Multifunctional support for aviation plug welding

By designing a multi-functional bracket, the problem of reliance on operator experience in aviation plug welding was solved, enabling fast and precise welding, reducing quality accidents, improving production efficiency, and the modular design is flexible and highly adaptable.

CN223932774UActive Publication Date: 2026-02-24HARBIN ELECTRIC GRP OCEAN INTELLIGENT EQUIP CO LTD
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Patent Information

Application Number
CN202520352904.4
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-03-03
Publication Date
2026-02-24
Estimated Expiration
2035-03-03

AI Technical Summary

Technical Problem

In existing technologies, welding of aviation plugs relies on the operator's experience and hand stability, resulting in inconsistent welding quality and difficulty in performing the work quickly and accurately.

Method used

Design a multi-functional stand, including a lifting structure, an angle adjustment structure, a support block, a U-shaped clamping groove, and a clamping rod, for holding wires, aviation plugs, and soldering irons, and providing multiple operating modes to assist soldering.

Benefits of technology

It enables fast and precise welding of aviation plugs, reduces quality accidents, improves production progress, and its modular design allows for upgrades and improvements as needed, while being cost-effective and easy to operate.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides a multifunctional support for aviation plug welding, and belongs to the technical field of clamps. The problems that in the prior art, the welding mode of the aviation plug depends on the experience and hand stability of an operator, and welding operation cannot be rapidly and accurately conducted are solved. The device comprises a base, a connecting block, a lifting structure, an angle adjusting structure, a supporting block, a supporting frame, a first abutting rod and a second abutting rod, the connecting block is connected with the base through the lifting structure, the lifting structure can adjust the height of the connecting block, the supporting block is connected with the connecting block through the angle adjusting structure, and the angle adjusting structure can adjust the angle of the supporting block relative to the connecting block; the supporting block is provided with a U-shaped clamping groove and a containing hole in a spaced mode, the first abutting rod is in threaded connection with the supporting frame and can ascend and descend in the depth direction of the U-shaped clamping groove, and the second abutting rod is in threaded connection with the supporting block and extends into the containing hole in the radial direction of the containing hole. The aviation plug welding device can assist in rapid and accurate aviation plug welding.
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Description

Technical Field

[0001] This utility model belongs to the field of clamping technology, and in particular relates to a multifunctional bracket for welding aviation plugs. Background Technology

[0002] Aviation connectors are a type of connector used to connect electrical circuits. Also known as plug sockets, they are widely used in various electrical circuits to connect or disconnect circuits. The quality of the soldering of aviation connectors affects their stability and reliability; good soldering quality maximizes the connector's functionality. Therefore, the soldering quality of aviation connectors plays a crucial role in the stability of the entire product's electrical unit, and its importance is self-evident.

[0003] Soldering aviation connectors involves soldering the wires and the wires to the connector contacts. Soldering the connector contacts at the rear end to the wires is the most crucial step in assembly. Since the contacts connect to the front pins, any weak or incomplete soldering directly affects the quality of the connector. Furthermore, because the contacts vary in size and thickness, requiring different heating times with the soldering iron, and because adjacent contacts are very close together in a confined space, and because the connector must be wrapped with heat-shrink tubing after soldering to prevent solder burrs, contact soldering demands exceptional skill and experience from the operator.

[0004] In existing technologies, the common operating method involves the operator using both hands: the left hand holds the wire and solder wire, while the right hand holds the soldering iron, performing the soldering simultaneously. However, this method requires a high level of experience and hand stability from the operator. If the operator lacks relevant experience, quality problems such as incomplete soldering or weak welds are prone to occur during the soldering process, which will seriously delay production progress.

[0005] Therefore, there is an urgent need for a tool that can quickly and accurately perform welding of aviation plugs. Utility Model Content

[0006] In view of this, in order to solve the problem that the welding method of aviation plugs in the prior art relies on the operator's experience and hand stability, and cannot be performed quickly and accurately, this utility model proposes a multi-functional bracket for welding aviation plugs.

[0007] To achieve the above objectives, the present invention adopts the following technical solution:

[0008] A multi-functional bracket for aircraft plug soldering, comprising:

[0009] The base, connecting block, and lifting structure are included. The connecting block is connected to the base via the lifting structure, which allows the height of the connecting block to be adjusted.

[0010] An angle adjustment structure and a support block are provided. The support block is connected to the connecting block through the angle adjustment structure. The angle adjustment structure can adjust the angle of the support block relative to the connecting block. The support block is provided with U-shaped grooves and receiving holes at intervals.

[0011] The support frame and the first clamping rod are connected to the support block through an angle adjustment structure. The first clamping rod is screwed to the support frame and can move up and down along the depth direction of the U-shaped groove.

[0012] The second abutting rod is screwed to the support block and extends into the receiving hole radially.

[0013] As a preferred embodiment of the aforementioned multifunctional bracket for welding aviation plugs, the lifting structure includes a lifting screw, a first lifting nut, and a second lifting nut. The lifting screw is fixedly mounted on the base, and a connecting block is screwed onto the lifting screw. Both the first and second lifting nuts are screwed onto the lifting screw. The upper part of the connecting block abuts against the first lifting nut, and the lower part of the connecting block abuts against the second lifting nut.

[0014] As a preferred embodiment of the aforementioned multifunctional bracket for welding aviation plugs, the lifting structure further includes a first fixing nut, one end of the lifting screw is screwed to the base, the first fixing nut is screwed to the lifting screw, and the first fixing nut is abutted against the base.

[0015] As a preferred embodiment of the aforementioned multifunctional bracket for welding aviation plugs, the angle adjustment structure includes a rotating screw and an adjusting nut. The rotating screw is fixedly mounted on the connecting block, and the adjusting nut, support frame, and support block are all screwed to the rotating screw. The two ends of the support frame are respectively abutted against the adjusting nut and the support block.

[0016] As a preferred embodiment of the aforementioned multifunctional bracket for welding aviation plugs, the angle adjustment structure further includes a second fixing nut, one end of the rotating screw is screwed to the connecting block, the second fixing nut is screwed to the rotating screw, and the second fixing nut is pressed against the connecting block.

[0017] As a preferred embodiment of the aforementioned multifunctional bracket for welding aviation plugs, the multifunctional bracket for welding aviation plugs further includes a pad, which is located between the first clamping rod and the bottom wall of the U-shaped clamping groove.

[0018] As a preferred embodiment of the aforementioned multifunctional bracket for welding aviation plugs, a rubber pad is provided at one end of the second clamping rod that extends into the receiving hole.

[0019] As a preferred embodiment of the aforementioned multifunctional bracket for welding aviation plugs, the base, the connecting block, and the support block are all made of wood.

[0020] As a preferred embodiment of the aforementioned multifunctional bracket for welding aviation plugs, the inner wall of the U-shaped clamping groove is provided with anti-slip texture.

[0021] As a preferred embodiment of the aforementioned multifunctional bracket for welding aviation plugs, the base is provided with a connecting structure that can be connected to the connecting structure of the base of another multifunctional bracket for welding aviation plugs.

[0022] Compared with the prior art, the beneficial effects of the multifunctional bracket for aviation plug welding provided by this utility model are:

[0023] This utility model provides a multi-functional bracket for soldering aviation plugs. This bracket assists in the soldering of aviation plugs with multiple functions. The first function is clamping the wires. The operation method is as follows: the operator adjusts the height and angle of the support block to a convenient height and angle for soldering using the lifting and angle adjustment structures. Multiple loose wires are threaded into the U-shaped clamping groove. The first clamping rod is rotated to move downwards until the multiple wires are clamped. Then, the operator holds the solder wire in the left hand and the soldering iron in the right hand to solder the exposed wires. After soldering, it is easy to observe whether the solder is sufficient. This allows the operator to fully and reasonably utilize both hands simultaneously, avoiding insufficient solder that could lead to subsequent soldering problems.

[0024] The second function is to clamp the aviation plug. The operation method is as follows: the operator adjusts the height and angle of the support block to a height and angle that is convenient for soldering through the lifting structure and angle adjustment structure, places the aviation plug in the receiving hole and uses the first clamping rod to press against the side wall of the aviation plug so that the aviation plug is fixed in the receiving hole and the rear end of the aviation plug is exposed outside the receiving hole. The operator first solders the cup corner, then holds the wire in the left hand and the soldering iron in the right hand to solder the cup corner to the wire. After the soldering is completed, it is convenient to observe whether there is a cold solder joint or the soldering is not firm.

[0025] The third function is to hold the soldering iron. The operation method is as follows: the operator adjusts the height and angle of the support block to a height and angle that is convenient for soldering by using the lifting structure and the angle adjustment structure. The soldering iron is inserted into the receiving hole and the first clamping rod is used to press against the side wall of the soldering iron to fix the soldering iron in the receiving hole. The operator holds the wire to perform wire soldering.

[0026] The fourth function is to clamp the vulcanized cable. The operation method is as follows: use two multi-functional brackets for aviation plug welding, fix the two sides of the cable in the U-shaped clamping grooves of the two multi-functional brackets for aviation plug welding respectively, adjust the height and angle so that the cable is horizontal and the exposed part of the cable is in the middle position of the two multi-functional brackets for aviation plug welding, and then vulcanize it. This function can easily fix the vulcanized cable.

[0027] This multi-functional bracket for welding aviation plugs can assist in the rapid and precise welding of aviation plugs, greatly reducing quality accidents and improving production progress. The modular design allows for the upgrading and improvement of the mounted module head according to production task requirements, and it is also inexpensive to manufacture and easy to operate. Attached Figure Description

[0028] The accompanying drawings, which form part of this utility model, are used to provide a further understanding of the utility model. The illustrative embodiments of the utility model and their descriptions are used to explain the utility model and do not constitute an undue limitation of the utility model. In the drawings:

[0029] Figure 1 This is a structural schematic diagram of a multifunctional bracket for welding aviation plugs provided in a specific embodiment of this utility model.

[0030] In the picture:

[0031] 1. Base;

[0032] 21. Lifting screw; 22. First lifting nut; 23. Second lifting nut; 24. First fixing nut;

[0033] 3. Connecting block;

[0034] 41. Rotate the screw; 42. Adjust the nut; 43. Second fixing nut;

[0035] 5. Support block;

[0036] 6. U-shaped clamping groove;

[0037] 7. Receiving hole;

[0038] 8. Support frame;

[0039] 9. First clamping rod;

[0040] 10. Second clamping rod. Detailed Implementation

[0041] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. It should be noted that, unless otherwise specified, the embodiments and features in the embodiments of the present utility model can be combined with each other, and the described embodiments are only some embodiments of the present utility model, not all embodiments.

[0042] In the description of this utility model, unless otherwise explicitly specified and limited, the terms "connected," "linked," and "fixed" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral part; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal communication of two components or the interaction between two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0043] In this invention, unless otherwise explicitly specified and limited, "above" or "below" the second feature can include direct contact between the first and second features, or contact between the first and second features through another feature between them. Furthermore, "above," "over," and "on top" of the second feature includes the first feature directly above or diagonally above the second feature, or simply indicates that the first feature is at a higher horizontal level than the second feature. "Below," "below," and "under" the second feature includes the first feature directly below or diagonally below the second feature, or simply indicates that the first feature is at a lower horizontal level than the second feature.

[0044] In the description of this embodiment, the terms "upper," "lower," "right," etc., refer to the orientation or positional relationship shown in the accompanying drawings. They are used only for ease of description and simplification of operation, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model. In addition, the terms "first" and "second" are only used for distinction in description and have no special meaning.

[0045] See Figure 1 This invention provides a multifunctional bracket for welding aviation plugs. The bracket includes a base 1, a connecting block 3, a lifting structure, an angle adjustment structure, a support block 5, a support frame 8, a first clamping rod 9, and a second clamping rod 10. The connecting block 3 is connected to the base 1 via the lifting structure, which adjusts the height of the connecting block 3. The support block 5 is connected to the connecting block 3 via the angle adjustment structure, which adjusts the angle of the support block 5 relative to the connecting block 3. The support block 5 is provided with U-shaped grooves 6 and receiving holes 7 spaced apart. The support frame 8 is connected to the support block 5 via the angle adjustment structure. The first clamping rod 9 is screwed to the support frame 8 and can move up and down along the depth direction of the U-shaped grooves 6. The second clamping rod 10 is screwed to the support block 5 and extends radially into the receiving hole 7.

[0046] This multi-functional bracket for soldering aviation connectors offers several advantages during the soldering process. The first function is clamping the wires. The operation involves the operator adjusting the height and angle of the support block 5 using the lifting and angle adjustment mechanisms to a convenient soldering position. Multiple loose wires are then threaded into the U-shaped clamping groove 6. The first clamping rod 9 is rotated downwards until it clamps the wires securely. The operator then holds the solder wire in their left hand and the soldering iron in their right hand to solder the exposed wires. After soldering, it is easy to check if sufficient solder has been applied. This design allows the operator to utilize both hands effectively, preventing insufficient solder from causing problems in subsequent soldering operations.

[0047] The second function is to clamp the aviation connector. The operation method is as follows: The operator adjusts the height and angle of the support block 5 to a convenient height and angle for soldering using the lifting and angle adjustment mechanisms. The aviation connector is placed in the receiving hole 7, and the first clamping rod 9 is used to press against the side wall of the aviation connector, fixing it within the receiving hole 7 with the rear end of the connector protruding outside. The operator first solders the cup corner, then holds the wire in their left hand and the soldering iron in their right hand to solder the cup corner to the wire. After soldering, it is easy to observe whether there is a cold solder joint or a weak solder joint. The third function is to clamp the soldering iron. The operation method is as follows: The operator adjusts the height and angle of the support block 5 to a convenient height and angle for soldering using the lifting and angle adjustment mechanisms. The soldering iron is inserted into the receiving hole 7, and the first clamping rod 9 is used to press against the side wall of the soldering iron, fixing it within the receiving hole 7. The operator then holds the wire to perform wire bonding.

[0048] The fourth function is to clamp the vulcanized cable. The operation method is as follows: use two multi-functional brackets for aviation plug welding, fix the two sides of the cable in the U-shaped clamping grooves 6 of the two multi-functional brackets for aviation plug welding respectively, adjust the height and angle so that the cable is horizontal and the exposed part of the cable is in the middle position of the two multi-functional brackets for aviation plug welding, and then vulcanize it. This function can easily fix the vulcanized cable.

[0049] This multi-functional bracket for welding aviation plugs can assist in the rapid and precise welding of aviation plugs, greatly reducing quality accidents and improving production progress. The modular design allows for the upgrading and improvement of the mounted module head according to production task requirements, and it is also inexpensive to manufacture and easy to operate.

[0050] Optionally, the lifting structure includes a lifting screw 21, a first lifting nut 22, and a second lifting nut 23. The lifting screw 21 is fixedly mounted on the base 1, and the connecting block 3 is screwed onto the lifting screw 21. Both the first lifting nut 22 and the second lifting nut 23 are screwed onto the lifting screw 21. The upper part of the connecting block 3 abuts against the first lifting nut 22, and the lower part of the connecting block 3 abuts against the second lifting nut 23. When the height needs to be adjusted, simply rotate the first lifting nut 22, the connecting block 3, and the second lifting nut 23 respectively to adjust the height of the connecting block 3, thereby adjusting the height of the support block 5.

[0051] Optionally, the lifting structure also includes a first fixing nut 24. One end of the lifting screw 21 is screwed to the base 1, and the first fixing nut 24 is screwed to the lifting screw 21, and the first fixing nut 24 abuts against the base 1. This can fix the lifting screw 21 to the base 1.

[0052] Optionally, the angle adjustment structure includes a rotating screw 41 and an adjusting nut 42. The rotating screw 41 is fixedly mounted on the connecting block 3. The adjusting nut 42, the support frame 8, and the support block 5 are all screwed to the rotating screw 41. The two ends of the support frame 8 are respectively pressed against the adjusting nut 42 and the support block 5. When the angle needs to be adjusted, simply rotate the adjusting nut 42 and the support block 5. First, rotate the adjusting nut 42 away from the support block 5, then rotate the support block 5 to the required angle, and then rotate the adjusting nut 42 closer to the support block 5 to lock the support block 5. Similarly, the angle of the support frame 8 can also be adjusted. By adjusting the angle of the support frame 8, the angle of the first clamping rod 9 relative to the U-shaped clamping groove 6 can be adjusted. When it is necessary to clamp the wire, the first clamping rod 9 is adjusted so that its extension direction is perpendicular to the extension direction of the U-shaped clamping groove 6. It can be understood that when clamping the wire, the extension direction of the wire is opposite to the extension direction of the U-shaped clamping groove 6.

[0053] Optionally, the angle adjustment structure further includes a second fixing nut 43. One end of the rotating screw 41 is screwed to the connecting block 3, and the second fixing nut 43 is screwed to the rotating screw 41, with the second fixing nut 43 abutting against the connecting block 3. This fixes the rotating screw 41 onto the connecting block 3.

[0054] Optionally, the multi-functional bracket for welding aviation plugs also includes a pad located between the first clamping rod 9 and the bottom wall of the U-shaped clamping groove 6. The first clamping rod 9 abuts against the pad, allowing multiple wires to be clamped between the pad and the U-shaped clamping groove 6, improving clamping stability.

[0055] Optionally, the end of the second clamping rod 10 that extends into the receiving hole 7 is provided with a rubber pad. This prevents damage to the aviation connector.

[0056] Optionally, the base 1, connecting block 3, and support block 5 are all made of wood.

[0057] Optionally, the inner wall of the U-shaped groove 6 is provided with anti-slip texture. This can improve the friction between the wire and the U-shaped groove 6.

[0058] Optionally, base 1 is provided with a connecting structure that can be connected to the connecting structure of another multi-functional bracket for aircraft plug soldering. When two multi-functional brackets for aircraft plug soldering are required, connecting the two bases 1 via the connecting structure improves operational stability.

[0059] Obviously, the above-disclosed embodiments of the present invention are merely for illustrating the present invention. The embodiments do not exhaustively describe all details, nor do they limit the present invention to specific implementations. Many modifications and variations can be made based on the content of this specification. This specification selects and specifically describes these embodiments to better explain the principles and practical applications of the present invention, thereby enabling those skilled in the art to better understand and utilize the present invention. It is neither necessary nor possible to exhaustively describe all implementation methods here.

Claims

1. A multifunctional bracket for welding aviation plugs, characterized in that, include: The base (1), the connecting block (3) and the lifting structure are provided. The connecting block (3) is connected to the base (1) through the lifting structure. The lifting structure can adjust the height of the connecting block (3). An angle adjustment structure and a support block (5) are provided. The support block (5) is connected to the connecting block (3) through the angle adjustment structure. The angle adjustment structure can adjust the angle of the support block (5) relative to the connecting block (3). The support block (5) is provided with U-shaped grooves (6) and receiving holes (7) at intervals. The support frame (8) and the first abutting rod (9) are connected to the support block (5) through an angle adjustment structure. The first abutting rod (9) is screwed to the support frame (8). The first abutting rod (9) can move up and down along the depth direction of the U-shaped groove (6). The second abutting rod (10) is screwed to the support block (5) and extends into the receiving hole (7) radially.

2. The multifunctional bracket for welding aviation plugs according to claim 1, characterized in that: The lifting structure includes a lifting screw (21), a first lifting nut (22), and a second lifting nut (23). The lifting screw (21) is fixedly installed on the base (1). The connecting block (3) is screwed to the lifting screw (21). The first lifting nut (22) and the second lifting nut (23) are both screwed to the lifting screw (21). The upper part of the connecting block (3) abuts against the first lifting nut (22), and the lower part of the connecting block (3) abuts against the second lifting nut (23).

3. The multifunctional bracket for welding aviation plugs according to claim 2, characterized in that: The lifting structure also includes a first fixing nut (24), one end of the lifting screw (21) is screwed to the base (1), the first fixing nut (24) is screwed to the lifting screw (21), and the first fixing nut (24) abuts against the base (1).

4. The multifunctional bracket for welding aviation plugs according to claim 1, characterized in that: The angle adjustment structure includes a rotating screw (41) and an adjusting nut (42). The rotating screw (41) is fixedly mounted on the connecting block (3). The adjusting nut (42), the support frame (8), and the support block (5) are all screwed to the rotating screw (41). The two ends of the support frame (8) are respectively pressed against the adjusting nut (42) and the support block (5).

5. The multifunctional bracket for welding aviation plugs according to claim 4, characterized in that: The angle adjustment structure also includes a second fixing nut (43), one end of the rotating screw (41) is screwed to the connecting block (3), the second fixing nut (43) is screwed to the rotating screw (41), and the second fixing nut (43) abuts against the connecting block (3).

6. The multifunctional bracket for welding aviation plugs according to claim 1, characterized in that: It also includes a pad, which is located between the first clamping rod (9) and the bottom wall of the U-shaped groove.

7. The multifunctional bracket for welding aviation plugs according to claim 1, characterized in that: The second abutting rod (10) has a rubber pad at one end that extends into the receiving hole (7).

8. The multifunctional bracket for welding aviation plugs according to claim 1, characterized in that: The base (1), the connecting block (3), and the support block (5) are all made of wood.

9. The multifunctional bracket for welding aviation plugs according to claim 1, characterized in that: The inner wall of the U-shaped groove (6) is provided with anti-slip texture.

10. The multifunctional bracket for welding aviation plugs according to claim 1, characterized in that: The base (1) is provided with a connecting structure that can be connected to the connecting structure of another base (1) of the multifunctional bracket for welding aviation plugs.