Probe boot device for detecting arc area of composite material
By designing the probe boot device of frame components, radial components and contact components, the problem that existing devices can only install probes of a single size and radius is solved, achieving the effect of no blind spots in detection and short replacement time and low cost.
Patent Information
- Application Number
- CN202421846913.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-01
- Publication Date
- 2025-07-01
- Estimated Expiration
- 2034-08-01
AI Technical Summary
The existing probe boot device can only be equipped with arc-surface phased array probes of size and radius. There are blind spots for part end detection, making it difficult to ensure that the probe position is in the optimal detection position, and the replacement time is long and the cost is high.
A probe boot device including a frame assembly, a radial assembly and a contact assembly is designed. The frame assembly is used to adjust the lateral position of the probe, the radial assembly is used to adjust the radial position of the probe, and the contact assembly is used to realize the relative position of the probe and the arc area of the material, ensuring that the encoder wheel is perpendicular to the surface of the part, and the wheel contacts are aligned with the center of the width of the probe, so as to achieve no blind spots when end detection is achieved.
The installation of arc-surface phased array probes of different sizes and radii is realized to ensure that there are no blind spots in the inspection, reduce replacement time and cost, and expand the scope of use of boot components.
Smart Images

Figure CN223051260U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of non-destructive testing of composite materials, in particular to a probe boot device for detecting the arc area of composite materials. Background Art
[0002] In the prior art, due to its excellent designability, fatigue resistance, corrosion resistance and high weight reduction efficiency, composite materials have become the necessary materials for various advanced aircraft structures. The application proportion of composite materials on advanced aircraft has been increasing year by year. In the production stage of composite components, the non-destructive testing of composite materials mainly adopts conventional ultrasonic longitudinal wave testing technology and ultrasonic longitudinal wave phased array testing technology. Conventional ultrasonic longitudinal wave testing technology includes manual contact reflection method, automatic reflection method, manual penetration method, automatic water spray penetration method, etc. Ultrasonic longitudinal wave phased array technology includes manual contact reflection method, automatic reflection method, manual penetration method, automatic water spray penetration method, etc. Usually, for plane or curved surface parts with an area greater than 1 square foot or a curvature radius greater than 1 inch and an opening greater than 4 inches, an automatic penetration large ultrasonic C-scan system is used for detection to improve the detection efficiency; for complex-shaped composite parts that do not meet the above conditions, due to the limitation of shape or detection space, automated detection cannot achieve complete ultrasonic coverage of the component, and generally a manual ultrasonic conventional system or phased array system is used for detection. For example, small-radius arcs and narrow flanges are commonly present in composite wing ribs, spars and stringers of panels. For the large and small structures, see the attached drawings of the specification Figure 1 、 Figure 2 , automated detection cannot detect the arc area and flange area, and for these areas, manual methods are usually used for detection.
[0003] There are various ultrasonic detection methods for composite materials. However, no matter which detection method is used, a suitable probe boot assembly must be used to achieve effective detection of composite components. Different detection methods result in different structures and functions of the probe boot assembly. For example, the structures and functions of the contact method boot and the immersion method boot are different, the structures and functions of the immersion method boot and the water spray method boot are different, the structures and functions of the boots for automated detection and manual detection are different, different configurations of the detection probes lead to different structures and functions of the probe boot assembly, different configurations of the composite materials to be detected also result in different structures and functions of the probe boot assembly, and the structures and functions of the probe boots for detecting flat surfaces, convex surfaces and concave surfaces are different. Designing and manufacturing specific probe boot assemblies according to the detection method, probe configuration and part configuration is the key to the successful implementation of ultrasonic detection of composite materials.
[0004] The ultrasonic phased array manual immersion reflection method is the development direction for detecting the arc area of composite parts. Its detection principle is described as follows: When detecting the fillet area of a composite part, an ultrasonic phased array probe usually uses a concave arc surface linear array probe. A typical configuration is 36 - 64 wafers, with a frequency of 3.5 MHz and an arc radius of 0.5 - 1.5 inches. The more the number of wafers, the larger the arc radius, and the larger the probe size. The larger the arc radius of the part, the more wafers and the larger the arc radius of the probe are required. The elements of the concave arc surface linear array probe are arranged in an arc. The ultrasonic waves emitted by each element are naturally geometrically focused at the center of the arc of the arc array, where the sound field energy is the strongest. When the center of curvature of the workpiece arc coincides with the center of the probe arc, during scanning, each element is directly excited without any delay processing, and the ultrasonic beam of each element can be made to be incident at 90 degrees to the surface of the part fillet, as if performing a planar detection, greatly reducing the energy loss of the ultrasonic waves before they enter the workpiece surface. The entire arc area can be covered in one scan. During the production process of composite materials, this kind of fillet detection can be carried out from the inside or the outside of the fillet. Usually, it is carried out from the arc surface on the side of the laying tooling. See the attached Figure 3 When using the immersion reflection method to detect the fillet area of composite materials, an arc surface phased array probe is used, and the detection of an arc area with a certain radius can only be achieved through an arc surface delay boot assembly.
[0005] However, the probe boot device in the prior art has the following disadvantages:
[0006] 1) It can only install an arc surface phased array probe of one size and radius, increasing the number of boot assemblies;
[0007] 2) It can install a distance encoder, but its contacts are generally not aligned and synchronized with the phased array probe, resulting in a detection blind area problem at the end of the part;
[0008] 3) It can only adjust and fix the probe water distance. When the arc of the part is irregular, it is very difficult to ensure that the probe position is in the best detection position, and the quality of the detection image deteriorates;
[0009] 4) It can only detect an arc area with a single size of opening angle. When there are many types of part opening angles, the quantity requirements for boot assemblies, probes, and encoders are large, the cost increases significantly, and the replacement time is long.
[0010] The Chinese invention patent with the application number 201210014624.X discloses an ultrasonic transducer fixture for detecting the convex R area of a composite material, which consists of a guiding frame, a transducer seat and a locking handle; the guiding frame is composed of two guiding plates with the same structure, two connecting pins and four screws. However, this ultrasonic transducer fixture for detecting the convex R area of a composite material can only install an arc surface phased array probe of one size and radius, increasing the number of boot components. It can install a distance encoder, but its contacts are not aligned and synchronized with the phased array probe, resulting in a detection blind area problem at the end of the part. It can only adjust and fix the water distance of the probe. When the arc of the part is irregular, it is difficult to ensure that the probe position is in the best detection position, and the quality of the detection image decreases. It can only detect the arc area with a single large and small opening angle. When there are many types of part opening angles, the number of boot components, probes and encoders required is large, the cost increases significantly, and the replacement time is long. Utility Model Content
[0011] The purpose of the present utility model is to provide a probe boot device for detecting the arc area of a composite material.
[0012] To achieve the above purpose, the technical solution proposed by the present utility model is:
[0013] A probe boot device for detecting the arc area of a composite material, including a base and an ultrasonic phased array probe, the ultrasonic phased array probe is arranged inside the base, and further includes a frame assembly for adjusting the lateral position of the ultrasonic phased array probe, a radial assembly for adjusting the radial position of the ultrasonic phased array probe, and a contact assembly for realizing the relative positioning of the probe boot device and the material arc area. The frame assembly is arranged on the upper part of the base, the radial assembly is assembled inside the frame assembly, and the contact assembly is configured on the lower part of the base.
[0014] The base is composed of frame side plates and frame connectors. There are two groups of frame side plates, and the two groups of frame side plates are arranged side by side at intervals. A lateral installation groove is provided on the opposite side of the two groups of frame side plates. There are two groups of frame connectors, and the two groups of frame connectors are symmetrically arranged between the two groups of frame side plates, and their two ends are respectively fixedly connected to the two groups of frame side plates through fixing screws.
[0015] The frame component includes an installation frame, a connection frame, and frame locking screws. The installation frame is arranged on one inner side of the base and is slidably connected to the base through a transverse installation groove. The connection frame is arranged on one side of the installation frame and is fixedly connected to the installation frame through connection screws. The connection frame is slidably connected to the base through the transverse installation groove. The installation frame and the connection frame together form a transverse moving frame structure. The frame locking screws are arranged corresponding to the installation frame on one side of the base and penetrate through the base and are threadedly connected to the base. The frame locking screws are arranged corresponding to the transverse installation groove, and the frame locking screws are in contact with the installation frame.
[0016] The radial component includes a radial installation block, a radial coarse adjustment structure, and a radial fine adjustment structure. The radial installation block is arranged at the upper end of the installation frame and is fixedly connected to the installation frame through fixing screws. The radial coarse adjustment structure is arranged at the bottom of the radial installation block and is located inside the installation frame. The radial fine adjustment structure is assembled on one side of the radial coarse adjustment structure close to the connection frame.
[0017] The radial coarse adjustment structure includes coarse adjustment guide rods, coarse adjustment sliders, coarse adjustment springs, and coarse adjustment locking screws. There are two groups of coarse adjustment guide rods. The two groups of coarse adjustment guide rods are symmetrically arranged at the bottom of the radial installation block, and their upper ends are fixedly connected to the radial installation block through fixing screws. The coarse adjustment sliders are arranged at the lower parts of the two groups of coarse adjustment guide rods and are sleeved and connected to the coarse adjustment guide rods. A radial installation groove is arranged on one side of the coarse adjustment slider close to the connection frame. There are two groups of coarse adjustment springs. The two groups of coarse adjustment springs are respectively sleeved on the upper parts of the two groups of coarse adjustment guide rods and are located between the coarse adjustment slider and the radial installation block. The coarse adjustment locking screws are arranged corresponding to the coarse adjustment sliders at the middle part of one side of the installation frame away from the connection frame and penetrate through the installation frame and are threadedly connected to the installation frame. The coarse adjustment locking screws are in contact with the coarse adjustment sliders.
[0018] The radial fine adjustment structure includes a fine adjustment slider, a fine adjustment guide rod, and a fine adjustment handle. The fine adjustment slider is arranged on one side of the coarse adjustment slider close to the connection frame and is slidably connected to the coarse adjustment slider through a radial installation groove. The ultrasonic phased array probe is arranged on one side of the fine adjustment slider close to the connection frame. The fine adjustment guide rod is vertically arranged in the middle of the fine adjustment slider and penetrates through the fine adjustment slider and is threadedly connected to the fine adjustment slider. The upper part of the fine adjustment guide rod is rotatably connected to the coarse adjustment slider. The fine adjustment handle is arranged at the upper end of the fine adjustment guide rod and is fixedly connected to the fine adjustment guide rod.
[0019] It further includes a fine-tuning mounting block and a fine-tuning locking screw. The fine-tuning mounting block is arranged at the lower end of the fine-tuning guide rod and is rotatably connected to the fine-tuning guide rod. The fine-tuning mounting block is fixedly connected to the coarse-tuning slider. The fine-tuning locking screw is arranged corresponding to the fine-tuning slider on one side of the coarse-tuning slider and penetrates through the coarse-tuning slider and is threadedly connected to the coarse-tuning slider. The fine-tuning locking screw abuts against the fine-tuning slider.
[0020] The contact assembly includes a hinge structure, a contact plate, and a coding structure. There are two groups of hinge structures, and the two groups of hinge structures are symmetrically arranged on both sides of the base. There are two groups of contact plates, and the two groups of contact plates are symmetrically arranged on the lower sides of both sides of the two groups of hinge structures. One of the contact plates is provided with a mounting opening corresponding to the coding structure, and the coding structure is arranged at the mounting opening of the corresponding contact plate.
[0021] The hinge structure includes a mounting rotating shaft, a gear hinge, and a spread angle locking screw. There are two mounting rotating shafts, and the two mounting rotating shafts are symmetrically arranged in the middle of one side of the base and are fixedly connected to the base. There are two gear hinges, and the gear ends of the two gear hinges are respectively arranged in the middle of the two mounting rotating shafts and are rotatably connected to the corresponding mounting rotating shafts. The gear ends of the two gear hinges are meshed and connected with each other. The contact plate is arranged at the lower part of the hinge end of the gear hinge and is fixedly connected to the corresponding gear hinge. There are two spread angle locking screws, and the two spread angle locking screws are symmetrically arranged in the middle of one side of the base and are threadedly connected to the base. The spread angle locking screw penetrates through the corresponding gear hinge.
[0022] The coding structure includes a coding mounting piece and an encoder. The coding mounting piece is arranged at the hinge end of one of the gear hinges and is fixedly connected to the corresponding gear hinge through a fixing screw. The encoder is arranged at the end of the coding mounting piece away from the gear hinge and is fixedly connected to the coding mounting piece through a fixing screw. The encoder is arranged at the mounting opening of the corresponding contact plate.
[0023] The beneficial effects of the present utility model are as follows:
[0024] The cooperation of the frame assembly and the radial assembly can meet the installation requirements of phased array probes with different sizes and radii of arc surfaces, ensure that the encoder wheel is perpendicular to the part surface, the wheel contact point is aligned with the center of the probe width synchronously, achieve no blind area in the end detection, make the arc center and the center symmetry line of the probe coincide with the arc center and the center symmetry line of the part, ensure that the sound beam is perpendicular to the arc surface of the part, and is provided with a contact assembly, which can adjust the spread angle of the contact plate to both sides simultaneously and fix it according to the size of the part spread angle, so that the center line of the probe remains unchanged, so as to expand the use range of the boot assembly. Description of the Drawings
[0025] Figure 1 It is a schematic diagram of the structure of the arc area of the composite material L-shaped configuration;
[0026] Figure 2 It is a schematic diagram of the structure of the arc area of the composite material T-shaped configuration;
[0027] Figure 3 It is a schematic diagram of the overall structure of the present utility model;
[0028] Figure 4 It is a side view of the present utility model;
[0029] Figure 5 It is a sectional view of the cooperation between the radial component and the base of the present utility model;
[0030] Figure 6 It is a bottom view of the present utility model;
[0031] Figure 7 It is a schematic diagram of the cooperation between the contact component and the base of the present utility model.
[0032] In the figure: 1. Base; 2. Ultrasonic phased array probe; 3. Installation frame; 4. Connection frame; 5. Frame locking screw; 6. Radial installation block; 7. Coarse adjustment guide rod; 8. Coarse adjustment slider; 9. Coarse adjustment spring; 10. Coarse adjustment locking screw; 11. Fine adjustment slider; 12. Fine adjustment guide rod; 13. Fine adjustment handle; 14. Fine adjustment installation block; 15. Fine adjustment locking screw; 16. Contact plate; 17. Installation rotating shaft; 18. Gear hinge; 19. Angular locking screw; 20. Coding installation part; 21. Encoder. Specific embodiments
[0033] The following further describes the present utility model in detail with reference to the accompanying drawings.
[0034] A probe boot device for detecting the arc area of a composite material includes a base 1 and an ultrasonic phased array probe 2. The ultrasonic phased array probe 2 is arranged inside the base 1. It further includes a frame assembly for adjusting the lateral position of the ultrasonic phased array probe 2, a radial assembly for adjusting the radial position of the ultrasonic phased array probe 2, and a contact assembly for realizing the relative positioning of the probe boot device and the material arc area. The frame assembly is arranged on the upper part of the base 1, the radial assembly is assembled inside the frame assembly, and the contact assembly is configured on the lower part of the base 1. The schematic diagram of the overall structure of the present utility model is as Figure 3 shown.
[0035] The base 1 is composed of frame side plates and frame connectors. There are two groups of frame side plates. The two groups of frame side plates are arranged side by side at intervals, and a transverse installation groove is provided on the opposite side of the two groups of frame side plates. There are two groups of frame connectors. The two groups of frame connectors are symmetrically arranged between the two groups of frame side plates, and their two ends are respectively fixedly connected to the two groups of frame side plates through fixing screws. Among them, the frame side plates are used to form the main structure of the base 1, the frame connectors are used to connect the two groups of frame side plates to form a frame-type base 1 structure, and the transverse installation groove is used as an installation structure on the frame side plates to provide sliding installation support for the frame assembly. The side view of the present utility model is as shown in Figure 4 shown.
[0036] The frame assembly includes an installation frame 3, a connection frame 4, and a frame locking screw 5. The installation frame 3 is arranged on one side inside the base 1 and is slidably connected to the base 1 through the transverse installation groove. The connection frame 4 is arranged on one side of the installation frame 3 and is fixedly connected to the installation frame 3 through a connection screw. The connection frame 4 is slidably connected to the base 1 through the transverse installation groove. The installation frame 3 and the connection frame 4 together form a transverse moving frame structure. The frame locking screw 5 is arranged corresponding to the installation frame 3 on one side of the base 1 and penetrates through the base 1 and is threadedly connected to the base 1. The frame locking screw 5 is arranged corresponding to the transverse installation groove, and the frame locking screw 5 abuts against the installation frame 3. The frame assembly is cooperated by the installation frame 3, the connection frame 4, and the frame locking screw 5 to form a frame structure, so as to provide installation support for the radial assembly and drive the radial assembly to move horizontally along the transverse installation groove to adjust its horizontal position. Among them, the installation frame 3 is used to provide installation support for the radial assembly and laterally slidably connect the radial assembly to the base 1 under the action of the transverse installation groove. The connection frame 4 is used to jointly form a frame structure with the installation frame 3. The frame locking screw 5 is used as a positioning structure of the frame assembly, and the frame assembly can be fixed at a specified position by rotating the frame locking screw 5 to make it abut against the installation frame 3.
[0037] The radial assembly includes a radial installation block 6, a radial coarse adjustment structure, and a radial fine adjustment structure. The radial installation block 6 is arranged at the upper end of the installation frame 3 and is fixedly connected to the installation frame 3 through a fixing screw. The radial coarse adjustment structure is arranged at the bottom of the radial installation block 6 and is located inside the installation frame 3. The radial fine adjustment structure is assembled on the side of the radial coarse adjustment structure close to the connection frame 4. The radial assembly is cooperated by the radial installation block 6, the radial coarse adjustment structure, and the radial fine adjustment structure to form a radial moving structure of the probe boot device to adjust the radial position of the ultrasonic phased array probe 2. Among them, the radial installation block 6 is used to provide installation support for the radial coarse adjustment structure. The radial coarse adjustment structure is used to roughly adjust the radial position of the radial fine adjustment structure and the probe boot device. The radial fine adjustment structure is used to finely adjust the radial position of the ultrasonic phased array probe 2. The cross-sectional view of the cooperation between the radial assembly of the present utility model and the base 1 is as shown in Figure 5 shown.
[0038] The radial coarse adjustment structure includes a coarse adjustment guide rod 7, a coarse adjustment slider 8, a coarse adjustment spring 9, and a coarse adjustment locking screw 10. There are two sets of coarse adjustment guide rods 7, which are symmetrically arranged at the bottom of the radial mounting block 6, and their upper ends are fixedly connected to the radial mounting block 6 through fixing screws. The coarse adjustment slider 8 is arranged at the lower part of the two sets of coarse adjustment guide rods 7 and is sleeved on the coarse adjustment guide rods 7. A radial mounting groove is provided on one side of the coarse adjustment slider 8 close to the connection frame 4. There are two sets of coarse adjustment springs 9, which are respectively sleeved on the upper parts of the two sets of coarse adjustment guide rods 7 and are located between the coarse adjustment slider 8 and the radial mounting block 6. The coarse adjustment locking screw 10 is correspondingly arranged at the middle part of the side of the mounting frame 3 away from the connection frame 4 and penetrates through the mounting frame 3 and is threadedly connected to the mounting frame 3. The coarse adjustment locking screw 10 abuts against the coarse adjustment slider 8. The radial coarse adjustment structure cooperates with the coarse adjustment guide rod 7, the coarse adjustment slider 8, the coarse adjustment spring 9, and the coarse adjustment locking screw 10 to coarsely adjust the radial position of the radial fine adjustment structure and the ultrasonic phased array probe 2. Among them, the coarse adjustment guide rod 7 is used to provide guiding support for the coarse adjustment slider 8, the coarse adjustment slider 8 is used to provide mounting support for the radial fine adjustment structure to drive the radial fine adjustment structure to slide along the coarse adjustment guide rod 7, so as to coarsely adjust the radial position of the radial fine adjustment structure and the ultrasonic phased array probe 2. The coarse adjustment spring 9 is used to provide elastic support for the coarse adjustment slider 8, and the coarse adjustment locking screw 10 is used to fix the position of the coarse adjustment slider 8 to fix the radial position of the radial fine adjustment structure and the ultrasonic phased array probe 2. The position of the coarse adjustment slider 8 can be fixed by rotating the coarse adjustment locking screw 10 to make it abut against the coarse adjustment slider 8.
[0039] The radial fine-tuning structure includes a fine-tuning slider 11, a fine-tuning guide rod 12, and a fine-tuning handle 13. The fine-tuning slider 11 is arranged on the side of the coarse-tuning slider 8 close to the connection frame 4 and is slidably connected to the coarse-tuning slider 8 through a radial installation groove. The ultrasonic phased array probe 2 is arranged on the side of the fine-tuning slider 11 close to the connection frame 4. The fine-tuning guide rod 12 is vertically arranged in the middle of the fine-tuning slider 11 and penetrates through the fine-tuning slider 11 and is threadedly connected to the fine-tuning slider 11. The upper part of the fine-tuning guide rod 12 is rotatably connected to the coarse-tuning slider 8. The fine-tuning handle 13 is arranged at the upper end of the fine-tuning guide rod 12 and is fixedly connected to the fine-tuning guide rod 12. The radial fine-tuning structure cooperates with the fine-tuning slider 11, the fine-tuning guide rod 12, and the fine-tuning handle 13 to finely adjust the radial position of the ultrasonic phased array probe 2. Among them, the fine-tuning slider 11 is used to provide installation support for the ultrasonic phased array probe 2 and perform lifting actions under the action of the fine-tuning guide rod 12 to drive the ultrasonic phased array probe 2 to lift, so as to finely adjust the radial position of the ultrasonic phased array probe 2. The fine-tuning guide rod 12 is used to provide installation support for the fine-tuning slider 11 and adjust the radial position of the fine-tuning slider 11. The fine-tuning handle 13 is used as a handle structure on the fine-tuning guide rod 12 for the staff to control the fine-tuning guide rod 12.
[0040] It also includes a fine-tuning installation block 14 and a fine-tuning locking screw 15. The fine-tuning installation block 14 is arranged at the lower end of the fine-tuning guide rod 12 and is rotatably connected to the fine-tuning guide rod 12. The fine-tuning installation block 14 is fixedly connected to the coarse-tuning slider 8. The fine-tuning locking screw 15 is arranged on one side of the coarse-tuning slider 8 corresponding to the fine-tuning slider 11 and penetrates through the coarse-tuning slider 8 and is threadedly connected to the coarse-tuning slider 8. The fine-tuning locking screw 15 abuts against the fine-tuning slider 11. Among them, the fine-tuning installation block 14 is used as an installation structure on the coarse-tuning slider 8 to provide installation support for the fine-tuning guide rod 12. The fine-tuning locking screw 15 is used to position the fine-tuning slider 11. The bottom view of the present invention is as Figure 6 shown.
[0041] The contact assembly includes a hinge structure, a contact plate 16, and a coding structure. There are two sets of hinge structures, which are symmetrically arranged on both sides of the base 1. There are two sets of contact plates 16, which are symmetrically arranged on the lower sides of the two sets of hinge structures. One of the contact plates 16 is provided with an installation opening corresponding to the coding structure, and the coding structure is arranged at the installation opening of the corresponding contact plate 16. The contact assembly is combined with the hinge structure, the contact plate 16, and the coding structure to form the contact structure of the probe boot device to achieve the positioning between the probe boot device and the arc area of the material to be measured. Among them, the hinge structure is used to provide installation support for the contact plate 16 and ensure the synchronous movement of the two sets of contact plates 16. The contact plate 16 is used to form the contact structure of the probe boot device to achieve the positioning between the probe boot device and the arc area of the material to be measured under the action of the hinge structure. The coding structure is used to form the encoder 21 part in the probe boot device. The schematic diagram of the cooperation between the contact assembly of the present invention and the base 1 is as Figure 7 shown.
[0042] The hinge structure includes an installation rotating shaft 17, a gear hinge 18, and an included angle locking screw 19. There are two installation rotating shafts 17, which are symmetrically arranged in the middle of one side of the base 1 and fixedly connected to the base 1. There are two gear hinges 18, and the gear ends of the two gear hinges 18 are respectively arranged in the middle of the two installation rotating shafts 17 and rotatably connected to the corresponding installation rotating shafts 17. The gear ends of the two gear hinges 18 are meshed and connected to each other. The contact plate 16 is arranged below the hinge end of the gear hinge 18 and fixedly connected to the corresponding gear hinge 18. There are two included angle locking screws 19, which are symmetrically arranged in the middle of one side of the base 1 and threadedly connected to the base 1. The included angle locking screw 19 penetrates through the corresponding gear hinge 18. The hinge structure is combined with the installation rotating shaft 17, the gear hinge 18, and the included angle locking screw 19 to provide installation support for the contact plate 16 and realize the synchronous movement of the two sets of contact plates 16. Among them, the installation rotating shaft 17 is used to provide rotational support for the gear hinge 18 to rotatably connect the gear hinge 18 to the base 1. The gear hinge 18 is used to provide installation support for the contact plate 16 and realize the synchronous movement of the two sets of contact plates 16 through the meshing connection of the two gear ends. The included angle locking screw 19 is used to lock the installation angle of the gear hinge 18 to lock the included angle between the two sets of contact plates 16.
[0043] The coding structure includes a coding mounting member 20 and an encoder 21. The coding mounting member 20 is arranged at the hinge end of one set of gear hinges 18 and is fixedly connected to the corresponding gear hinge 18 through a fixing screw. The encoder 21 is arranged at one end of the coding mounting member 20 away from the gear hinge 18 and is fixedly connected to the coding mounting member 20 through a fixing screw. The encoder 21 is arranged at the installation opening of the corresponding contact plate 16. The coding structure, through the cooperation of the coding mounting member 20 and the encoder 21, constitutes the encoder 21 part in the probe boot device. Among them, the coding mounting member 20 is used to mount the encoder 21 on one set of gear hinges 18, and the encoder 21 is used to convert angular displacement or linear displacement into an electrical signal.
[0044] Among them, the contact plate 16 is supported by hard plastic, which can reduce friction and prevent scratching the surface of parts.
[0045] The process of the probe boot device detecting the arc area of the composite material part from the outer arc is as follows:
[0046] a. Install a suitable ultrasonic arc surface phased array probe on this boot assembly and connect it to the ultrasonic phased array instrument;
[0047] b. Install the corresponding encoder 21 on this boot assembly and connect it to the ultrasonic phased array instrument;
[0048] c. Fix the composite material profile part to be detected in the water tank, power on the instrument, and open the appropriate detection setting file in the ultrasonic phased array instrument;
[0049] d. Contact plate 16 angular adjustment: Loosen the angular locking screw 19, straddle this boot assembly on the outer arc surface of the arc area of the composite material part to be detected, make the two contact plates 16 tightly adhere to the flanges on both sides of the arc, and then tighten the angular locking screw 19;
[0050] e. Horizontally adjust the ultrasonic arc surface phased array probe to the optimal position through the frame assembly: Loosen the frame locking screw 5, gently push the frame assembly, observe the display of the ultrasonic instrument S, and when it shows a vertically symmetric arc shape, tighten the frame locking screw 5. At this time, the symmetric center line of the probe arc surface coincides with the symmetric center line of the part arc;
[0051] f. Radially adjust the ultrasonic arc surface phased array probe to the optimal position through the radial assembly: Loosen the coarse adjustment locking screw 10, pinch the fine adjustment handle 13 and lift it up and down for coarse adjustment. Observe the display of the ultrasonic instrument S. When it basically shows a vertical line shape, tighten the coarse adjustment locking screw 10, and then rotate the fine adjustment handle 13 to finely adjust the fine adjustment slider 11 until the S display shows an ideal vertical line shape, and then tighten the fine adjustment locking screw 15. At this time, the center of the probe coincides with the center of the part arc;
[0052] g. Move and scan the boot assembly along the length direction of the part arc for inspection.
[0053] Among them, the ultrasonic phased array instrument and the inspection setup file can both adopt the general equipment and files in this field.
[0054] Among them, by installing and designing the encoder 21, the wheel contact point of the encoder 21 is aligned with the center of the probe width, achieving a blind zone of 0 for end detection.
[0055] Among them, the radial coarse and fine adjustments of the probe are achieved through the coarse adjustment guide rod 7 and the fine adjustment guide rod 12.
[0056] Among them, the lateral adjustment of the probe is achieved through the lateral installation groove structure.
[0057] Among them, the included angle of the contact plate 16 can be adjusted to increase or decrease simultaneously on both sides through the double gear hinge 18 mechanism.
[0058] Among them, phased array probes with different sizes and radii of arc surfaces can be installed, such as: GE 115-000-531, GE115-000-532, GE 115-000-607, 00-010878-IPEX. They are convenient to replace and disassemble, expanding the application range of this boot assembly, and enabling the inspection of arc regions with different outer arc radii (0.1 - 1.0 inches) of composite material profiles.
[0059] Among them, a water-immersed miniature distance encoder 21 (ENC1-10-DE) can be installed and ensure that the wheel of the distance encoder 21 is perpendicular to the part surface, and the wheel contact point is aligned and synchronized with the center of the probe width, achieving a blind zone of 0 for end detection. The distance between the wheel and the center line of the probe is as small as possible to ensure the inspection of the arc region of the composite material profile structure with a flanging width of 1 inch or more than 1 inch. It is convenient to replace and disassemble, expanding the application range of this boot assembly.
[0060] Among them, the water distance of the probe can be coarsely and finely adjusted along the center symmetry line of the probe to the optimal position and locked. The adjustment is convenient, making the arc center of the probe coincide with the arc center of the part, and ensuring that the sound beam is perpendicular to the arc surface of the part.
[0061] Among them, the lateral position of the probe can be adjusted along the vertical direction of the symmetry line of the probe to the optimal position and locked. The adjustment is convenient, making the center symmetry line of the probe coincide with the center symmetry line of the part arc.
[0062] Working principle:
[0063] Through the cooperation of the frame component, the radial component and the contact component, a probe boot device is jointly formed, which can install phased array probes with different sizes and radii of arcs to expand its uses. The ultrasonic phased array probe 2 is installed on the fine-tuning slider 11 by screws. The frame component adjusts the lateral positions of the radial component and the ultrasonic phased array probe 2, and the radial component adjusts the radial position of the ultrasonic phased array probe 2, so that the center of the probe arc and the symmetric center line coincide with the center of the part arc and the center line. The double-gear hinge 18 mechanism is used to realize that the opening angle of the contact plate 16 can be adjusted to become larger or smaller simultaneously on both sides, and the position of the opening angle center line remains basically unchanged.
[0064] The beneficial effects of the present invention are that the cooperation of the frame component and the radial component can meet the installation requirements of phased array probes with different sizes and radii of arc surfaces, and can ensure that the encoder wheel is perpendicular to the part surface and the wheel contact point is aligned with the center of the probe width synchronously, realizing no blind area in the end detection. It can make the center of the probe arc and the center symmetry line coincide with the center of the part arc and the center symmetry line, ensuring that the sound beam is perpendicular to the part arc surface. There is a contact component, which can adjust the opening angle of the contact plate to become larger or smaller on both sides simultaneously with the size of the part opening angle and fix it, so that the center line of the probe remains unchanged, so as to expand the use range of the boot component.
[0065] The above has described in detail an embodiment of the present invention, but the content is only the preferred embodiment of the present invention and cannot be considered as limiting the implementation scope of the present invention. All equivalent changes and improvements made according to the scope of the present invention application should still fall within the scope covered by the patent of the present invention.
Claims
1. A probe boot device for detecting a composite material arc region, comprising a base (1) and an ultrasonic phased array probe (2), wherein the ultrasonic phased array probe (2) is arranged on the inner side of the base (1), and is characterized in that: It also comprises a frame assembly for adjusting the lateral position of the ultrasonic phased array probe (2), a radial assembly for adjusting the radial position of the ultrasonic phased array probe (2), and a contact assembly for realizing the relative positioning of the probe shoe device and the arc area of the material, wherein the frame assembly is arranged on the upper part of the base (1), the radial assembly is assembled on the inner side of the frame assembly, and the contact assembly is arranged on the lower part of the base (1).
2. A probe boot device for detecting arc areas of composite materials as claimed in claim 1, characterized in that: The base (1) is composed of frame side panels and frame connecting members, wherein two groups of frame side panels are provided, the two groups of frame side panels are arranged side by side and spaced apart, and the two groups of frame side panels are provided with transverse mounting grooves on opposite sides, and two groups of frame connecting members are provided, the two groups of frame connecting members are symmetrically arranged between the two groups of frame side panels, and the two ends of the frame connecting members are fixedly connected to the two groups of frame side panels by fixing screws respectively.
3. A probe boot device for detecting arc areas of composite materials as claimed in claim 2, characterized in that: The frame assembly comprises a mounting frame (3), a connecting frame (4) and a frame locking screw (5); the mounting frame (3) is arranged on one side of the interior of the base (1) and is slidably connected to the base (1) via a transverse mounting groove; the connecting frame (4) is arranged on one side of the mounting frame (3) and is fixedly connected to the mounting frame (3) via a connecting screw; the connecting frame (4) is slidably connected to the base (1) via the transverse mounting groove; the mounting frame (3) and the connecting frame (4) together constitute a transverse movable frame structure; the frame locking screw (5) is arranged on one side of the base (1) corresponding to the mounting frame (3) and penetrates the base (1) and is threadedly connected to the base (1); the frame locking screw (5) is arranged corresponding to the transverse mounting groove; and the frame locking screw (5) abuts against the mounting frame (3).
4. A probe boot device for detecting arc areas of composite materials as claimed in claim 3, characterized in that: The radial assembly comprises a radial mounting block (6), a radial coarse adjustment structure and a radial fine adjustment structure, wherein the radial mounting block (6) is arranged at the upper end of the mounting frame (3) and is fixedly connected to the mounting frame (3) via fixing screws, the radial coarse adjustment structure is arranged at the bottom of the radial mounting block (6) and is located on the inner side of the mounting frame (3), and the radial fine adjustment structure is assembled on a side of the radial coarse adjustment structure close to the connecting frame (4).
5. A probe shoe device for detecting arc areas of composite materials as claimed in claim 4, characterized in that: The radial coarse adjustment structure comprises a coarse adjustment guide rod (7), a coarse adjustment slider (8), a coarse adjustment spring (9) and a coarse adjustment locking screw (10). The coarse adjustment guide rod (7) is provided with two groups. The two groups of coarse adjustment guide rods (7) are symmetrically arranged at the bottom of the radial mounting block (6) and the upper ends thereof are fixedly connected to the radial mounting block (6) by fixing screws. The coarse adjustment slider (8) is arranged at the lower part of the two groups of coarse adjustment guide rods (7) and is sleeve-connected to the coarse adjustment guide rods (7). The coarse adjustment slider (8) is close to one side of the connecting frame (4). A radial mounting groove is provided on the side, and two groups of coarse adjustment springs (9) are provided. The two groups of coarse adjustment springs (9) are respectively mounted on the upper parts of the two groups of coarse adjustment guide rods (7) and are located between the coarse adjustment slider (8) and the radial mounting block (6). The coarse adjustment locking screw (10) is arranged at the middle part of the side of the mounting frame (3) away from the connecting frame (4) corresponding to the coarse adjustment slider (8) and passes through the mounting frame (3) and is threadedly connected to the mounting frame (3). The coarse adjustment locking screw (10) abuts against the coarse adjustment slider (8).
6. A probe shoe device for detecting arc areas of composite materials as claimed in claim 5, characterized in that: The radial fine adjustment structure comprises a fine adjustment slider (11), a fine adjustment guide rod (12) and a fine adjustment handle (13); the fine adjustment slider (11) is arranged on a side of the coarse adjustment slider (8) close to the connecting frame (4) and is slidably connected to the coarse adjustment slider (8) through a radial mounting groove; the ultrasonic phased array probe (2) is arranged on a side of the fine adjustment slider (11) close to the connecting frame (4); the fine adjustment guide rod (12) is vertically arranged in the middle of the fine adjustment slider (11) and passes through the fine adjustment slider (11) and is threadedly connected to the fine adjustment slider (11); the upper part of the fine adjustment guide rod (12) is rotatably connected to the coarse adjustment slider (8); the fine adjustment handle (13) is arranged at the upper end of the fine adjustment guide rod (12) and is fixedly connected to the fine adjustment guide rod (12).
7. A probe shoe device for detecting arc areas of composite materials as claimed in claim 6, characterized in that: It also includes a fine adjustment mounting block (14) and a fine adjustment locking screw (15), wherein the fine adjustment mounting block (14) is arranged at the lower end of the fine adjustment guide rod (12) and is rotatably connected to the fine adjustment guide rod (12), the fine adjustment mounting block (14) is fixedly connected to the coarse adjustment slider (8), the fine adjustment locking screw (15) is arranged on one side of the coarse adjustment slider (8) corresponding to the fine adjustment slider (11) and passes through the coarse adjustment slider (8) and is threadedly connected to the coarse adjustment slider (8), and the fine adjustment locking screw (15) abuts against the fine adjustment slider (11).
8. A probe shoe device for detecting arc areas of composite materials as claimed in claim 7, characterized in that: The contact assembly comprises a hinge structure, a contact plate (16) and a coding structure, wherein the hinge structure is provided with two groups, and the two groups of hinge structures are symmetrically arranged on both sides of the base (1), and the contact plates (16) are provided with two groups, and the two groups of contact plates (16) are symmetrically arranged on both sides of the lower part of the two groups of hinge structures, wherein one group of the contact plates (16) is provided with a mounting opening corresponding to the coding structure, and the coding structure is arranged at the mounting opening of the corresponding contact plate (16).
9. A probe shoe device for detecting arc areas of composite materials as claimed in claim 8, characterized in that: The hinge structure comprises a mounting shaft (17), a gear hinge (18) and an angle locking screw (19). The mounting shaft (17) is provided with two, and the two mounting shafts (17) are symmetrically arranged in the middle of one side of the base (1) and fixedly connected to the base (1). The gear hinge (18) is provided with two, and the gear ends of the two gear hinges (18) are respectively arranged in the middle of the two mounting shafts (17) and are rotatably connected to the corresponding mounting shafts (17). The gear ends of the two gear hinges (18) are meshed and connected with each other. The contact plate (16) is arranged at the lower part of the hinge end of the gear hinge (18) and is fixedly connected to the corresponding gear hinge (18). The angle locking screw (19) is provided with two, and the two angle locking screws (19) are symmetrically arranged in the middle of one side of the base (1) and are threadedly connected to the base (1). The angle locking screw (19) passes through the corresponding gear hinge (18).
10. A probe shoe device for detecting arc areas of composite materials as claimed in claim 9, characterized in that: The encoding structure comprises an encoding mounting member (20) and an encoder (21), wherein the encoding mounting member (20) is arranged at a hinge end of one group of the gear hinges (18) and is fixedly connected to the corresponding gear hinge (18) via a fixing screw, and the encoder (21) is arranged at an end of the encoding mounting member (20) away from the gear hinge (18) and is fixedly connected to the encoding mounting member (20) via a fixing screw, and the encoder (21) is arranged at a mounting opening of the corresponding contact plate (16).
Citation Information
Patent Citations
Ultrasonic transducer clamp for detecting convex R region of composite material
CN102590350A