A kind of aviation plug connector forming device

Abstract

The present invention belongs to the technical field of aviation connector molding, and specifically relates to an aviation connector molding device, comprising a molding cylinder, a maintenance cylinder, a grinding repair mechanism, and a rotary bulging mechanism. The maintenance cylinder is disposed between the upper and bottom walls of the molding cylinder, and the maintenance cylinder is provided through the molding cylinder. The grinding repair mechanism is disposed on the maintenance cylinder, and the rotary bulging mechanism is disposed on the inner wall of the molding cylinder. The grinding repair mechanism includes an assembly mechanism and a rotary grinding mechanism. The present invention provides an aviation connector molding device that can detect and repair surface depressions of aviation connector pins during grinding operations.

Description

Technical Field

[0001] The present invention belongs to the technical field of aviation plug connector molding, and in particular relates to an aviation plug connector molding device. Background Art

[0002] Aviation connectors are a common component in electronic engineering. Their function is simple: to bridge blocked or isolated circuits within a circuit, allowing current to flow and the circuit to achieve its intended function.

[0003] The existing aviation connector molding device has the following problems:

[0004] When repairing the pin depression of the aviation plug connector, the existing aviation plug connector forming device mostly adopts a manual knocking method. The above method is likely to damage other parts of the aviation plug connector pin depression, which increases the deformation area of ​​the aviation plug connector pin, resulting in a decrease in the quality of the aviation plug connector pin transmitting signal, resulting in the pin being scrapped, reducing the repair and forming efficiency of the aviation plug connector. Therefore, it cannot meet the existing use requirements of the aviation plug connector forming device. Summary of the Invention

[0005] In view of the above situation, in order to overcome the defects of the prior art, the present invention provides an aviation plug connector forming device that can detect and repair the depressions on the surface of the aviation plug connector when grinding the pins of the aviation plug connector.

[0006] The technical solution adopted in this scheme is as follows: This scheme proposes an aviation plug connector forming device, including a forming cylinder, a maintenance cylinder, a grinding type repair mechanism and a rotary measuring type bulging mechanism. The maintenance cylinder is arranged between the upper wall and the bottom wall of the forming cylinder, and the maintenance cylinder is arranged through. The grinding type repair mechanism is arranged on the maintenance cylinder, and the rotary measuring type bulging mechanism is arranged on the inner wall of the forming cylinder. The grinding type repair mechanism includes an assembly mechanism and a rotary grinding mechanism. The assembly mechanism is arranged on the upper wall of the forming cylinder, and the rotary grinding mechanism is arranged on the side wall of the maintenance cylinder. The rotary measuring type bulging mechanism includes a distance measuring mechanism and a heat conducting mechanism. The distance measuring mechanism is arranged on the inner wall of the forming cylinder, and the heat conducting mechanism is arranged on the side of the distance measuring mechanism close to the maintenance cylinder.

[0007] As a further preferred embodiment of the present invention, the assembly mechanism includes a threaded hole, a threaded block, a bottom rubber block, a top rubber block, a clamping port and an aviation connector pin. The threaded hole is provided on the bottom wall of the forming cylinder, the threaded block is provided inside the threaded hole, the threaded block is threadedly connected to the threaded hole, the bottom rubber block is rotatably provided on the upper wall of the threaded block, the top rubber block is rotatably provided on the top inner wall of the forming cylinder, the bottom rubber block and the top rubber block are arranged opposite to each other, the clamping ports are respectively provided on the side of the bottom rubber block away from the threaded block and the side of the top rubber block away from the top inner wall of the forming cylinder, the clamping ports are arranged opposite to each other, the aviation connector pin is provided between the clamping ports, and the diameter of the clamping port is smaller than that of the aviation connector The diameter of the device pin; the rotary grinding mechanism includes a driving motor, a guide column, a grinding plate, a sponge grinding layer, a grinding heat-resistant electromagnet, a limiting iron block and an expansion spring, the driving motor is arranged on the upper wall of the forming cylinder, the power end of the driving motor passes through the forming cylinder and is connected to the top rubber block, multiple groups of guide columns are arranged through the side wall of the maintenance cylinder, the grinding plate is arranged on the side wall of the guide column inside the maintenance cylinder, the sponge grinding layer is arranged on the side of the grinding plate away from the guide column, the sponge grinding layers are arranged relatively, the grinding heat-resistant electromagnet is arranged on the side wall of the maintenance cylinder outside the guide column, the limiting iron block is arranged on the side of the guide column away from the grinding plate, and the expansion spring is arranged between the maintenance cylinder outside the guide column and the limiting iron block.

[0008] When in use, rotate the threaded block, the threaded block is unscrewed from the threaded hole, and the aviation connector pin is inserted into the clamping hole on the upper wall of the bottom rubber block. Since the diameter of the clamping hole is smaller than the diameter of the aviation connector pin, the aviation connector pin is inserted into the clamping hole through the deformation of the bottom rubber block. The threaded block drives the aviation connector pin through the threaded hole into the maintenance cylinder. The threaded block is screwed into the threaded hole, and the end of the aviation connector pin away from the bottom rubber block is inserted into the clamping hole on the bottom wall of the top rubber block. The aviation connector pin is fixed between the clamping holes. The expansion spring is set to shorten, and the grinding and heat-resistant electromagnet is energized to generate magnetism. The grinding and heat-resistant electromagnet is fixed to the side wall of the maintenance cylinder and absorbs the limiting iron block through magnetic force. The limiting iron block drives the guide column to slide along the inner wall of the maintenance cylinder through the deformation of the expansion spring. The guide column drives the sponge polishing layer to move relative to each other through the grinding plate. The sponge polishing layer fits with the side wall of the aviation connector pin. The driving motor drives the top rubber block to rotate through the power end, and the top rubber block drives the aviation connector pin to rotate. The sponge polishing layer grinds and repairs the needle body surface of the aviation connector pin during the rotation process.

[0009] Preferably, the distance measuring mechanism includes a distance measuring seat, a distance measuring sensor, a heat insulation cover and a distance measuring groove, multiple groups of the distance measuring seats are arranged on the inner wall of the forming cylinder, multiple groups of the distance measuring sensors are arranged in sequence from top to bottom on the side of the distance measuring seat close to the maintenance cylinder, the heat insulation cover is arranged on the side wall of the distance measuring seat outside the distance measuring sensor, multiple groups of the distance measuring grooves are arranged on the side wall of the maintenance cylinder, and the distance measuring sensor and the distance measuring groove are arranged opposite to each other; the heat conducting mechanism includes a sliding spring, a sliding magnetic block, a pushing temperature-resistant electromagnet, a metal rod, a heating coil, a straight port, a vacuum pump and a heat insulation block, the sliding spring is arranged on the side of the heat insulation cover away from the distance measuring seat On one side, the sliding magnetic block is arranged on the side of the sliding spring away from the heat insulation cover, the pushing temperature-resistant electromagnet is arranged on the side wall of the heat insulation cover outside the sliding spring, the heat insulation block is arranged on the side of the sliding magnetic block away from the sliding spring, the metal rod is arranged on the side of the heat insulation block away from the sliding magnetic block, the heating coil is arranged on the side wall of the heat insulation block outside the metal rod, and the end of the metal rod away from the heat insulation block is arranged inside the ranging groove, the straight line openings are respectively arranged on the inner walls of the heat insulation cover, the sliding magnetic block, the metal rod and the aviation connector pin, the vacuum pump is arranged on the upper wall of the forming cylinder, and the vacuum pump suction end is arranged through the inside of the forming cylinder.

[0010] When in use, the distance measuring end of the distance measuring sensor detects the distance between it and the surface of the aviation connector pin through the straight line mouth. During the rotation of the aviation connector pin, the distance measuring sensor detects the circumferential surface of the aviation connector pin through the distance measuring end. When there is a slight depression on the surface of the aviation connector pin, the distance between the distance measuring end of the distance measuring sensor and the surface of the aviation connector pin increases, and then drives the metal rod on the same horizontal plane with it, pushing the heat-resistant electromagnet to energize to generate magnetism, pushing the heat-resistant electromagnet and the sliding magnetic block to be set with the same pole, pushing the heat-resistant electromagnet to push the sliding magnetic block through the repulsive force under the deformation of the sliding spring, and the sliding magnetic block drives the metal rod to slide along the distance measuring groove through the heat insulation block close to the side wall of the aviation connector pin. The distance between the aviation connector pin and the metal rod is the minimum, the heating coil heats the metal rod, and the metal rod has a depression on the aviation connector pin. The side wall at the sunken position is heated. After the sunken part of the aviation connector pin is heated to the temperature specified by the operator, the hardness of the aviation connector pin will decrease and the plasticity will increase. The vacuum pump discharges the gas inside the molding cylinder through the exhaust end. The gas pressure inside the molding cylinder is reduced, and the pin is deformed under the action of external pressure and its own stress, causing the slightly sunken part of the aviation connector pin to bulge, thereby ensuring the signal transmission quality of the aviation connector pin. In the process of the driving motor power end driving the aviation connector pin to rotate through the top rubber block, each point on the surface of the aviation connector pin will be affected by centrifugal force. The magnitude of this force is proportional to the rotation radius and the square of the angular velocity, so that the sunken part on the surface of the aviation connector pin is affected by a large centrifugal force, thereby causing deformation, and to a certain extent, auxiliary repair of the sunken part of the aviation connector pin is performed.

[0011] Wherein, a controller is provided on the upper wall of the forming cylinder.

[0012] Preferably, the controller is electrically connected to the driving motor, the grinding temperature-resistant electromagnet, the distance sensor, the pushing temperature-resistant electromagnet, the heating coil and the vacuum pump respectively.

[0013] Furthermore, the model of the controller is SYC89C52RC-401.

[0014] Furthermore, the model of the vacuum pump is SPT-GL-811.

[0015] The beneficial effects achieved by adopting the above structure are as follows:

[0016] Compared with the prior art, this solution combines heating, low pressure, and rotating centrifugal force. Through the provided grinding repair mechanism and rotary measuring bulging mechanism, the assembly mechanism, rotary grinding mechanism, distance measuring mechanism, and heat conduction mechanism work together to grind and repair impurities on the surface of the aviation connector pin. It can also perform heating, low pressure, and centrifugal repair on the surface of the aviation connector pin. This extends the life of the aviation connector pin while ensuring the signal transmission quality of the aviation connector pin, and to a certain extent improves the efficiency of the aviation connector pin forming equipment. The heating coil heats the metal rod, which in turn heats the circumferential sidewalls of the aviation connector pin at the height of the bulge. After the bulge reaches the temperature specified by the operator, the hardness of the aviation connector pin decreases and the plasticity increases. The vacuum pump discharges the gas inside the forming cylinder through the exhaust port, reducing the gas pressure inside the forming cylinder. Under the action of external pressure and its own stress, the cylinder deforms, causing the slight bulge of the aviation connector pin, thereby ensuring the signal transmission quality of the aviation connector pin. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is a schematic diagram of the overall structure of this scheme;

[0018] Figure 2 This is a bottom-up perspective view of this scheme;

[0019] Figure 3 This is a schematic diagram of the internal structure of this scheme;

[0020] Figure 4 This is a schematic diagram of the structure of the assembly mechanism of this scheme;

[0021] Figure 5 Schematic diagram of the structure of the heat conduction mechanism of this scheme;

[0022] Figure 6 This is a schematic diagram of the distance measuring mechanism of this scheme;

[0023] Figure 7 This is a schematic diagram of the structure of the maintenance cylinder of this scheme;

[0024] Figure 8 This is a schematic diagram of the structure of the atherectomy mechanism of this solution;

[0025] Figure 9 This is the main view of this scheme;

[0026] Figure 10 This is a side view of the scheme;

[0027] Figure 11 This is a top view of the scheme;

[0028] Figure 12 for Figure 11 AA section view;

[0029] Figure 13 for Figure 10 BB partial cross-sectional view;

[0030] Figure 14 for Figure 12 A magnified structural view of part I;

[0031] Figure 15 for Figure 13 A magnified structural view of Part II;

[0032] Figure 16 for Figure 3 A magnified structural view of part III.

[0033] Among them, 1. forming cylinder, 2. maintenance cylinder, 3. grinding type repair mechanism, 4. assembly mechanism, 5. threaded hole, 6. threaded block, 7. bottom rubber block, 8. top rubber block, 9. clamping mouth, 10. rotary grinding mechanism, 11. driving motor, 12. guide column, 13. grinding plate, 14. sponge grinding layer, 15. grinding heat-resistant electromagnet, 16. limiting iron block, 17. rotary measuring type bulging mechanism, 18. distance measuring mechanism, 19. distance measuring seat, 20. distance measuring sensor, 21. heat insulation cover, 22. distance measuring groove, 23. heat conducting mechanism, 24. sliding spring, 25. sliding magnetic block, 26. pushing heat-resistant electromagnet, 27. metal rod, 28. heating coil, 29. straight line mouth, 30. vacuum pump, 31. controller, 32. aviation connector pin, 33. expansion spring, 34. heat insulation block.

[0034] The accompanying drawings are used to provide further understanding of the present solution and constitute a part of the specification. Together with the embodiments of the present solution, they are used to explain the present solution and do not constitute a limitation to the present solution. DETAILED DESCRIPTION

[0035] The technical solutions in the embodiments of this solution will be clearly and completely described below in conjunction with the drawings in the embodiments of this solution. Obviously, the described embodiments are only part of the embodiments of this solution, not all of the embodiments; based on the embodiments in this solution, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of this solution.

[0036] In the description of this solution, it should be understood that terms such as "up", "down", "front", "back", "left", "right", "top", "bottom", "inside", and "outside" indicating directions or positional relationships are based on the directions or positional relationships shown in the accompanying drawings. They are only for the convenience of describing this solution and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific direction, be constructed and operated in a specific direction. Therefore, they should not be understood as limitations on this solution.

[0037] like Figures 1-16 As shown, the present invention proposes an aviation plug connector forming device, comprising a forming cylinder 1, a maintenance cylinder 2, a grinding type repair mechanism 3 and a rotary measuring type bulging mechanism 17, wherein the maintenance cylinder 2 is arranged between the upper wall and the bottom wall of the forming cylinder 1, and the maintenance cylinder 2 is arranged through, the grinding type repair mechanism 3 is arranged on the maintenance cylinder 2, and the rotary measuring type bulging mechanism 17 is arranged on the inner wall of the forming cylinder 1, the grinding type repair mechanism 3 comprises an assembly mechanism 4 and a rotary grinding mechanism 10, the assembly mechanism 4 is arranged on the upper wall of the forming cylinder 1, the rotary grinding mechanism 10 is arranged on the side wall of the maintenance cylinder 2, the rotary measuring type bulging mechanism 17 comprises a distance measuring mechanism 18 and a heat conducting mechanism 23, the distance measuring mechanism 18 is arranged on the inner wall of the forming cylinder 1, and the heat conducting mechanism 23 is arranged on the side of the distance measuring mechanism 18 close to the maintenance cylinder 2.

[0038] The assembly mechanism 4 includes a threaded hole 5, a threaded block 6, a bottom rubber block 7, a top rubber block 8, a clamping port 9 and an aviation connector pin 32. The threaded hole 5 is provided on the bottom wall of the forming cylinder 1, the threaded block 6 is provided inside the threaded hole 5, the threaded block 6 is threadedly connected to the threaded hole 5, the bottom rubber block 7 is rotatably provided on the upper wall of the threaded block 6, the top rubber block 8 is rotatably provided on the top inner wall of the forming cylinder 1, the bottom rubber block 7 and the top rubber block 8 are arranged opposite to each other, the clamping port 9 is respectively provided on the side of the bottom rubber block 7 away from the threaded block 6 and the side of the top rubber block 8 away from the top inner wall of the forming cylinder 1, the clamping ports 9 are arranged opposite to each other, the aviation connector pin 32 is provided between the clamping ports 9, and the diameter of the clamping port 9 is smaller than the diameter of the aviation connector pin 32; the rubbing mechanism 10 includes a driving Motor 11, guide column 12, grinding plate 13, sponge polishing layer 14, grinding heat-resistant electromagnet 15, limiting iron block 16 and expansion spring 33, the driving motor 11 is arranged on the upper wall of the forming cylinder 1, the power end of the driving motor 11 passes through the forming cylinder 1 and is connected to the top rubber block 8, multiple groups of guide columns 12 are arranged through the side wall of the maintenance cylinder 2, the grinding plate 13 is arranged on the side wall of the guide column 12 inside the maintenance cylinder 2, the sponge polishing layer 14 is arranged on the side of the grinding plate 13 away from the guide column 12, the sponge polishing layer 14 is arranged relatively, the grinding heat-resistant electromagnet 15 is arranged on the side wall of the maintenance cylinder 2 outside the guide column 12, the limiting iron block 16 is arranged on the side of the guide column 12 away from the grinding plate 13, and the expansion spring 33 is arranged between the maintenance cylinder 2 outside the guide column 12 and the limiting iron block 16.

[0039] The distance measuring mechanism 18 includes a distance measuring seat 19, a distance measuring sensor 20, a heat insulation cover 21 and a distance measuring groove 22. Multiple groups of the distance measuring seats 19 are arranged on the inner wall of the forming cylinder 1, and multiple groups of the distance measuring sensors 20 are arranged from top to bottom on the side of the distance measuring seat 19 close to the maintenance cylinder 2. The heat insulation cover 21 is arranged on the side wall of the distance measuring seat 19 outside the distance measuring sensor 20. Multiple groups of the distance measuring grooves 22 are arranged on the side wall of the maintenance cylinder 2, and the distance measuring sensor 20 is arranged opposite to the distance measuring groove 22; the heat conducting mechanism 23 includes a sliding spring 24, a sliding magnetic block 25, a pushing temperature-resistant electromagnet 26, a metal rod 27, a heating coil 28, a straight port 29, a vacuum pump 30 and a heat insulation block 34. The sliding spring 24 is arranged on the side of the heat insulation cover 21 away from the distance measuring seat 19. side, the sliding magnetic block 25 is arranged on the side of the sliding spring 24 away from the heat insulation cover 21, the pushing temperature-resistant electromagnet 26 is arranged on the side wall of the heat insulation cover 21 outside the sliding spring 24, the heat insulation block 34 is arranged on the side of the sliding magnetic block 25 away from the sliding spring 24, the metal rod 27 is arranged on the side of the heat insulation block 34 away from the sliding magnetic block 25, the heating coil 28 is arranged on the side wall of the heat insulation block 34 outside the metal rod 27, and the end of the metal rod 27 away from the heat insulation block 34 is arranged inside the ranging groove 22, the straight line opening 29 is respectively arranged on the inner walls of the heat insulation cover 21, the sliding magnetic block 25, the metal rod 27 and the aviation connector pin 32, the vacuum pump 30 is arranged on the upper wall of the forming cylinder 1, and the vacuum pump 30 exhaust end is arranged through the inside of the forming cylinder 1.

[0040] A controller 31 is provided on the upper wall of the forming cylinder 1 .

[0041] The controller 31 is electrically connected to the driving motor 11 , the grinding temperature-resistant electromagnet 15 , the distance sensor 20 , the pushing temperature-resistant electromagnet 26 , the heating coil 28 and the vacuum pump 30 .

[0042] The model of the controller 31 is SYC89C52RC-401.

[0043] The model of the vacuum pump 30 is SPT-GL-811.

[0044] During specific use, when it is necessary to repair the pin of the aviation connector, manually rotate the threaded block 6, the threaded block 6 is unscrewed from the inside of the threaded hole 5, and the aviation connector pin 32 is inserted into the clamping opening 9 on the upper wall of the bottom rubber block 7. Since the diameter of the clamping opening 9 is smaller than the diameter of the aviation connector pin 32, the aviation connector pin 32 is inserted into the clamping opening 9 through the deformation of the bottom rubber block 7. The threaded block 6 drives the aviation connector pin 32 through the threaded hole 5 into the interior of the maintenance cylinder 2. The threaded block 6 is screwed into the inside of the threaded hole 5. The end of the aviation connector pin 32 away from the bottom rubber block 7 is inserted into the clamping opening 9 on the bottom wall of the top rubber block 8. The aviation connector pin 32 is fixed between the clamping openings 9;

[0045] Specifically, the expansion spring 33 is set to shorten, the controller 31 controls the grinding heat-resistant electromagnet 15 to start, the grinding heat-resistant electromagnet 15 is energized to generate magnetism, the grinding heat-resistant electromagnet 15 is fixed to the side wall of the maintenance cylinder 2 and absorbs the limiting iron block 16 by magnetic force, the limiting iron block 16 drives the guide column 12 to slide along the inner wall of the maintenance cylinder 2 through the deformation of the expansion spring 33, the guide column 12 drives the sponge polishing layer 14 to move relative to each other through the grinding plate 13, the sponge polishing layer 14 is in contact with the side wall of the aviation connector pin 32, the controller 31 controls the drive motor 11 to start, the drive motor 11 drives the top rubber block 8 to rotate through the power end, the top rubber block 8 drives the aviation connector pin 32 to rotate, and the sponge polishing layer 14 grinds and repairs the needle body surface of the aviation connector pin 32 during the rotation process;

[0046] The controller 31 controls the starting of the distance measuring sensor 20. The distance measuring end of the distance measuring sensor 20 detects the distance between the distance measuring end and the surface of the aviation connector pin 32 through the straight port 29. During the rotation of the aviation connector pin 32, the distance measuring sensor 20 detects the circumferential surface of the aviation connector pin 32 through the distance measuring end. When there is a slight depression on the surface of the aviation connector pin 32, the distance between the distance measuring end of the distance measuring sensor 20 and the surface of the aviation connector pin 32 increases, and then drives the metal rod 27 on the same horizontal plane with it. The controller 31 controls the starting of the heat-resistant electromagnet 26, and drives the heat-resistant electromagnet 26 to generate magnetism, and pushes the heat-resistant electromagnet 26 to be set with the same pole as the sliding magnet block 25. The heat-resistant electromagnet 26 pushes the sliding magnet block 25 through the repulsive force under the deformation of the sliding spring 24. The sliding magnet block 25 drives the metal rod 27 to slide along the distance measuring slot 22 close to the side wall of the aviation connector pin 32 through the heat insulation block 34. The distance between the aviation connector pin 32 and the metal rod 27 is the minimum.

[0047] The controller 31 activates the heating coil 28, which heats the metal rod 27. The metal rod 27 heats the sidewall of the copper aviation connector pin 32 where the depression is located. After the depression is heated to the temperature specified by the operator, the hardness of the aviation connector pin 32 decreases and its plasticity increases. The vacuum pump 30 exhausts the gas inside the forming cylinder 1 through the exhaust port, reducing the gas pressure inside the forming cylinder 1. Under the action of external pressure and internal stress, the forming cylinder 1 deforms, causing the slightly depressed area of ​​the aviation connector pin 32 to bulge, thereby ensuring the signal transmission quality of the aviation connector pin 32. As the power end of the drive motor 11 drives the aviation connector pin 32 to rotate through the top rubber block 8, each point on the surface of the aviation connector pin 32 is subjected to centrifugal force. The magnitude of this force is proportional to the rotation radius and the square of the angular velocity. This causes the depressed area on the surface of the aviation connector pin 32 to be subjected to a large centrifugal force, causing deformation, and to a certain extent, assisting in repairing the depressed area of ​​the aviation connector pin 32. The above operation can be repeated for the next use.

[0048] It should be noted that, in this document, relational terms such as first and second, etc., are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "comprises," "comprising," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that includes a list of elements includes not only those elements but also other elements not explicitly listed, or elements inherent to such process, method, article, or apparatus.

[0049] The above description of the present solution and its implementation methods is non-limiting. The drawings show only one implementation method of the present solution, and the actual structure is not limited thereto. In short, if a person skilled in the art is inspired by this and, without departing from the purpose of the present solution, designs a similar structure and embodiment without creatively designing, they shall fall within the scope of protection of the present solution.

Claims

1. An aviation connector forming device, comprising a forming cylinder and a maintenance cylinder, characterized in that: It also includes a grinding type repair mechanism and a rotary measuring type bulging mechanism. The repair cylinder is arranged between the upper wall and the bottom wall of the forming cylinder, and the repair cylinder is arranged through. The grinding type repair mechanism includes an assembly mechanism and a rubbing mechanism; The assembly mechanism is arranged on the upper wall of the forming cylinder, and the rubbing mechanism is arranged on the side wall of the maintenance cylinder; The rotary measuring type swelling mechanism includes a distance measuring mechanism and a heat conducting mechanism; The distance measuring mechanism is arranged on the inner wall of the forming cylinder, and the heat conducting mechanism is arranged on a side of the distance measuring mechanism close to the maintenance cylinder; The assembly mechanism includes a threaded hole, a threaded block, a bottom rubber block, a top rubber block and an aviation connector pin; The threaded hole is provided on the bottom wall of the forming cylinder, the threaded block is provided inside the threaded hole, the threaded block is threadedly connected to the threaded hole, the bottom rubber block is rotatably provided on the upper wall of the threaded block, the top rubber block is rotatably provided on the top inner wall of the forming cylinder, and the bottom rubber block and the top rubber block are arranged opposite to each other; The atherectomy mechanism includes a drive motor; The driving motor is arranged on the upper wall of the forming cylinder, and the power end of the driving motor passes through the forming cylinder and is connected to the top rubber block; The distance measuring mechanism includes a distance measuring seat, a distance measuring sensor and a heat shield; Multiple groups of the distance measuring seats are arranged on the inner wall of the forming cylinder, multiple groups of the distance measuring sensors are arranged in sequence from top to bottom on a side of the distance measuring seat close to the maintenance cylinder, and the heat insulation cover is arranged on the side wall of the distance measuring seat outside the distance measuring sensor; The heat conduction mechanism includes a sliding spring, a sliding magnetic block, a pushing temperature-resistant electromagnet, a metal rod, a heating coil and a heat insulation block; The sliding spring is arranged on the side of the heat insulation cover away from the distance measuring seat, the sliding magnetic block is arranged on the side of the sliding spring away from the heat insulation cover, the pushing temperature-resistant electromagnet is arranged on the side wall of the heat insulation cover outside the sliding spring, the heat insulation block is arranged on the side of the sliding magnetic block away from the sliding spring, the metal rod is arranged on the side of the heat insulation block away from the sliding magnetic block, and the heating coil is arranged on the side wall of the heat insulation block outside the metal rod; When the power end of the driving motor drives the aviation connector pin to rotate through the top rubber block, each point on the surface of the aviation connector pin will be affected by centrifugal force. The magnitude of this force is proportional to the rotation radius and the square of the angular velocity, causing the depression on the surface of the aviation connector pin to be affected by a large centrifugal force, resulting in deformation, which to a certain extent assists in repairing the depression of the aviation connector pin.

2. The aviation connector forming device according to claim 1, characterized in that: The assembly mechanism also includes clamping openings, which are respectively arranged on the side of the bottom rubber block away from the threaded block and the side of the top rubber block away from the top inner wall of the forming cylinder. The clamping openings are arranged opposite to each other, and the aviation connector pin is arranged between the clamping openings. The diameter of the clamping opening is smaller than the diameter of the aviation connector pin.

3. The aviation connector forming device according to claim 2, characterized in that: The rotary grinding mechanism also includes a guide column, a grinding plate, a sponge grinding layer, a grinding heat-resistant electromagnet, a limiting iron block and an expansion spring. Multiple groups of the guide columns are arranged through the side wall of the maintenance cylinder, the grinding plate is arranged on the side wall of the guide column inside the maintenance cylinder, the sponge grinding layer is arranged on the side of the grinding plate away from the guide column, and the sponge grinding layers are arranged relatively. The grinding heat-resistant electromagnet is arranged on the side wall of the maintenance cylinder outside the guide column, the limiting iron block is arranged on the side of the guide column away from the grinding plate, and the expansion spring is arranged between the maintenance cylinder outside the guide column and the limiting iron block.

4. The aviation connector forming device according to claim 3, characterized in that: The distance measuring mechanism also includes a distance measuring groove, a plurality of groups of the distance measuring grooves are arranged on the side wall of the maintenance cylinder, the distance measuring sensor is arranged opposite to the distance measuring groove, and the end of the metal rod away from the insulation block is arranged inside the distance measuring groove.

5. The aviation connector forming device according to claim 4, characterized in that: The heat conduction mechanism also includes a linear port and a vacuum pump. The linear port is respectively arranged on the inner wall of the heat insulation cover, the sliding magnetic block, the metal rod and the aviation connector pin. The vacuum pump is arranged on the upper wall of the forming cylinder, and the vacuum pump suction end is arranged through the inside of the forming cylinder.

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