CN219746583U - Aviation plug hot air welding device - Google Patents
Aviation plug hot air welding device Download PDFInfo
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- CN219746583U CN219746583U CN202321122917.XU CN202321122917U CN219746583U CN 219746583 U CN219746583 U CN 219746583U CN 202321122917 U CN202321122917 U CN 202321122917U CN 219746583 U CN219746583 U CN 219746583U
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- welding
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- plug
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- 238000003466 welding Methods 0.000 title claims abstract description 66
- 229910000679 solder Inorganic materials 0.000 claims abstract description 11
- 230000005540 biological transmission Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 description 6
- 238000004804 winding Methods 0.000 description 3
- 244000309464 bull Species 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
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Abstract
The utility model discloses an aviation plug hot air welding device, which particularly relates to the field of welding devices, and comprises a workbench, a bracket, a welding component, a hot air gun, a solder paste needle head, a first support plate, a follow-up mechanism, a second support plate, a rotating mechanism and a clamping mechanism. The utility model has the advantages that the aviation plug can be clamped and fixed, so that welding is more stable, bad generation is prevented, and meanwhile, the aviation plug can be rotated, so that the aviation plug can be subjected to annular welding, and the welding efficiency is improved.
Description
Technical Field
The utility model belongs to the technical field of welding devices, and particularly relates to an aviation plug hot air welding device.
Background
Aviation plug is an element for connecting electric lines, and consists of a plug and a socket. The connection and disconnection of the circuit are realized through the plugging and separating of the plug. In the construction of aviation plugs, three connecting modes of bolt tightening, buckling and pressing and traditional welding are usually adopted, and the former two modes are easier; the aviation plug is manufactured in a welding mode, is influenced by various factors, has good welding quality, and has great influence on the running stability and reliability of production equipment.
The utility model patent of the patent application publication number CN213104970U discloses an automatic hot air welding device, and the whole spot solder paste welding process is automatic, so that no labor is needed, the efficiency is improved, and the labor is saved; the equipment has high flexibility, and different carriers can be replaced to realize hot air welding of different products; the equipment has simple structure, low cost and high cost performance.
However, in the structure, when the welding device is actually used, the welding part is supported by the tray, but the welding part cannot be fixed, and is easily affected by wind power to move in the process of heating by hot air, so that poor welding is easily caused, meanwhile, on the welding of the aviation plug, circumferential welding is required to be carried out on the plug, and the tray cannot rotate the supported plug, so that the welding point is more troublesome to adjust, and the welding efficiency is affected.
Disclosure of Invention
The technical scheme of the utility model aims at solving the technical problem of overlarge singleness in the prior art and provides a solution which is obviously different from the prior art. The utility model provides an aviation plug hot air welding device, which aims to solve the problems.
The utility model is realized in such a way that the utility model provides the following technical scheme: the utility model provides an aviation plug hot air welding device, including workstation, support, welding set spare, hot air gun, solder paste syringe needle, first backup pad, follower, second backup pad, slewing mechanism and fixture, the support is installed on the workstation top, and the support top supports has welding set spare, and welding set spare bottom is connected with the hot air gun, and hot air gun one side is provided with the solder paste syringe needle, installs first backup pad and second backup pad on the workstation symmetry, installs follower in the first backup pad, installs slewing mechanism in the second backup pad, and slewing mechanism is connected with fixture.
Preferably, the round groove is formed in the middle of the first supporting plate, a welding frame is arranged on one side of the round groove, one end of the follow-up mechanism is arranged on the welding frame, and the other end of the follow-up mechanism is in plug-in fit in the round groove.
Preferably, the follower mechanism comprises a first motor mounted on the weld carrier.
And one end of the rotating rod is connected with the first motor.
The rotary table is arranged at the other end of the rotary rod and is in sliding connection with the inner wall of the circular groove.
The wire hole is formed at the edge of the turntable.
Preferably, the rotation mechanism includes a second motor mounted at one side of the second support plate.
The connecting plate is arranged on the other side of the second supporting plate and is connected with the transmission end of the second motor.
And the two connecting rods are symmetrically arranged on the connecting plate, and the other ends of the two connecting rods are respectively connected to two sides of the clamping mechanism.
Preferably, the clamping mechanism comprises a clamping frame, which is connected with the two connecting rods.
And the two connecting blocks are welded on two sides of the clamping frame respectively and are connected with the corresponding connecting rods respectively.
The cylinder is arranged in the middle of the bottom end of the clamping frame.
One end of the push rod is connected with the cylinder.
The push plate is arranged at the other end of the push rod.
And the two sliding sleeves are symmetrically sleeved on the push plate.
One end of each first movable rod is movably connected with the top end of the corresponding sliding sleeve.
And each clamping jaw is symmetrically and slidably arranged on the clamping frame and is respectively connected with the other end of the corresponding first movable rod.
And one end of each second movable rod is movably connected with the bottom end of the corresponding sliding sleeve, and the other end of each second movable rod is movably connected with the clamping frame.
And each guide block is symmetrically welded on the clamping frame and is respectively in sliding fit with the corresponding clamping jaw.
Preferably, the guide block is provided with a guide hole, and the bottom ends of the clamping jaws are slidably inserted into the guide hole.
Compared with the prior art, the utility model has the beneficial effects that:
1. compared with the prior art, the welding aviation plug can be clamped through the arrangement of the support, the connecting block, the air cylinder, the push rod, the push plate, the sliding sleeve, the first movable rod, the clamping jaw, the second movable rod and the guide block, so that the influence of wind power generated by the hot air gun on the position of the aviation plug is avoided, the stability of the aviation plug in the welding process is improved, and the welding quality is ensured;
2. through the setting of first motor, bull stick, carousel, line hole, second motor, connecting plate and connecting rod, compare with prior art, can rotate the plug to realize the annular welding to the plug, make the welding of plug more comprehensive, it is more firm, and can prevent the line body of plug connection along with removing, thereby prevent that the line body from taking place the winding phenomenon.
Drawings
Fig. 1 is a schematic diagram of the overall structure of the present utility model.
Fig. 2 is a schematic diagram of a connection structure between a clamping mechanism and a rotating mechanism according to the present utility model.
Figure 3 is a schematic view of the structure of the clamping mechanism of the present utility model,
fig. 4 is a schematic structural view of the follower mechanism of the present utility model.
In the figure: 1. a work table; 2. a bracket; 3. welding the assembly; 4. a heat gun; 5. a solder paste needle; 6. a first support plate; 7. a follower mechanism; 701. a first motor; 702. a rotating rod; 703. a turntable; 704. a wire hole; 8. a second support plate; 9. a rotating mechanism; 901. a second motor; 902. a connecting plate; 903. a connecting rod; 10. a clamping mechanism; 1001. a clamping frame; 1002. a connecting block; 1003. a cylinder; 1004. a push rod; 1005. a push plate; 1006. a sliding sleeve; 1007. a first movable lever; 1008. a clamping jaw; 1009. a second movable rod; 1010. and a guide block.
Detailed Description
The present utility model will be described in further detail with reference to the drawings and examples, in order to make the objects, technical solutions and advantages of the present utility model more apparent. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the utility model.
The aviation plug hot air welding device comprises a workbench 1, a support 2, a welding assembly 3, a hot air gun 4, a solder paste needle 5, a first support plate 6, a follow-up mechanism 7, a second support plate 8, a rotating mechanism 9 and a clamping mechanism 10, wherein the support 2 is arranged at the top end of the workbench 1, the welding assembly 3 is supported at the top end of the support 2, the bottom end of the welding assembly 3 is connected with the hot air gun 4, the solder paste needle 5 is arranged on one side of the hot air gun 4, the first support plate 6 and the second support plate 8 are symmetrically arranged on the workbench 1, the follow-up mechanism 7 is arranged on the first support plate 6, the rotating mechanism 9 is arranged on the second support plate 8, and the rotating mechanism 9 is connected with the clamping mechanism 10.
Further, the circular groove is formed in the middle of the first supporting plate 6, a welding frame is arranged on one side of the circular groove, one end of the follow-up mechanism 7 is installed on the welding frame, the other end of the follow-up mechanism is in plug-in fit in the circular groove, so that a wire body connected with the plug is supported, and the wire body is kept flush with the aviation plug.
Further, the follower 7 includes a first motor 701, and the first motor 701 is mounted on a welding carriage.
The rotating rod 702, the rotating rod 702 one end is connected with the first motor 701.
The carousel 703, carousel 703 is installed at the bull stick 702 other end, and carousel 703 and circular slot inner wall sliding engagement.
Wire holes 704, the wire holes 704 are formed at the edge of the turntable 703.
In order to prevent the wire body connected with the plug from winding in the rotating process, the first motor 701 in the follower 7 synchronously runs with the second motor 901, so that the rotating rod 702 rotates, and the rotating disc 703 rotates along with the rotation, so that the wire hole 704 is always matched with the position of the plug at the center horizontally.
Further, the rotation mechanism 9 includes a second motor 901, and the second motor 901 is mounted on the side of the second support plate 8.
The connecting plate 902, the connecting plate 902 is arranged on the other side of the second supporting plate 8 and is connected with the driving end of the second motor 901.
Two connecting rods 903, each connecting rod 903 is symmetrically installed on the connecting plate 902, and the other ends of the two connecting rods 903 are respectively connected to two sides of the clamping mechanism 10.
When the plug is subjected to omnibearing welding, the second motor 901 operates, so that the connecting plate 902 rotates, the connecting rods 903 rotate along with the rotation, the clamping mechanism 10 rotates along with the rotation under the connection of the two connecting rods 903, the plug clamped on the clamping mechanism 10 rotates, and the hot air gun 4 with the shafting moving at the top end and the solder paste needle 5 move along with the rotation of the plug in a matched manner, so that the plug is subjected to annular welding.
Further, the clamping mechanism 10 comprises a clamping frame 1001, and the clamping frame 1001 is connected to two connecting rods 903.
Two connection blocks 1002, each connection block 1002 is welded on both sides of the clamping frame 1001, and the two connection blocks 1002 are connected with the corresponding connection rods 903, respectively.
The cylinder 1003, the cylinder 1003 is installed in the middle of the bottom end of the holder 1001.
A push rod 1004, and one end of the push rod 1004 is connected with a cylinder 1003.
A push plate 1005, the push plate 1005 being mounted on the other end of the push rod 1004.
Two sliding sleeves 1006, each sliding sleeve 1006 is symmetrically sleeved on the push plate 1005.
And one end of each first movable rod 1007 is movably connected with the top end of the corresponding sliding sleeve 1006.
Two clamping jaws 1008, each clamping jaw 1008 is symmetrically and slidingly arranged on the clamping frame 1001 and is respectively connected with the other end of the corresponding first movable rod 1007.
And one end of each second movable rod 1009 is movably connected with the bottom end of the corresponding sliding sleeve 1006, and the other end of each second movable rod 1009 is movably connected with the clamping frame 1001.
Two guide blocks 1010, each guide block 1010 is symmetrically welded on the clamping frame 1001 and is in sliding fit with the corresponding clamping jaw 1008.
When the aviation plug is clamped, the air cylinder 1003 operates, so that the push rod 1004 pushes the push plate 1005, two sliding sleeves 1006 sleeved on the push plate 1005 synchronously move towards the middle of the push plate 1005 under the connection of the second movable rod 1009, so that the two first movable rods 1007 are stressed, the two first movable rods 1007 push the two clamping jaws 1008, and the two clamping jaws 1008 are close to each other to clamp the aviation plug under the guidance of the two guide blocks 1010.
Further, the guide block 1010 is provided with a guide hole, and the bottom end of the clamping jaw 1008 is slidably inserted into the guide hole, so that the bottom position of the clamping jaw 1008 is limited, and the clamping jaw 1008 can move.
The working principle of the utility model is as follows: when the aviation plug hot air welding device is used for welding an aviation plug, the air cylinder 1003 operates, so that the push rod 1004 pushes the push plate 1005, two sliding sleeves 1006 sleeved on the push plate 1005 synchronously move towards the middle part of the push plate 1005 under the connection of the second movable rod 1009, so that the two first movable rods 1007 are stressed, the two first movable rods 1007 push the two clamping jaws 1008, the two clamping jaws 1008 are close to each other to clamp the aviation plug under the guidance of the two guide blocks 1010, and then a wire body connected with one end of the plug is inserted into a wire hole 704 formed in the rotary table 703;
in the welding process, the second motor 901 operates to enable the connecting plate 902 to rotate, so that the connecting rods 903 rotate along with the rotation, the clamping mechanism 10 rotates along with the rotation under the connection of the two connecting rods 903, so that the plug clamped on the clamping mechanism 10 rotates, and the hot air gun 4 with shafting movement at the top end and the solder paste needle 5 move along with the rotation of the plug in a matched manner, so that the plug is subjected to annular welding;
in order to prevent the wire body connected with the plug from winding in the rotating process, the first motor 701 in the follower 7 synchronously runs with the second motor 901, so that the rotating rod 702 rotates, and the rotating disc 703 rotates along with the rotation, so that the wire hole 704 is always matched with the position of the plug at the extreme center and horizontally.
The utility model has the advantages that the aviation plug can be clamped and fixed, so that welding is more stable, bad generation is prevented, and meanwhile, the aviation plug can be rotated, so that the aviation plug can be subjected to annular welding, and the welding efficiency is improved.
The foregoing description of the preferred embodiments of the utility model is not intended to be limiting, but rather is intended to cover all modifications, equivalents, and alternatives falling within the spirit and principles of the utility model.
Claims (6)
1. The utility model provides an aviation plug hot air welding device, includes workstation, support, welding set, hot air gun, solder paste syringe needle, first backup pad, follower, second backup pad, slewing mechanism and fixture, its characterized in that: the welding device comprises a workbench, and is characterized in that a support is arranged at the top end of the workbench, a welding assembly is supported at the top end of the support, a hot air gun is connected to the bottom end of the welding assembly, a solder paste needle is arranged on one side of the hot air gun, a first support plate and a second support plate are symmetrically arranged on the workbench, a follow-up mechanism is arranged on the first support plate, a rotating mechanism is arranged on the second support plate, and a clamping mechanism is connected to the rotating mechanism.
2. An aircraft plug hot air welding apparatus according to claim 1, wherein: the round groove is formed in the middle of the first supporting plate, a welding frame is arranged on one side of the round groove, one end of the follow-up mechanism is arranged on the welding frame, and the other end of the follow-up mechanism is in plug-in fit with the round groove.
3. An aircraft plug hot air welding apparatus according to claim 1, wherein: the follow-up mechanism comprises a first motor, and the first motor is arranged on the welding frame;
one end of the rotating rod is connected with the first motor;
the rotary table is arranged at the other end of the rotary rod and is in sliding connection with the inner wall of the circular groove;
and the wire hole is formed in the edge of the turntable.
4. An aircraft plug hot air welding apparatus according to claim 1, wherein: the rotating mechanism comprises a second motor, and the second motor is arranged at one side of a second supporting plate;
the connecting plate is arranged on the other side of the second supporting plate and is connected with the second motor transmission end;
and the two connecting rods are symmetrically arranged on the connecting plate, and the other ends of the two connecting rods are respectively connected to two sides of the clamping mechanism.
5. An aircraft plug hot air welding apparatus according to claim 1, wherein: the clamping mechanism comprises a clamping frame, and the clamping frame is connected with two connecting rods;
the two connecting blocks are welded on two sides of the clamping frame respectively and are connected with the corresponding connecting rods respectively;
the air cylinder is arranged in the middle of the bottom end of the clamping frame;
one end of the push rod is connected with the air cylinder;
the push plate is arranged at the other end of the push rod;
the two sliding sleeves are symmetrically sleeved on the push plate;
one end of each first movable rod is movably connected with the top end of the corresponding sliding sleeve;
the clamping jaws are symmetrically and slidably arranged on the clamping frame and are respectively connected with the other end of the corresponding first movable rod;
one end of each second movable rod is movably connected with the bottom end of the corresponding sliding sleeve, and the other end of each second movable rod is movably connected with the clamping frame;
and the two guide blocks are symmetrically welded on the clamping frame respectively and are in sliding fit with the corresponding clamping jaws respectively.
6. An aircraft plug hot air welding apparatus according to claim 5, wherein: the guide block is provided with a guide hole, and the bottom ends of the clamping jaws are slidably inserted into the guide hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321122917.XU CN219746583U (en) | 2023-05-11 | 2023-05-11 | Aviation plug hot air welding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321122917.XU CN219746583U (en) | 2023-05-11 | 2023-05-11 | Aviation plug hot air welding device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219746583U true CN219746583U (en) | 2023-09-26 |
Family
ID=88086725
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321122917.XU Active CN219746583U (en) | 2023-05-11 | 2023-05-11 | Aviation plug hot air welding device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219746583U (en) |
-
2023
- 2023-05-11 CN CN202321122917.XU patent/CN219746583U/en active Active
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