Aerial plug docking system

Abstract

The utility model provides an aviation plug docking system, and relates to the technical field of magnetic control switch production. The aviation plug docking system comprises a switch positioning device and a pneumatic assembly. The switch positioning device is used for positioning a magnetically controlled switch. The pneumatic assembly comprises a first pneumatic device, a second pneumatic device and an adjusting piece, the first pneumatic device is located above the switch positioning device, the driving end of the first pneumatic device is detachably connected with the adjusting piece, and the driving end of the second pneumatic device is located on one side of the driving end of the first pneumatic device; the fixed end of the second pneumatic device is detachably connected with the adjusting piece, and the adjusting piece is used for adjusting the relative position of the driving end of the second pneumatic device and the magnetic control switch; the first pneumatic device is used for pressing the magnetic control switch. According to the embodiment of the invention, automation can be realized while the docking precision of the aviation plug system is ensured, so that the product yield is improved.

Description

Technical Field

[0001] The embodiments of the present application relate to but are not limited to the field of magnetically controlled switch production technology, and in particular to an aviation plug-in docking system. Background Art

[0002] The aviation plug, also known as the aviation plug, is usually installed on the insertion port of the magnetic control switch. Since the pins of the aviation plug are usually copper pins with a diameter of 1 to 1.5 mm, and in order to ensure the conductivity of the aviation plug and the magnetic control switch, each pin of the aviation plug needs to be tightly matched with the insertion port on the magnetic control switch. Therefore, during the insertion of the aviation plug, there are often certain requirements for the insertion pressure to prevent the pressure from being too small and not being inserted in place or the pressure from being too high, causing damage to the pins of the aviation plug and the insertion port of the magnetic control switch. In the related art, the docking of the aviation plug and the magnetic control switch can be achieved by manual insertion, but this method is greatly affected by human factors, resulting in insufficient insertion accuracy and low product yield. Although hydraulic, electric servo and other drives can also be used to achieve stable pressure output, thereby realizing the automation of the aviation plug docking system, the size of such drive devices is often large, and the output pressure is also very large, which exceeds the needs of the aviation plug and needs to be customized. Therefore, how to ensure the docking accuracy of the aviation plug system while achieving automation to improve the product yield is a technical problem that needs to be solved urgently. Utility Model Content

[0003] The following is an overview of the subject matter described in detail herein. This overview is not intended to limit the scope of protection of the claims. The present application embodiment provides an aerial plug docking system that can achieve automation while ensuring the docking accuracy of the aerial plug system, thereby improving the product yield.

[0004] According to the aerial docking system proposed in the embodiment of the present application, the aerial docking system includes:

[0005] A switch positioning device, the switch positioning device is used to position the magnetically controlled switch;

[0006] A pneumatic assembly, the pneumatic assembly comprising a first pneumatic device, a second pneumatic device and an adjusting piece, the first pneumatic device being located above the switch positioning device, the driving end of the first pneumatic device being detachably connected to the adjusting piece, the driving end of the second pneumatic device being located on one side of the driving end of the first pneumatic device; the fixed end of the second pneumatic device being detachably connected to the adjusting piece, the adjusting piece being used to adjust the relative position of the driving end of the second pneumatic device and the magnetically controlled switch; the first pneumatic device being used to press the magnetically controlled switch.

[0007] Therefore, the above-mentioned embodiments of the present application have at least the following beneficial effects: after positioning by the switch positioning device, the first pneumatic device presses the magnetically controlled switch, thereby ensuring that the position of the magnetically controlled switch remains unchanged as much as possible during the insertion of the aviation plug, and at the same time, since the adjustment part is detachably connected to the second pneumatic device, the relative position of the driving end of the second pneumatic device and the magnetically controlled switch is adjusted by the adjustment part before plugging in the same type of magnetic air switch, thereby improving the docking accuracy between the aviation plug located at the driving end of the second pneumatic device and the magnetically controlled switch, and driving through the second pneumatic device. At this time, since the pressure and volume that can be provided by the second pneumatic device can meet the pressure requirements of the aviation plug, the embodiments of the present application can ensure the docking accuracy of the aviation plug in the aviation plug system while realizing the automation of aviation plug insertion, thereby improving the product yield.

[0008] According to some embodiments of the present application, the adjusting member includes a connecting plate and a positioning block, the first end of the connecting plate is connected to the driving end of the first pneumatic device, the second end of the connecting plate is fixedly connected to the positioning block, and the positioning block is provided with a plurality of first positioning grooves arranged parallel to the driving direction, and the fixed ends of the second pneumatic devices can be detachably connected to the first positioning grooves.

[0009] According to some embodiments of the present application, a plurality of second positioning grooves along the driving direction are opened on the second end of the connecting plate, and the first positioning grooves are vertically arranged to the second positioning grooves, and the positioning block is detachably connected to the second positioning grooves.

[0010] According to some embodiments of the present application, the second pneumatic device includes a cylinder body and a driving rod, the first end of the driving rod is connected to the cylinder body, and the cylinder body is connected to the adjusting member, and the aviation docking system also includes a positioning sensor, which is arranged in a groove of the cylinder body. The positioning sensor is used to position the insertion port 210 of the magnetic control switch to adjust the position of the cylinder body on the adjusting member according to the detection result of the positioning sensor.

[0011] According to some embodiments of the present application, three driving rods are provided.

[0012] According to some embodiments of the present application, the switch positioning device includes a positioning plate and a positioning drive component, the positioning drive component is used to drive the positioning plate to move upward to a preset position, and the positioning plate is used to horizontally limit the magnetically controlled switch.

[0013] According to some embodiments of the present application, the aerial docking system further includes two symmetrically arranged conveying tracks, and the positioning plate is located between the two conveying tracks.

[0014] According to some embodiments of the present application, the aerial docking system further includes an in-place sensor, which is located on one side of the conveying track, and is used to detect the magnetically controlled switch on the conveying track for in-place detection.

[0015] According to some embodiments of the present application, the pneumatic assembly further includes a third pneumatic device, which is arranged in parallel with the first pneumatic device, and the third pneumatic device and the first pneumatic device are both used to press the magnetically controlled switch.

[0016] According to some embodiments of the present application, the aviation docking system also includes a frame, the fixed ends of the first pneumatic device and the third pneumatic device are both connected to the frame, and the switch positioning device is arranged on the frame. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] The accompanying drawings are used to provide further understanding of the technical solution of the present application and constitute a part of the specification. Together with the embodiments of the present application, they are used to explain the technical solution of the present application and do not constitute a limitation on the technical solution of the present application.

[0018] Figure 1 It is a structural schematic diagram of an embodiment of the aviation plug-in docking system provided by the present application;

[0019] Figure 2a A schematic diagram of the structure of the magnetically controlled switch for automatic docking of the aviation docking system provided in this application;

[0020] Figure 2b A schematic diagram of the structure of another magnetically controlled switch for automatic docking of the aviation docking system provided in this application;

[0021] Figure 2c A schematic diagram of the structure of another magnetically controlled switch for automatic docking of the aviation docking system provided in this application;

[0022] Figure 3 It is a schematic diagram of the structure of the pneumatic components in the aviation docking system provided by the present application;

[0023] Figure 4 yes Figure 3 A schematic diagram of the structure of the pneumatic assembly from another perspective is shown;

[0024] Figure 5 yes Figure 3 A schematic structural diagram of the pneumatic component from another perspective is shown.

[0025] Reference numerals:

[0026] Switch positioning device 100, positioning plate 110,

[0027] Magnetic switch 200, insertion port 210, support column 220,

[0028] Pneumatic assembly 300, first pneumatic device 310, second pneumatic device 320, cylinder 321, drive rod 322, adjustment member 330, connecting plate 331, positioning block 332, first positioning slide groove 333, second positioning slide groove 334, third pneumatic device 340, positioning sensor 410, conveying track 420, frame 430,

[0029] Hangcha 500. DETAILED DESCRIPTION

[0030] In order to make the purpose, technical solution and advantages of the present application more clearly understood, the present application is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present application and are not used to limit the present application.

[0031] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as those generally understood by those skilled in the art belonging to the technical field of the present application. The terms used herein are only for the purpose of describing the embodiments of the present application and are not intended to limit the present application. The terms "first", "second", "third", "fourth", etc. (if present) in the specification of the present application and the above-mentioned drawings are used to distinguish similar objects, and need not be used to describe a specific order or sequential order.

[0032] In addition, the described features, structures or characteristics may be combined in one or more embodiments in any suitable manner. In the following description, many specific details are provided to provide a full understanding of the embodiments of the present disclosure. However, those skilled in the art will appreciate that the technical solutions of the present disclosure may be practiced without one or more of the specific details, or other methods, components, devices, steps, etc. may be adopted. In other cases, known methods, devices, implementations or operations are not shown or described in detail to avoid blurring the various aspects of the present disclosure.

[0033] Reference Figures 1 to 5 As shown, according to the aerial docking system proposed in the embodiment of the present application, the aerial docking system includes:

[0034] A switch positioning device 100, the switch positioning device 100 is used to position the magnetic control switch 200;

[0035] Pneumatic assembly 300, the pneumatic assembly 300 includes a first pneumatic device 310, a second pneumatic device 320 and an adjusting member 330, the first pneumatic device 310 is located above the switch positioning device 100, the driving end of the first pneumatic device 310 is detachably connected to the adjusting member 330, and the driving end of the second pneumatic device 320 is located on one side of the driving end of the first pneumatic device 310; the fixed end of the second pneumatic device 320 is detachably connected to the adjusting member 330, and the adjusting member 330 is used to adjust the relative position of the driving end of the second pneumatic device 320 and the magnetic control switch 200; the first pneumatic device 310 is used to press the magnetic control switch 200.

[0036] Therefore, after positioning by the switch positioning device 100, the first pneumatic device 310 presses the magnetic control switch 200, thereby ensuring that the position of the magnetic control switch 200 remains unchanged as much as possible during the insertion of the aviation plug 500. At the same time, since the adjustment part 330 is detachably connected to the second pneumatic device 320, the relative position of the driving end of the second pneumatic device 320 and the magnetic control switch 200 is adjusted by the adjustment part 330 before plugging in the same type of magnetic air switch, so as to improve the docking accuracy between the aviation plug 500 located at the driving end of the second pneumatic device 320 and the magnetic control switch 200, and drive it through the second pneumatic device 320. At this time, since the pressure and volume that can be provided by the second pneumatic device 320 can meet the pressure requirements of the aviation plug 500, the embodiment of the present application can realize the automation of the insertion of the aviation plug 500 while ensuring the docking accuracy of the aviation plug 500 in the aviation plug 500 system, thereby improving the product yield.

[0037] It should be noted that the first pneumatic device 310 and the second pneumatic device 320 are both powered devices using gas as a driving source, such as a cylinder. The first pneumatic device 310 and the second pneumatic device 320 can both achieve controllable and adjustable output pressure and stable output pressure, and their structures are relatively simple and their volumes are smaller.

[0038] It should be noted that there are multiple types of magnetic control switches 200, and the insertion ports of different types of magnetic control switches 200 are set at different positions; therefore, the adjustment member 330 needs to be set to be detachably connected to the second pneumatic device 320, so as to adapt to different types of magnetic control switches 200. For example, Figure 2a-2b As shown, the magnetic switch 200 is provided with three types in total, wherein: Figure 2a The insertion port 210 of the magnetic switch 200 is located on the right side. Figure 2b The insertion port 210 of the magnetic switch 200 is located on the left side. Figure 2c The height of the support 220 of the magnetic switch 200 and Figure 2a , Figure 2bTherefore, by setting the adjustment member 330 to be detachably connected to the second pneumatic device 320, the same aviation plug-in docking system can be used for adaptation. When different types of magnetic switches 200 are plugged in, high-precision position adjustment is first performed, so that only the output pressure of the second pneumatic device 320 needs to be controlled to achieve accurate insertion and improve product yield.

[0039] It should be noted that, during docking, the magnetically controlled switch 200 is located between the switch positioning device 100 and the first pneumatic device 310 .

[0040] Understandably, referring to Figure 1 , Figures 3 to 5 As shown, the adjustment member 330 includes a connecting plate 331 and a positioning block 332. The first end of the connecting plate 331 is connected to the driving end of the first pneumatic device 310, and the second end of the connecting plate 331 is fixedly connected to the positioning block 332. The positioning block 332 is provided with a plurality of first positioning grooves 333 arranged parallel to the driving direction, and the fixed ends of the second pneumatic device 320 can be slidably connected to the first positioning grooves 333.

[0041] It should be noted that, by providing the first positioning slot 333, the height adjustment in the vertical direction and the position adjustment in the driving direction can be achieved by fasteners such as screws passing through the first positioning slot 333. For example, Figure 3 and Figure 4 As shown, the driving direction is the moving direction of the driving end of the second pneumatic device 320. Two first positioning slots 333 are provided, namely slot 1 and slot 2. Slot 1 and slot 2 are arranged in parallel along the driving direction, and slot 1 and slot 2 are arranged along the vertical direction. In some embodiments, by adjusting the connection relationship between the second pneumatic device 320 and slot 1 or slot 2, the position adjustment in the driving direction can be achieved, so as to ensure that the pressure in the driving direction is sufficient; when the second pneumatic device 320 is determined to be connected to the slot 1, the height adjustment can be achieved by adjusting the position on the slot 1, so as to adapt to magnetic switches 200 of different heights. In other embodiments, the first positioning slot 333 is only used to adjust the vertical position of the second pneumatic device 320. The provision of multiple first positioning slots 333 can further make the second pneumatic device 320 more stable. Multiple mounting holes connected to the first pneumatic device 310 are provided on the connecting plate, so that the distance between the second pneumatic device 320 and the insertion port 210 of the magnetic switch 200 meets the pressure requirement during docking.

[0042] Understandably, referring to Figure 3 and Figure 5As shown, a plurality of second positioning slots 334 along the driving direction are formed on the second end of the connecting plate 331 , and the first positioning slots 333 and the second positioning slots 334 are vertically arranged, and the positioning block 332 is detachably connected to the second positioning slots 334 .

[0043] It should be noted that the position of the magnetic switch 200 is used as a reference. Figure 3 and Figure 5 As shown, the position of the second pneumatic device 320 in the left-right direction can be adjusted by setting the second positioning slot 334, so as to further improve the docking accuracy between the driving end of the second pneumatic device 320 and the insertion port 210 of the magnetic switch 200.

[0044] It is understandable that if Figure 1 , Figures 3 to 5 As shown, the second pneumatic device 320 includes a cylinder body 321 and a driving rod 322, the first end of the driving rod 322 is connected to the cylinder body 321, and the cylinder body 321 is connected to the adjusting member 330. The aviation docking system also includes a positioning sensor 410, which is arranged in a groove of the cylinder body 321. The positioning sensor 410 is used to position the insertion port 210 of the magnetic control switch 200 so as to adjust the position of the cylinder body 321 on the adjusting member 330 according to the detection result of the positioning sensor 410.

[0045] It should be noted that by arranging the positioning sensor 410 in the groove of the cylinder body 321, the position of the positioning sensor 410 and the driving end can be relatively fixed, thereby ensuring that the positioning of the positioning sensor 410 is more accurate and improving the accuracy of the position of the second pneumatic device 320.

[0046] In some embodiments, the positioning sensor 410 is configured as a magnetic induction switch.

[0047] It is understandable that three driving rods 322 are provided.

[0048] By providing three driving rods 322 , the stability during the insertion process can be improved.

[0049] Understandably, referring to Figure 1 As shown, the switch positioning device 100 includes a positioning plate 110 and a positioning drive component. The positioning drive component is used to drive the positioning plate 110 to move up to a preset position. The positioning plate 110 is used to horizontally limit the magnetic control switch 200.

[0050] It should be noted that, in some embodiments, the positioning drive component is configured as a motor.

[0051] It is understandable that if Figure 1 As shown, the aerial docking system further includes two symmetrically arranged conveying rails 420 , and the positioning plate 110 is located between the two conveying rails 420 .

[0052] By providing the positioning plate 110 and the positioning drive, the magnetic switch 200 on the conveying track 420 can be separated from the conveying track 420 for positioning, thereby realizing batch automatic docking. The automation efficiency is higher.

[0053] It is understandable that the aerial docking system also includes an in-place sensor, which is located on one side of the conveying track 420 . The in-place sensor is used to detect the magnetic switch 200 on the conveying track 420 for in-place detection.

[0054] By providing an in-position sensor, it can be further ensured that during batch insertion, each magnetic switch 200 is automatically docked only after reaching a preset position, thereby further ensuring the docking accuracy.

[0055] It is understandable that if Figure 1 As shown, the pneumatic assembly 300 also includes a third pneumatic device 340, which is arranged in parallel with the first pneumatic device 310. The third pneumatic device 340 and the first pneumatic device 310 are both used to press the magnetic control switch 200, and the driving end of the third pneumatic device 340 is detachably connected to the adjustment member 330.

[0056] It should be noted that, in some embodiments, the spacing between the third pneumatic device 340 and the first pneumatic device 310 is the distance between the insertion ports 210 at different positions. At this time, since the adjustment member 330 is detachably connected, when the adjustment member 330 is installed on the third pneumatic device 340, the magnetic switch 200 with the insertion port 210 located on the left can be automatically docked. And by pressing the magnetic switch with multiple pneumatic devices, the docking effect is better.

[0057] It is understandable that if Figure 1 As shown, the aerial docking system further includes a frame 430 , the fixed ends of the first pneumatic device 310 and the third pneumatic device 340 are both connected to the frame 430 , and the switch positioning device 100 is disposed on the frame 430 .

[0058] It should be noted that, by providing the rack 430 , all components in the aerial docking system are integrated on the rack 430 , thereby making the entire aerial docking system more miniaturized.

[0059] The above is a specific description of the preferred implementation of the present application, but the present application is not limited to the above-mentioned implementation mode. Technical personnel familiar with the field can also make various equivalent deformations or substitutions without violating the spirit of the present application. These equivalent deformations or substitutions are all included in the scope defined by the claims of the present application.

Claims

1. An aerial docking system, characterized in that: The aerial docking system comprises: A switch positioning device, the switch positioning device is used to position the magnetically controlled switch; A pneumatic assembly, the pneumatic assembly comprising a first pneumatic device, a second pneumatic device and an adjusting piece, the first pneumatic device being located above the switch positioning device, the driving end of the first pneumatic device being detachably connected to the adjusting piece, the driving end of the second pneumatic device being located on one side of the driving end of the first pneumatic device; the fixed end of the second pneumatic device being detachably connected to the adjusting piece, the adjusting piece being used to adjust the relative position of the driving end of the second pneumatic device and the magnetically controlled switch; the first pneumatic device being used to press the magnetically controlled switch.

2. The aerial docking system according to claim 1, characterized in that: The adjusting member includes a connecting plate and a positioning block, the first end of the connecting plate is connected to the driving end of the first pneumatic device, the second end of the connecting plate is fixedly connected to the positioning block, and the positioning block is provided with a plurality of first positioning grooves arranged parallel to the driving direction, and the fixed ends of the second pneumatic device can be slidably connected to the first positioning grooves.

3. The aerial docking system according to claim 2, characterized in that: A plurality of second positioning slots along the driving direction are formed on the second end of the connecting plate, and the first positioning slots are vertically arranged to the second positioning slots, and the positioning block is detachably connected to the second positioning slots.

4. The aerial docking system according to claim 1, characterized in that: The second pneumatic device includes a cylinder body and a driving rod, the first end of the driving rod is connected to the cylinder body, and the cylinder body is connected to the adjusting member. The aviation docking system also includes a positioning sensor, and the positioning sensor is arranged in a groove of the cylinder body. The positioning sensor is used to position the insertion port of the magnetic control switch to adjust the position of the cylinder body on the adjusting member according to the detection result of the positioning sensor.

5. The aerial docking system according to claim 4, characterized in that: The number of driving rods is three.

6. The aerial docking system according to claim 1, characterized in that: The switch positioning device comprises a positioning plate and a positioning driving component, wherein the positioning driving component is used to drive the positioning plate to move upward to a preset position, and the positioning plate is used to horizontally limit the magnetically controlled switch.

7. The aerial docking system according to claim 6, characterized in that: The aerial docking system further includes two symmetrically arranged conveying tracks, and the positioning plate is located between the two conveying tracks.

8. The aerial docking system according to claim 7, characterized in that: The aerial docking system further includes an in-place sensor, which is located at one side of the conveying track and is used to detect the magnetically controlled switch on the conveying track for in-place detection.

9. The aerial docking system according to claim 1, characterized in that: The pneumatic assembly also includes a third pneumatic device, which is arranged in parallel with the first pneumatic device. The third pneumatic device and the first pneumatic device are both used to press the magnetic control switch, and the third pneumatic device is detachably connected to the adjusting member.

10. The aerial docking system according to claim 9, characterized in that: The aviation docking system also includes a frame, the fixed ends of the first pneumatic device and the third pneumatic device are both connected to the frame, and the switch positioning device is arranged on the frame.

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