods 2, a tool box 5, a consumable box 6, a plurality of standard component boxes 7, an adjusting component and a rotating component;
a pair of bracing piece 2 is installed on the wall on the base 1, door type support frame 3 and a pair of be equipped with adjusting part between the bracing piece 2, bracing piece 2 is installed door type support frame 3 is last, tool holder 5 with be equipped with runner assembly between the bracing piece 2, consumptive material box 6 is installed door type support frame 3 is last, and is a plurality of standard component box 7 is located 6 right sides of consumptive material box.
It should be noted that, when rocket assembly needs to set up standard part, instrument and consumptive material, can place the standard part in a plurality of standard part boxes 7, place the consumptive material in consumptive material box 6, place the instrument in tool box 5, correspond and place improvement identification efficiency, and can use the adjusting part according to the high demand of difference, adjust tool box 5, the height of consumptive material box 6 and a plurality of standard part boxes 7, according to the angle of using custom adjustment tool box 5.
In one embodiment, the adjusting assembly further comprises: a pair of lead screw modules 8, a pair of moving blocks 9 and a connecting rod 10;
the pair of lead screw modules 8 are respectively installed on the pair of support rods 2, the pair of moving blocks 9 are installed on the moving ends of the pair of lead screw modules 8, the portal support frame 3 is installed on the pair of moving blocks 9, the connecting rod 10 is installed on the portal support frame 3, and the connecting rod 10 is located below the consumable box 6 and the plurality of standard component boxes 7.
When the height needs to be adjusted, the pair of lead screw modules 8 mounted on the pair of support rods 2 are energized, the moving ends of the pair of lead screw modules 8 move to drive the pair of moving blocks 9 mounted on the moving ends of the pair of lead screw modules 8 to move, so that the height of the portal support frame 3 is adjusted, and the connecting rod 10 mounted on the portal support frame 3 plays a supporting role.
In one embodiment, the rotating assembly further comprises: hinge mount 11, connecting block 12 and rotating shaft 13;
the hinge seat 11 is installed on the tool box 5, the connecting block 12 is installed at the right end of the supporting rod 2, through holes are formed in the upper wall surface and the lower wall surface of the connecting block 12, and the rotating shaft 13 is movably installed at the through holes formed in the hinge seat 11 and the upper wall surface of the connecting block 12.
It should be noted that, since the rotating shaft 13 is installed at the through holes formed on the upper and lower wall surfaces of the hinge base 11 and the connecting block 12, the hinge base 11 can rotate around the rotating shaft 13, so that the angle of the tool box 5 can be adjusted.
In the specific implementation process, a reinforcing rib 14 for supporting is further arranged between the pair of supporting rods 2 and the base 1.
In the specific implementation process, furthermore, a universal wheel 15 for moving is arranged below the base 1.
In a specific implementation process, a clamp spring 16 for fastening is further disposed on the rotating shaft 13.
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 (6)

1. A multifunctional material storing and taking device for rocket assembly comprises a base, and is characterized in that a multifunctional material storing and taking structure is arranged on the base;
the multifunctional material storing and taking structure comprises: the pair of supporting rods, the door-shaped supporting frame, the supporting rods, the tool box, the consumable box, the plurality of standard component boxes, the adjusting component and the rotating component are arranged on the box body;
the utility model discloses a door type bracing piece, including door type support frame, bracing piece, tool box, consumable box, door type support frame, a plurality of standard component boxes are installed on the door type support frame, it is a plurality of the standard component box is located consumable box right side.
2. A rocket assembly multifunctional material access device as recited in claim 1, wherein said adjustment assembly comprises: the pair of screw rod modules, the pair of moving blocks and the connecting rod are arranged in the groove;
the pair of lead screw modules are respectively installed on the pair of support rods, the pair of moving blocks are installed on the pair of lead screw module moving ends, the portal type support frame is installed on the pair of moving blocks, the connecting rod is installed on the portal type support frame, and the connecting rod is located below the consumable box and the plurality of standard component boxes.
3. A rocket assembly multifunctional material access device as recited in claim 1, wherein said rotating assembly comprises: the hinge comprises a hinge seat, a connecting block and a rotating shaft;
the hinge seat is installed on the tool box, the connecting block is installed at the right end of the supporting rod, through holes are formed in the upper wall surface and the lower wall surface of the connecting block, and the rotating shaft is movably installed at the hinge seat and the through holes formed in the upper wall surface of the connecting block.
4. A multifunctional material storing and taking device for rocket assembly as recited in claim 1, wherein a reinforcing rib is provided between a pair of said supporting rods and said base for supporting.
5. A rocket assembly multifunctional material storing and taking device as recited in claim 1, wherein universal wheels for moving are arranged below said base.
6. The multifunctional material storing and taking device for rocket assembly according to claim 3, wherein said rotating shaft is provided with a clamp spring for fastening.
CN202221754401.2U 2022-07-07 2022-07-07 Rocket assembly is with multi-functional material access arrangement Active CN218255065U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202221754401.2U CN218255065U (en) 2022-07-07 2022-07-07 Rocket assembly is with multi-functional material access arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221754401.2U CN218255065U (en) 2022-07-07 2022-07-07 Rocket assembly is with multi-functional material access arrangement

Publications (1)

Publication Number Publication Date
CN218255065U true CN218255065U (en) 2023-01-10

Family

ID=84759449

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202221754401.2U Active CN218255065U (en) 2022-07-07 2022-07-07 Rocket assembly is with multi-functional material access arrangement

Country Status (1)

Country Link
CN (1) CN218255065U (en)

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