CN220388471U - Civil air defense engineering door location welding frock - Google Patents

Civil air defense engineering door location welding frock Download PDF

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Publication number
CN220388471U
CN220388471U CN202322019701.7U CN202322019701U CN220388471U CN 220388471 U CN220388471 U CN 220388471U CN 202322019701 U CN202322019701 U CN 202322019701U CN 220388471 U CN220388471 U CN 220388471U
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China
Prior art keywords
air defense
civil air
defense engineering
positioning
engineering door
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Active
Application number
CN202322019701.7U
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Chinese (zh)
Inventor
余辉
沈志刚
周盼盼
陈宇豪
余荣诚
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Jiangsu Jingbao Engineering Detection Co ltd
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Jiangsu Jingbao Engineering Detection Co ltd
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Abstract

The utility model discloses a civil air defense engineering door positioning and welding tool, and relates to the technical field of processing and positioning of civil air defense engineering doors; the utility model comprises a fixed column; the positioning pressing plate is required to move upwards, the civil air defense engineering door is placed on the machining adjusting plate, the inserting rod is taken out from the inserting hole, after the inserting rod is taken out, the positioning spring pushes the positioning pressing plate to move downwards, so that the positioning pressing plate presses the civil air defense engineering door, when the tool is used, people can move the positioning pressing plate up and down, the civil air defense engineering doors with different thicknesses are fixed by adjusting the height of the positioning pressing plate, when the tool is used, the machining adjusting plate is required to be rotated according to the position to be machined of the civil air defense engineering door, the civil air defense engineering door is further rotated, the position of the civil air defense engineering door is adjusted, after the position is adjusted, the machining adjusting plate is fixed, and when the tool is used, the people do not need to frequently change the position of the people to machine the civil air defense engineering door, so that convenience when the civil air defense engineering door is machined is greatly improved.

Description

Civil air defense engineering door location welding frock
Technical Field
The utility model relates to the technical field of civil air defense engineering door processing and positioning, in particular to a civil air defense engineering door positioning and welding tool.
Background
The civil air defense engineering door is important equipment in the civil air defense engineering, so the requirements on the door are higher, the door not only has good anti-collision capability, but also has a flame-retardant function, and the door still has more inconvenient problems;
when producing and processing civil air defense engineering door, personnel can use the civil air defense engineering door to fix the civil air defense engineering door with the frock of welding to personnel welds it, and current civil air defense engineering door location welding frock needs place the civil air defense engineering door above that when using, later personnel frequently change the position of standing around the frock and weld the position that needs welded on the civil air defense engineering door, in whole course of working, personnel need frequently change the position of oneself and process the civil air defense engineering door, thereby are difficult to improve the convenience when personnel process the civil air defense engineering door.
In order to solve the problems, the inventor provides a civil air defense engineering door positioning and welding tool for solving the problems.
Disclosure of Invention
In order to solve the problem that personnel need to frequently change the position of the personnel to process the civil air defense engineering door in the whole processing process; the utility model aims to provide a civil air defense engineering door positioning and welding tool.
In order to solve the technical problems, the utility model adopts the following technical scheme: the utility model provides a people's air defense engineering door location welding frock, the steam generator comprises a fixed column, the fixed column's fixed surface is connected with spacing supporting ring, spacing supporting ring's top swing joint has the processing regulating plate, spacing round hole has been seted up on the surface of processing regulating plate, spacing screw hole has been seted up on the surface of fixed column, spacing screw thread connection has spacing screw thread piece in spacing screw hole, utilize spacing screw thread piece can be fixed processing regulating plate, spacing round bar is pegged graft in the inside of spacing round bar, one end and one side fixed connection of spacing screw thread piece, fixed column and processing regulating plate swing joint, be convenient for process regulating plate and rotate on the fixed column, the other end fixedly connected with of spacing round bar is supplementary to remove the stick, utilize supplementary removal stick, be convenient for personnel to remove spacing round bar, the bottom fixedly connected with counter weight seat of fixed column, the top swing joint of processing regulating plate has the location pressure applying plate, utilize the location pressure applying plate can be fixed connection to the location stick, the surface swing joint of location stick has the location spring, location spring can promote the location pressure applying plate, make the location pressure applying plate to the top of location spring, the tip is fixed connection has the tip to be connected with the tip, the tip is fixed connection hole, the tip is provided with the thread hole at the rotation of the screw thread hole, the person's the person rotates the pipe is rotated at the inside of the fixed connection hole, the tip is screwed joint hole, the person is convenient for rotate, the person is connected with the screw thread hole, the person rotates the tip is fixed with the hole, the thread hole. The bottom of counter weight seat is provided with the universal wheel, and the other end and the grafting stick fixed connection of screw thread reinforcement pipe, the telescopic hole has been seted up at the top of link, and the spliced eye has all been seted up to the both sides of location pressurization board, and the inside grafting of spliced eye has the grafting stick.
Preferably, the number of the universal wheels is three, and the diameter of the telescopic hole is smaller than that of the positioning spring, so that the positioning spring is convenient to retract.
Preferably, the top of the limit supporting ring is provided with an auxiliary rotating hole, an auxiliary ball is movably connected in the auxiliary rotating hole, and the auxiliary ball is utilized to facilitate the rotation of the processing adjusting plate on the limit supporting ring.
Compared with the prior art, the utility model has the beneficial effects that:
when the tool is used, people can move the positioning pressing plate up and fix the civil air defense engineering doors with different thickness by adjusting the height of the positioning pressing plate, and the machining adjusting plate is rotated according to the position to be machined of the civil air defense engineering doors during machining, so that the civil air defense engineering doors are rotated, the positions of the civil air defense engineering doors are adjusted, the machining adjusting plate is fixed after the positions are adjusted, and when the tool is used, machining of the civil air defense engineering doors is performed without frequent change of the positions of machining personnel, so that the convenience of machining the civil air defense engineering doors is greatly improved.
Drawings
In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic diagram of the overall structure of the present utility model.
Fig. 2 is a schematic structural view of a plug rod according to the present utility model.
Fig. 3 is a schematic view of the structure of fig. 2 at a partially enlarged scale according to the present utility model.
Fig. 4 is a partially enlarged schematic view of the structure of fig. 2B according to the present utility model.
In the figure: 1. fixing the column; 2. a limit support ring; 3. machining an adjusting plate; 4. limiting round holes; 5. a limit threaded hole; 6. limiting thread blocks; 7. limiting round bars; 8. positioning a pressing plate; 9. a positioning rod; 10. a positioning spring; 11. a connecting frame; 12. a telescopic hole; 13. a plug hole; 14. an auxiliary moving rod; 15. a counterweight seat; 16. a threaded reinforcing hole; 17. a threaded reinforcing tube; 18. rotating the connecting rod; 19. a plug rod; 20. a universal wheel; 21. and (5) assisting the ball.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Examples: as shown in fig. 1-4, the utility model provides a positioning welding tool for a civil air defense engineering door, which comprises a fixed column 1, wherein the surface of the fixed column 1 is fixedly connected with a limiting support ring 2, the top of the limiting support ring 2 is movably connected with a processing adjusting plate 3, the surface of the processing adjusting plate 3 is provided with a limiting round hole 4, the surface of the fixed column 1 is provided with a limiting threaded hole 5, the internal thread of the limiting threaded hole 5 is connected with a limiting threaded block 6, the processing adjusting plate 3 can be fixed by the limiting threaded block 6, the inside of the limiting round hole 4 is inserted with a limiting round bar 7, the top of the processing adjusting plate 3 is movably connected with a positioning pressing plate 8, the two sides of the top of the positioning pressing plate 8 are fixedly connected with positioning bars 9, the surface of the positioning bars 9 is movably connected with positioning springs 10, the positioning springs 10 can push the positioning pressing plate 8 to press the civil air defense engineering door, the top of the positioning springs 10 is fixedly connected with a connecting frame 11, the top of the connecting frame 11 is provided with a telescopic hole 12, the two sides of the positioning pressing plate 8 are provided with inserting holes 13, and the inserting holes 19 are inserted into the inserting holes 13.
One end of a limiting round bar 7 is fixedly connected with one side of a limiting threaded block 6, and a fixing column 1 is movably connected with a machining adjusting plate 3.
By adopting the technical scheme, the fixed column 1 is movably connected with the processing adjusting plate 3, so that the processing adjusting plate 3 can conveniently rotate on the fixed column 1.
The other end of the limiting round bar 7 is fixedly connected with an auxiliary moving bar 14, and the bottom end of the fixed column 1 is fixedly connected with a counterweight base 15.
By adopting the technical scheme, the auxiliary moving rod 14 is utilized, so that a person can conveniently move the limiting round rod 7.
Both sides of the connecting frame 11 are provided with threaded reinforcing holes 16, and the inner threads of the threaded reinforcing holes 16 are connected with threaded reinforcing pipes 17.
By adopting the above technical scheme, install the screw reinforcement pipe 17 in the screw reinforcement hole 16, can improve the steadiness when the one end of grafting stick 19 is in spliced eye 13.
One end of the threaded reinforcing pipe 17 is fixedly connected with a rotary connecting rod 18, and the other end of the threaded reinforcing pipe 17 is fixedly connected with a plugging rod 19.
By adopting the above technical scheme, the screw reinforcement pipe 17 is convenient for personnel to move by using the rotary connecting rod 18.
Friction lines are arranged on the surfaces of the rotary connecting rod 18 and the auxiliary moving rod 14, and universal wheels 20 are arranged at the bottom of the counterweight seat 15.
By adopting the above technical scheme, the friction lines are utilized, so that a person can conveniently grip the rotary connecting rod 18 and the auxiliary moving rod 14.
The number of the universal wheels 20 is three, and the diameter of the telescopic hole 12 is smaller than that of the positioning spring 10.
By adopting the above technical scheme, the diameter of the telescopic hole 12 is smaller than that of the positioning spring 10, so that the positioning spring 10 is convenient to contract.
An auxiliary rotating hole is formed in the top of the limit supporting ring 2, and an auxiliary ball 21 is movably connected to the inside of the auxiliary rotating hole.
By adopting the technical scheme, the auxiliary ball 21 is utilized, so that the machining adjusting plate 3 can rotate on the limiting support ring 2 conveniently.
Working principle: during operation, need upwards remove location pressurization board 8, when its upwards remove, it will apply force to location spring 10, and then make location spring 10 shrink, afterwards insert plug rod 19 in jack 13, in order to fix location pressurization board 8 on certain height, place the people's air defense engineering door on processing regulating plate 3 again, after placing people's air defense engineering door, need take out plug rod 19 from jack 13, after taking out, location spring 10 will promote location pressurization board 8 and remove downwards, make location pressurization board 8 to the air defense engineering door pressure, and then fix people's air defense engineering door on processing regulating plate 3, afterwards insert plug rod 19 in jack 13, in order to fix location pressurization board 8, during the use, personnel can reciprocate location pressurization board 8, fix the air defense engineering door of thickness difference through adjusting the height of location pressurization board 8, during processing, need rotate processing regulating plate 3 according to the position that people's air defense engineering door is to be processed, and then make the air defense engineering door rotate, thereby adjust the position of people's air defense engineering door, adjust the position of good, insert 7 into limit 7 and need not to insert into limit stop 7 in the round limit stop plate 6 when processing round limit stop, the people's air defense engineering door is required to be processed, the round limit stop 7 is moved to the round limit stop 7, and the people's air defense engineering door is required to be processed, the round limit stop 7 is moved, and is adjusted, the round limit stop position is moved round, and is moved round, the people's air defense engineering door is moved, and is required to be processed, and is moved.
It will be apparent to those skilled in the art that various modifications and variations can be made to the present utility model without departing from the spirit or scope of the utility model. Thus, it is intended that the present utility model also include such modifications and alterations insofar as they come within the scope of the appended claims or the equivalents thereof.

Claims (8)

1. The utility model provides a civil air defense engineering door location welding frock, includes fixed column (1), its characterized in that: the surface of the fixed column (1) is fixedly connected with a limit supporting ring (2), the top of the limit supporting ring (2) is movably connected with a processing adjusting plate (3), a limit round hole (4) is formed in the surface of the processing adjusting plate (3), a limit threaded hole (5) is formed in the surface of the fixed column (1), a limit threaded block (6) is connected with the internal thread of the limit threaded hole (5), a limit round bar (7) is inserted in the limit round hole (4), the machining adjusting plate is characterized in that the top of the machining adjusting plate (3) is movably connected with a positioning pressing plate (8), two sides of the top of the positioning pressing plate (8) are fixedly connected with positioning rods (9), the surfaces of the positioning rods (9) are movably connected with positioning springs (10), the top ends of the positioning springs (10) are fixedly connected with connecting frames (11), the tops of the connecting frames (11) are provided with telescopic holes (12), two sides of the positioning pressing plate (8) are provided with inserting holes (13), and inserting rods (19) are inserted into the inserting holes (13).
2. The civil air defense engineering door positioning and welding tool as claimed in claim 1, wherein one end of the limiting round rod (7) is fixedly connected with one side of the limiting threaded block (6), and the fixing column (1) is movably connected with the machining adjusting plate (3).
3. The civil air defense engineering door positioning and welding tool as recited in claim 2, wherein the other end of the limiting round rod (7) is fixedly connected with an auxiliary moving rod (14), and the bottom end of the fixed column (1) is fixedly connected with a counterweight seat (15).
4. A civil air defense engineering door positioning and welding fixture as claimed in claim 3, wherein the two sides of the connecting frame (11) are provided with threaded reinforcing holes (16), and the inner threads of the threaded reinforcing holes (16) are connected with threaded reinforcing pipes (17).
5. The civil air defense engineering door positioning and welding tool as recited in claim 4, wherein one end of the threaded reinforcing pipe (17) is fixedly connected with a rotary connecting rod (18), and the other end of the threaded reinforcing pipe (17) is fixedly connected with the plugging rod (19).
6. The civil air defense engineering door positioning and welding tool as recited in claim 5, wherein friction lines are arranged on the surfaces of the rotary connecting rod (18) and the auxiliary moving rod (14), and universal wheels (20) are arranged at the bottom of the counterweight base (15).
7. The civil air defense engineering door positioning and welding fixture as recited in claim 6, wherein the number of the universal wheels (20) is three, and the diameter of the telescopic hole (12) is smaller than the diameter of the positioning spring (10).
8. The civil air defense engineering door positioning and welding tool as recited in claim 7, wherein an auxiliary rotating hole is formed in the top of the limiting support ring (2), and an auxiliary ball (21) is movably connected to the inside of the auxiliary rotating hole.
CN202322019701.7U 2023-07-31 2023-07-31 Civil air defense engineering door location welding frock Active CN220388471U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202322019701.7U CN220388471U (en) 2023-07-31 2023-07-31 Civil air defense engineering door location welding frock

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202322019701.7U CN220388471U (en) 2023-07-31 2023-07-31 Civil air defense engineering door location welding frock

Publications (1)

Publication Number Publication Date
CN220388471U true CN220388471U (en) 2024-01-26

Family

ID=89615532

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202322019701.7U Active CN220388471U (en) 2023-07-31 2023-07-31 Civil air defense engineering door location welding frock

Country Status (1)

Country Link
CN (1) CN220388471U (en)

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