Airplane electronic component welding device

Abstract

The utility model discloses an aircraft electronic component welding device which comprises a base, the top of the base is fixedly connected with a base and a vertical frame, the top of the vertical frame is fixedly connected with an air cylinder, the output end of one end of the air cylinder is fixedly connected with a movable plate, and the bottom of the movable plate is fixedly connected with a welding gun. A plurality of first bolts are in threaded connection with the inner side of the base, the outer sides of the first bolts are in threaded connection with bottom plates, and sliding grooves and stand columns are fixedly connected to the tops of the bottom plates correspondingly. When the aviation plug is placed, one wiring end on the aviation plug is placed on the placing seat, and a wire to be connected passes through the hole formed between the upper clamping block and the lower clamping block, so that the wire can be rapidly placed on the wiring end of the aviation plug, and a user can effectively and conveniently carry out rapid positioning and butt joint on the wire and a port of the aviation plug.

Description

Technical Field

[0001] The utility model belongs to the technical field of electronic welding, and particularly relates to a welding device for aircraft electronic components. Background Art

[0002] An aircraft electronic component welding device is a device specifically used for assembling and repairing electronic components in an aircraft electronic system. Such a device is usually used to permanently connect electronic components (such as integrated circuits, resistors, capacitors, sensors, etc.) to a printed circuit board or other supporting structures. The welding process may include traditional welding techniques, such as manual welding through welding needles or soldering irons, or the use of automated equipment, such as automatic welding robots, laser welding machines, etc.

[0003] When some existing aircraft electronic component welding devices are used for wire welding of aviation plugs, it is not convenient for operators to quickly position and dock the wires with the ports of the aviation plugs. Summary of the Utility Model

[0004] The technical problem to be solved by the utility model is to overcome the existing defects and provide a welding device for aircraft electronic components, so as to solve the problem that when some existing aircraft electronic component welding devices are used for wire welding of aviation plugs, it is not convenient for operators to quickly position and dock the wires with the ports of the aviation plugs as mentioned in the above background art.

[0005] To achieve the above object, the utility model provides the following technical scheme: A welding device for aircraft electronic components, including a base, on the top of which a pedestal and a vertical frame are respectively fixedly connected. A cylinder is fixedly connected to the top of the vertical frame. The output end of one end of the cylinder is fixedly connected to a moving plate. A welding gun is fixedly connected to the bottom of the moving plate. A first bolt is threadedly connected inside the pedestal. A plurality of the first bolts are symmetrically arranged. A bottom plate is threadedly connected to the outside of each first bolt. A chute and a column are respectively fixedly connected to the top of the bottom plate. A support member is slidably connected inside the chute. A placement seat is fixedly connected to one side of the column. A second bolt is threadedly connected inside the placement seat. Two of the second bolts are symmetrically arranged. A clamping member is threadedly connected to the outside of each second bolt.

[0006] Preferably, two sliding columns are slidably connected inside the moving plate. A first spring is movably connected to the outside of each sliding column. The first springs are located between the moving plate and the base.

[0007] Preferably, the support member includes a substrate, on the top of which an adjusting plate is fixedly connected. Two of the adjusting plates are symmetrically arranged. A third bolt is movably connected to the inside of each adjusting plate. A nut and a support seat are respectively threadedly connected to the outside of each third bolt.

[0008] Preferably, a first protective pad is fixedly connected to the top of the support base, and the first protective pad is located on one side of the adjusting plate.

[0009] Preferably, a first handle is fixedly connected to the bottom of one side of the support base, and the first handle is located above the substrate.

[0010] Preferably, a second handle is fixedly connected to one side of the substrate, and the second handle is located on one side of the adjusting plate.

[0011] Preferably, the clamping member includes a fixed frame. One side of the bottom of the fixed frame is fixedly connected to a second spring. The bottom of the second spring is fixedly connected to an upper clamping block. One side of the bottom of the fixed frame is fixedly connected to a lower clamping block. The other side of the bottom of the fixed frame is fixedly connected to a fixed block. There are two symmetrically arranged fixed blocks. One of the fixed blocks is fixedly connected to the lower clamping block on one side. Second protective pads are fixedly connected to one side of both the upper clamping block and the lower clamping block.

[0012] Preferably, gaskets are movably connected to the outer sides of one ends of the second bolts, and the gaskets are movably connected to the fixed blocks on one side.

[0013] Compared with the prior art, the utility model provides a welding device for aircraft electronic components, which has the following beneficial effects:

[0014] 1. By setting the clamping member in the utility model, the clamping member includes a fixed frame. One side of the bottom of the fixed frame is fixedly connected to a second spring. The bottom of the second spring is fixedly connected to an upper clamping block. The bottom of the upper clamping block is movably connected to a lower clamping block. One side of the lower clamping block is fixedly connected to the fixed frame. The other side of the lower clamping block is fixedly connected to a fixed block. There are two symmetrically arranged fixed blocks. One of the fixed blocks is fixedly connected to the fixed frame on one side. When it is necessary to weld wires to an aviation plug, first adjust the height of the support member, and then place the aviation plug on the support member, so that one of the wiring terminals on the aviation plug is placed on the placement seat. Pass the wire to be connected through the hole formed between the upper clamping block and the lower clamping block, so that the wire can be quickly placed on the wiring terminal of the aviation plug, effectively facilitating the user to quickly position and dock the wire with the port of the aviation plug;

[0015] 2. By setting the gasket in the utility model, the gasket is movably connected to the inner side of the second bolt, effectively increasing the stability of the second bolt, preventing the second bolt from loosening and falling off, which affects the fixation of the clamping member;

[0016] 3. By setting the sliding column and the first spring in the utility model, the sliding column is slidably connected to the inner side of the moving plate, and the first spring is movably connected to the outer side of the sliding column, effectively increasing the stability of the movement of the moving plate.

[0017] The parts not involved in this device are the same as those in the prior art or can be implemented using the prior art. The structure of this utility model is scientific and reasonable, safe and convenient to use, and provides great help to people. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The drawings are used to provide a further understanding of the present utility model, and constitute a part of the specification. Together with the embodiments of the present utility model, they are used to explain the present utility model, and do not constitute a limitation to the present utility model. In the drawings:

[0019] Figure 1 is an isometric structural schematic diagram of a welding device for aircraft electronic components proposed by the present utility model;

[0020] Figure 2 is Figure 1 an enlarged structural schematic diagram of part A in

[0021] Figure 3 is an exploded structural schematic diagram of a welding device for aircraft electronic components proposed by the present utility model;

[0022] Figure 4 is Figure 3 an enlarged structural schematic diagram of part B in

[0023] Figure 5 is Figure 3 an enlarged structural schematic diagram of part C in

[0024] Figure 6 is a side structural schematic diagram of a welding device for aircraft electronic components proposed by the present utility model;

[0025] In the figure: base 1, pedestal 2, first bolt 3, bottom plate 4, sliding groove 5, support member 6, column 7, placement seat 8, second bolt 9, clamping member 10, welding gun 11, moving plate 12, cylinder 13, vertical frame 14, sliding column 15, first spring 16, base plate 17, adjusting plate 18, third bolt 19, nut 20, support seat 21, first protective pad 22, first handle 23, second handle 24, fixing frame 25, second spring 26, upper clamping block 27, lower clamping block 28, fixing block 29, second protective pad 30, gasket 31. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0026] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0027] Please refer toFigures 1-6 , the present utility model provides a technical solution: an aircraft electronic component welding device, including a base 1, a base 2 and a vertical frame 14 are respectively fixedly connected to the top of the base 1, a cylinder 13 is fixedly connected to the top of the vertical frame 14, an output end of one end of the cylinder 13 is fixedly connected to a moving plate 12, a welding gun 11 is fixedly connected to the bottom of the moving plate 12, a first bolt 3 is threadedly connected inside the base 2, a plurality of first bolts 3 are symmetrically arranged, a bottom plate 4 is threadedly connected to the outside of each first bolt 3, a chute 5 and a column 7 are respectively fixedly connected to the top of the bottom plate 4, a support member 6 is slidably connected inside the chute 5, a placement seat 8 is fixedly connected to one side of the column 7, a second bolt 9 is threadedly connected inside the placement seat 8, two second bolts 9 are symmetrically arranged, clamping members 10 are threadedly connected to the outside of each second bolt 9. When wire welding of an aviation plug is required, first adjust the height of the support member 6, then place the aviation plug on the support member 6, such that one of the wiring terminals on the aviation plug is placed on the placement seat 8, and pass the wire to be connected through the hole formed between the upper clamping block 27 and the lower clamping block 28, so that the wire can be quickly placed on the wiring terminal of the aviation plug, effectively facilitating the user to quickly position and dock the wire with the port of the aviation plug.

[0028] In the present utility model, preferably, sliding columns 15 are slidably connected inside the moving plate 12, two sliding columns 15 are symmetrically arranged, first springs 16 are movably connected to the outside of each sliding column 15, and the first springs 16 are located between the moving plate 12 and the base 1, effectively increasing the stability of the movement of the moving plate 12.

[0029] In the present utility model, preferably, the support member 6 includes a base plate 17, an adjusting plate 18 is fixedly connected to the top of the base plate 17, two adjusting plates 18 are symmetrically arranged, third bolts 19 are movably connected to the inside of each adjusting plate 18, a nut 20 and a support seat 21 are respectively threadedly connected to the outside of each third bolt 19, effectively facilitating the user to adjust the height of the support seat 21 and facilitating the welding of the aviation plug and the wire.

[0030] In the present utility model, preferably, a first protective pad 22 is fixedly connected to the top of the support seat 21, and the first protective pad 22 is located on one side of the adjusting plate 18, effectively preventing the aviation socket from sliding on the support seat 21 and affecting the welding of the wire.

[0031] In the present utility model, preferably, a first handle 23 is fixedly connected to the bottom of one side of the support seat 21, and the first handle 23 is located above the base plate 17, effectively facilitating the user to hold the first handle 23 to move the support seat 21 up and down.

[0032] In the present utility model, preferably, a second handle 24 is fixedly connected to one side of the base plate 17, and the second handle 24 is located on one side of the adjusting plate 18, effectively facilitating the user to hold the second handle 24 to take out the support member 6.

[0033] In the present utility model, preferably, the clamping member 10 includes a fixed frame 25. One side of the bottom of the fixed frame 25 is fixedly connected to a second spring 26. The bottom of the second spring 26 is fixedly connected to an upper clamping block 27. One side of the bottom of the fixed frame 25 is fixedly connected to a lower clamping block 28. The other side of the bottom of the fixed frame 25 is fixedly connected to a fixed block 29. There are two symmetrically arranged fixed blocks 29. One of the fixed blocks 29 is fixedly connected to the lower clamping block 28 on one side. Second protective pads 30 are fixedly connected to one side of both the upper clamping block 27 and the lower clamping block 28, effectively preventing the wire from sliding during welding and affecting the welding.

[0034] In the present utility model, preferably, gaskets 31 are movably connected to the outer sides of one ends of the second bolts 9, and the gaskets 31 are movably connected to the fixed blocks 29 on one side.

[0035] The working principle and usage process of the present utility model: When in use, when it is necessary to weld wires to the aviation plug, first adjust the height of the support member 6, and then place the aviation plug on the support member 6, so that one of the wiring terminals on the aviation plug is placed on the placement seat 8. Pass the wire to be connected through the hole formed between the upper clamping block 27 and the lower clamping block 28, so that the wire can be quickly placed on the wiring terminal of the aviation plug, effectively facilitating the user to quickly position and dock the wire with the port of the aviation plug.

[0036] Although the embodiments of the present utility model have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions, and variations can be made to these embodiments without departing from the principle and spirit of the present utility model. The scope of the present utility model is defined by the appended claims and their equivalents.

Claims

1. An aircraft electronic component welding device, comprising a base (1), characterized in that: At the top of the base (1), a base (2) and a vertical frame (14) are respectively fixedly connected. At the top of the vertical frame (14), a cylinder (13) is fixedly connected. At one end of the cylinder (13), an output end is fixedly connected with a moving plate (12). At the bottom of the moving plate (12), a welding gun (11) is fixedly connected. Inside the base (2), a first bolt (3) is in threaded connection. A plurality of the first bolts (3) are symmetrically arranged. A bottom plate (4) is in threaded connection with the outer sides of the first bolts (3). At the top of the bottom plate (4), a chute (5) and a column (7) are respectively fixedly connected. Inside the chute (5), a support member (6) is slidably connected. On one side of the column (7), a placement seat (8) is fixedly connected. Inside the placement seat (8), a second bolt (9) is in threaded connection. Two of the second bolts (9) are symmetrically arranged. A clamping member (10) is in threaded connection with the outer sides of the second bolts (9).

2. The welding device for aircraft electronic components according to claim 1, characterized in that: Inside the moving plate (12), a sliding column (15) is slidably connected. Two of the sliding columns (15) are symmetrically arranged. A first spring (16) is movably connected to the outer sides of the sliding columns (15). The first spring (16) is located between the moving plate (12) and the base (1).

3. The welding device for aircraft electronic components according to claim 1, characterized in that: The support member (6) includes a base plate (17). At the top of the base plate (17), an adjusting plate (18) is fixedly connected. Two of the adjusting plates (18) are symmetrically arranged. Inside the adjusting plates (18), a third bolt (19) is movably connected. A nut (20) and a support seat (21) are respectively in threaded connection with the outer sides of the third bolts (19).

4. The welding device for aircraft electronic components according to claim 3, characterized in that: At the top of the support seat (21), a first protective pad (22) is fixedly connected. The first protective pad (22) is located on one side of the adjusting plate (18).

5. The welding device for aircraft electronic components according to claim 3, characterized in that: At the bottom of one side of the support seat (21), a first handle (23) is fixedly connected. The first handle (23) is located above the base plate (17).

6. The welding device for aircraft electronic components according to claim 3, wherein: On one side of the base plate (17), a second handle (24) is fixedly connected. The second handle (24) is located on one side of the adjusting plate (18).

7. The welding device for aircraft electronic components according to claim 1, characterized in that: The clamping member (10) includes a fixing frame (25). At the bottom of one side of the fixing frame (25), a second spring (26) is fixedly connected. At the bottom of the second spring (26), an upper clamping block (27) is fixedly connected. At the bottom of one side of the fixing frame (25), a lower clamping block (28) is fixedly connected. At the bottom of the other side of the fixing frame (25), fixing blocks (29) are fixedly connected. Two of the fixing blocks (29) are symmetrically arranged. On one side of one of the fixing blocks (29), a lower clamping block (28) is fixedly connected. Second protective pads (30) are fixedly connected to one side of the upper clamping block (27) and the lower clamping block (28).

8. The welding device for aircraft electronic components according to claim 1, wherein: On the outer sides of one end of the second bolts (9), washers (31) are movably connected. On one side of the washers (31), fixing blocks (29) are movably connected.

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