Flying probe automatic calibration mechanism for first workpiece detection
Through the automated fly needle calibration mechanism, the X-axis operation control, Y-axis operation control and CCD visual components are used to accurately calculate the fly needle position, solving the problems of inaccurate manual correction and replacement, and achieving efficient automatic correction and convenient replacement.
Patent Information
- Application Number
- CN202422470377.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-12
- Publication Date
- 2025-07-25
- Estimated Expiration
- 2034-10-12
AI Technical Summary
In the prior art, the movement and correction of the flying needles rely on manual operations, resulting in inaccurate position deviation and difficult to calculate the rotation accuracy, and replacing the worn flying needles increases the correction difficulty.
The automatic flying needle calibration mechanism is adopted to realize automatic calibration through X-axis operation control, Y-axis operation control and CCD vision components. Combined with the rotation mechanism and the opening and closing mechanism, the position of the flying needle is accurately calculated and supports automatic replacement of the flying needle.
It achieves high accuracy and low calibration difficulty for flying needle correction, simple operation, and more convenient replacement of flying needles.
Smart Images

Figure CN223154205U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the technical field of flying needle correction equipment, and particularly relates to a first-piece inspection flying needle automatic calibration mechanism. Background Technique
[0002] At present, in the industry, the flying needle alignment is manually moved, observed by the naked eye, and the position deviation is compensated manually in a estimating manner, which is extremely inaccurate and the rotation accuracy cannot be measured by the naked eye. Especially during the use process, it is also necessary to replace the worn old flying needles, resulting in increased calibration difficulty and certain limitations. Content of the Utility Model
[0003] The purpose of the utility model is to provide a first-piece inspection flying needle automatic calibration mechanism to solve the problems in the above background technique that the existing flying needle alignment is manually moved, observed by the naked eye, and the position deviation is compensated manually in a estimating manner, which is extremely inaccurate and the rotation accuracy cannot be measured by the naked eye. Especially during the use process, it is also necessary to replace the worn old flying needles, resulting in increased calibration difficulty and certain limitations.
[0004] To achieve the above purpose, the utility model provides the following technical scheme: a first-piece inspection flying needle automatic calibration mechanism, including a carrier platform, a carrier block is arranged at the upper end of the carrier platform, a fixed platform is fixedly connected to one side of the upper end of the carrier platform, an X-axis motion control is fixedly connected to the upper end of the fixed platform, a first moving block is slidably connected to the upper end of the X-axis motion control, a Y-axis motion control is fixedly connected to one side of the first moving block, a second moving block is slidably connected to one side of the Y-axis motion control, a CCD vision component is fixedly connected to one side of the second moving block, a fixed frame is fixedly connected to one side of the second moving block, a rotation mechanism is fixedly connected to the lower end of one side of the fixed frame, a left flying needle is fixedly connected to the lower end of one side of the rotation mechanism, and a right flying needle is fixedly connected to the lower end of the other side of the rotation mechanism.
[0005] Preferably, a Z-axis motion control is fixedly connected to the upper end of the carrier platform, a carrier moving plate is slidably arranged at the upper end of the Z-axis motion control, and a carrier block is fixedly connected to one side of the carrier moving plate.
[0006] Preferably, a clamping mechanism is fixedly connected to the lower end of the rotation mechanism, and a left flying needle and a right flying needle are fixedly connected to both sides of the clamping mechanism.
[0007] Compared with the prior art, the beneficial effects of the utility model are:
[0008] 1. The whole process of the needle alignment method of the utility model adopts an automatic needle alignment method, with high accuracy, low calibration difficulty, more convenient needle replacement, and simple operation. Description of the Drawings
[0009] Figure 1 It is a structural schematic diagram of the utility model;
[0010] Figure 2 This is a schematic structural diagram of the electrical wiring and control principle of the present utility model;
[0011] Figure 3 This is a schematic structural diagram of the Y-axis motion control of the present utility model;
[0012] Figure 4 This is a schematic structural diagram of the flying needle of the present utility model;
[0013] Figure 5 This is the present utility model Figure 1 An enlarged structural diagram of area A in it.
[0014] In the figure: 1, carrier platform; 2, fixed platform; 3, X-axis motion control; 4, first moving block; 5, Y-axis motion control; 6, Z-axis motion control; 7, carrier block; 8, CCD vision component; 9, left flying needle; 10, right flying needle; 11, second moving block; 12, fixed frame; 13, rotating mechanism; 14, carrier transport plate; 15, opening and closing mechanism. Specific embodiments
[0015] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.
[0016] Please refer to Figures 1-5 , the present utility model provides a technical solution: a first-piece inspection flying needle automatic calibration mechanism, including a carrier platform 1, a carrier block 7 is arranged at the upper end of the carrier platform 1, a fixed platform 2 is fixedly connected to one side of the upper end of the carrier platform 1, an X-axis motion control 3 is fixedly connected to the upper end of the fixed platform 2, a first moving block 4 is slidably connected to the upper end of the X-axis motion control 3, a Y-axis motion control 5 is fixedly connected to one side of the first moving block 4, a second moving block 11 is slidably connected to one side of the Y-axis motion control 5, a CCD vision component 8 is fixedly connected to one side of the second moving block 11, a fixed frame 12 is fixedly connected to one side of the second moving block 11, a rotating mechanism 13 is fixedly connected to the lower end of one side of the fixed frame 12, a left flying needle 9 is fixedly connected to the lower end of one side of the rotating mechanism 13, and a right flying needle 10 is fixedly connected to the lower end of the other side of the rotating mechanism 13.
[0017] In this implementation scheme, the X-axis motion control 3 and the Y-axis motion control 5 are set to perform motion control in the X and Y directions, so that the CCD vision component 8 can take pictures of the carrier block 7, thereby calculating the center position of the CCD vision component 8. At the same time, when continuing the motion control and moving, the left flying needle 9 or the right flying needle 10 is made to contact the carrier block 7. At this time, the carrier block 7 is connected to the left flying needle 9 or the right flying needle 10, and a voltage is output to the motion control card to generate a signal, thereby sending out a signal to stop the motion control, and calculating the moving distance at this time, comparing the deviation with the center position of the CCD vision component 8, so as to accurately calculate the positions of the left flying needle 9 and the right flying needle 10. This kind of needle comparison method adopts an automatic needle comparison method throughout the process, with high accuracy, low calibration difficulty, more convenient needle replacement, and simple operation.
[0018] Specifically, a Z-axis motion control 6 is fixedly connected to the upper end of the carrier platform 1, and a carrier moving plate 14 is slidably arranged on the upper end of the Z-axis motion control 6, and a carrier block 7 is fixedly connected to one side of the carrier moving plate 14.
[0019] In this embodiment, by setting the Z-axis motion control 6, the carrier moving plate 14 can be motion-controlled to move the carrier, so that the carrier block 7 can be motion-controlled.
[0020] Furthermore, a closing and opening mechanism 15 is fixedly connected to the lower end of the rotating mechanism 13, and a left flying needle 9 and a right flying needle 10 are fixedly connected to both sides of the closing and opening mechanism 15.
[0021] In this embodiment, by setting the rotating mechanism 13 to cooperate with the rotation and closing and opening of the closing and opening mechanism 15, the flying needles on both sides can perform processing at different angles.
[0022] Although the embodiments of the present invention have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions, and variations can be made to these embodiments without departing from the principles and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. An automatic calibration mechanism for the first-piece inspection flying probe, comprising a carrier platform (1), characterized in that: A carrier block (7) is provided at the upper end of the carrier platform (1). One side of the upper end of the carrier platform (1) is fixedly connected to a fixed platform (2). An X-axis motion control (3) is fixedly connected to the upper end of the fixed platform (2). A first moving block (4) is slidably connected to the upper end of the X-axis motion control (3). A Y-axis motion control (5) is fixedly connected to one side of the first moving block (4). A second moving block (11) is slidably connected to one side of the Y-axis motion control (5). A CCD vision component (8) is fixedly connected to one side of the second moving block (11). A fixing frame (12) is fixedly connected to one side of the second moving block (11). A rotating mechanism (13) is fixedly connected to the lower side of one side of the fixing frame (12). A left flying needle (9) is fixedly connected to the lower side of one side of the rotating mechanism (13). A right flying needle (10) is fixedly connected to the lower side of the other side of the rotating mechanism (13).
2. The first-piece inspection flying probe automatic calibration mechanism according to claim 1, wherein: A Z-axis motion control (6) is fixedly connected to the upper end of the carrier platform (1). A carrier moving plate (14) is slidably arranged at the upper end of the Z-axis motion control (6). A carrier block (7) is fixedly connected to one side of the carrier moving plate (14).
3. The first-piece inspection flying needle automatic calibration mechanism according to claim 1, characterized in that: A clamping mechanism (15) is fixedly connected to the lower end of the rotating mechanism (13). The left flying needle (9) and the right flying needle (10) are fixedly connected to both sides of the clamping mechanism (15).