Built-in composite material arc area detection probe boot device
By designing a built-in composite arc area detection probe boot device, the problem that existing devices cannot install probes of different sizes and radii at the same time and have detection blind spots is solved, and efficient detection of composite arc areas and flexible probe position adjustment is achieved.
Patent Information
- Application Number
- CN202422081667.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-27
- Publication Date
- 2025-07-01
- Estimated Expiration
- 2034-08-27
AI Technical Summary
The existing composite arc area detection probe boot device cannot install arc surface phased array probes of different sizes and radii at the same time, and there are problems such as difficulty in detecting blind spots and position adjustment of probes.
A built-in composite arc area detection probe boot device is designed, including an ultrasonic phased array probe, a probe mount, a base mechanism, an adjustment mechanism and a contact mechanism. The device can install arc-surface phased array probes of different sizes and radii, and achieve optimal position adjustment of the probe through an adjustment mechanism, which ensures that the probe is aligned with the inner side of the arc area of the material.
It realizes efficient detection of arc areas of different sizes and radii, eliminates detection blind spots, improves the flexibility and accuracy of probe position adjustment, and expands the scope of use of boot components.
Smart Images

Figure CN223051263U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of non-destructive testing of composite materials, in particular to an in-built detection probe boot device for 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 in 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. The conventional ultrasonic longitudinal wave testing technology includes manual contact reflection method, automatic reflection method, manual penetration method, automatic water spray penetration method, etc. The 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 one square foot or a curvature radius greater than one inch and an opening greater than four 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 found in composite wing ribs, spars and stringers of the skin. For the size structure, see the attached drawings of the specification Figure 1 、 Figure 2 , automated detection cannot detect the arc area and flange area, and these areas are usually detected by the manual method.
[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 automatic detection and manual detection are different, different configurations of the detection probe result in different structures and functions of the probe boot assembly, different configurations of the composite materials to be detected 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 a specific probe boot assembly 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 adopts 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, the larger the probe size, and 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 manner. The ultrasonic waves emitted by each element are naturally geometrically focused at the center of the arc of the arc array, and the sound field energy is the strongest at this point. When the curvature center 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 inner side of the fillet or from the outer side of the fillet. Usually, it is detected from the arc surface on the side of the laying tooling, but factors such as the surface state of the detection surface and the size of the detection space still need to be considered. See the attached drawings of the specification. Figure 3 When using the immersion reflection method to detect the fillet area of a composite material, an arc surface phased array probe is adopted, and the detection of an arc area with a certain radius can only be achieved through the 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 water distance of the probe. 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 and opening angle. When there are many types of part opening angles, the number of boot assemblies, probes, and encoders required is large, the cost increases significantly, and the replacement time is long.
[0010] The Chinese invention patent with the application number 201610424401.9 discloses a reference block for ultrasonic testing of the R - angle structure of a composite material. Its artificial defect is placed in the single - curvature arc surface that connects two flat surfaces in the R - angle structure. The artificial defect is rectangular in shape. The long side of the artificial defect is in the same direction as the arc direction of the single - curvature arc surface of the R - angle structure of the reference block, and the short side of the artificial defect is in the same direction as the extension direction of the single - curvature arc surface of the R - angle structure of the reference block. Moreover, the length of the short side is the maximum allowable defect size specified in the corresponding acceptance level of the R - angle structure to be detected. However, this kind of reference block for ultrasonic testing of the R - angle structure of a composite material cannot install an arc - surface phased - array probe, the detection method is slow, it can only detect the arc area with a single - size opening angle. When there are many types of part opening angles, the quantity requirements of the boot assembly, probe, and encoder are 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 built - in detection probe boot device for the arc area of a composite material.
[0012] To achieve the above - mentioned purpose, the technical solution proposed by the present utility model is:
[0013] A built - in detection probe boot device for the arc area of a composite material, including an ultrasonic phased - array probe and a probe mounting base. The ultrasonic phased - array probe is assembled at one end of the probe mounting base. It also includes a base mechanism for providing installation support for the ultrasonic phased - array probe, an adjustment mechanism for adjusting the position of the ultrasonic phased - array probe, and a contact mechanism for realizing the relative positioning between the probe boot device and the inner side of the material arc area. The base mechanism is arranged outside the ultrasonic phased - array probe, the adjustment mechanism is configured between the base mechanism and the ultrasonic phased - array probe, and the contact mechanism is assembled at one end of the base mechanism close to the ultrasonic phased - array probe.
[0014] The base mechanism includes a base support frame and a base mounting frame. The base support frame is arranged on one side of the ultrasonic phased - array probe. The base mounting frame is arranged on one side of the base support frame and is fixedly connected to the base support frame by screws. The base mounting frame and the base support frame together form a semi - enclosed frame structure, and the ultrasonic phased - array probe is located inside the semi - enclosed frame structure.
[0015] The base support frame is set as an L - shaped support frame structure, and a guiding groove is correspondingly arranged on the side of the base support frame opposite to the base mounting frame.
[0016] The adjusting mechanism includes a lateral movement component and a radial movement component. The lateral movement component is assembled inside the base support frame and the base mounting frame. The radial movement component is assembled inside the lateral movement component. The ultrasonic phased array probe is assembled at one end of the radial movement component and is configured inside the lateral movement component through the radial movement component.
[0017] The lateral movement component includes a lateral support frame, a lateral mounting frame, and a guiding convex edge. The lateral support frame is arranged inside the base mounting frame and is slidably connected to the base mounting frame. The lateral mounting frame is arranged on the side of the lateral support frame away from the base mounting frame and is fixedly connected to the lateral support frame by screws. The lateral mounting frame is slidably connected to the base support frame. There are two groups of guiding convex edges. The two groups of guiding convex edges are respectively arranged on the outer sides of the lateral support frame and the lateral mounting frame and are fixedly connected to the corresponding lateral support frame or the lateral mounting frame. The lateral support frame and the lateral mounting frame are respectively slidably connected to the corresponding base mounting frame and the base support frame through the guiding convex edges and guiding grooves.
[0018] It further includes a lateral locking screw. The lateral locking screw is arranged on the outer side of the base support frame and penetrates through the base support frame and is threadedly connected to the base support frame. The lateral locking screw abuts against the lateral mounting frame.
[0019] The radial movement component includes a moving slider, a moving screw rod, and a moving handle. The moving slider is arranged inside the lateral support frame and is slidably connected to the lateral support frame. The ultrasonic phased array probe is arranged on the side of the moving slider away from the lateral support frame and is fixedly connected to the moving slider by screws. The lateral support frame is provided with a guiding groove corresponding to the moving slider. One side of the moving slider close to the lateral support frame is provided with a guiding block corresponding to the guiding groove. The moving slider is slidably connected to the lateral support frame through the guiding block and the guiding groove. The moving screw rod is arranged on the side of the lateral support frame close to the moving slider and is rotatably connected to the lateral support frame through a limit fixing sleeve. The moving slider is sleeved on the moving screw rod through a moving sliding sleeve and is slidably connected to the moving screw rod. The moving handle is arranged at one end of the moving screw rod away from the moving slider and is fixedly connected to the moving screw rod.
[0020] It further includes a radial locking screw. The radial locking screw is arranged on the outer side of the base mounting frame and penetrates through the base mounting frame and the lateral support frame and is threadedly connected to the base mounting frame and the lateral support frame. The radial locking screw abuts against the moving screw rod.
[0021] The contact mechanism includes an included angle locking screw, a gear hinge, a contact plate, and a coding component. There are two sets of the included angle locking screws, and each set of the included angle locking screws consists of two locking screws arranged side by side at intervals. The two sets of the included angle locking screws are oppositely arranged at one end of the base support frame and the base mounting frame close to the ultrasonic phased array probe and penetrate through the base support frame or the base mounting frame and are threadedly connected to the corresponding base support frame or the base mounting frame. There are two sets of the gear hinges, and each set of the gear hinges consists of two symmetrically arranged hinge structures. The gear ends of the two sets of the gear hinges are respectively arranged in the middle of the two sets of the included angle locking screws and are rotatably connected to the corresponding included angle locking screws. The gear ends of the two hinge structures in each set of the gear hinges are meshed and connected with each other. The gear hinge is rotatably connected to the corresponding base support frame or the base mounting frame through the included angle locking screw. There are two sets of the contact plates, and the two sets of the contact plates are respectively arranged at the hinge ends of the two sets of the gear hinges and are fixedly connected to the corresponding gear hinges. One of the contact plates is provided with an installation opening corresponding to the coding component, and the coding component is arranged at the installation opening of the corresponding contact plate.
[0022] The coding component includes a coding mounting piece and an encoder. The coding mounting piece is arranged at the hinge end of one of the sets of the gear hinges and is fixedly connected to the corresponding gear hinge through a fixing screw. The encoder is arranged at one end of the coding mounting piece away from the gear hinge and is fixedly connected to the coding mounting piece through a mounting rod. The encoder is arranged at the installation opening of the corresponding contact plate.
[0023] The beneficial effects of the present utility model are as follows:
[0024] Phased array probes with arc surfaces of different sizes and radii can be installed to expand the usage range of the boot assembly. It is possible to make the encoder wheel perpendicular to the part surface and the wheel contact point aligned with the center of the probe width synchronously, achieving a zero blind zone for end detection. The water distance of the probe can be adjusted along the center symmetry line of the probe to the optimal position and fixed, so that the arc center of the probe coincides with the arc center of the part to ensure that the sound beam is perpendicular to the arc surface of the part. 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 fixed, so that the center symmetry line of the probe coincides with the center symmetry line of the part arc. The included angle of the contact plate can be adjusted and fixed simultaneously on both sides according to the included angle of the part, basically keeping the center line of the probe unchanged to expand the usage range of the boot assembly and achieving no blind zone for end detection. Description of the Drawings
[0025] Figure 1 It is a schematic diagram of the structure of the arc region of the composite material L-shaped configuration;
[0026] Figure 2It is a schematic diagram of the structure of the circular arc area of the composite material T-shaped configuration;
[0027] Figure 3 It is the detection principle of the circular arc surface linear array probe from the inner side of the circular arc;
[0028] Figure 4 It is a schematic diagram of the overall structure of the present invention;
[0029] Figure 5 It is a sectional view of the present invention;
[0030] Figure 6 It is a schematic diagram of the cooperation between the adjusting mechanism and the base mechanism of the present invention;
[0031] Figure 7 It is a schematic diagram of the cooperation between the radial moving component and the base mechanism of the present invention;
[0032] Figure 8 It is a schematic diagram of the cooperation between the contact mechanism and the base mechanism of the present invention.
[0033] In the figure: 1. Ultrasonic phased array probe; 2. Probe mounting seat; 3. Base support frame; 4. Base mounting frame; 5. Horizontal support frame; 6. Horizontal mounting frame; 7. Guide rib; 8. Horizontal locking screw; 9. Moving slider; 10. Moving screw; 11. Moving handle; 12. Radial locking screw; 13. Angular locking screw; 14. Gear hinge; 15. Contact plate; 16. Coding mounting part; 17. Encoder. Detailed implementation manners
[0034] The present invention will be further described in detail below with reference to the accompanying drawings.
[0035] An in-built composite material circular arc area detection probe boot device includes an ultrasonic phased array probe 1 and a probe mounting seat 2. The ultrasonic phased array probe 1 is assembled at one end of the probe mounting seat 2. It further includes a base mechanism for providing installation support for the ultrasonic phased array probe 1, an adjusting mechanism for adjusting the position of the ultrasonic phased array probe 1, and a contact mechanism for realizing the relative positioning between the probe boot device and the inner side of the material circular arc area. The base mechanism is arranged outside the ultrasonic phased array probe 1, the adjusting mechanism is configured between the base mechanism and the ultrasonic phased array probe 1, and the contact mechanism is assembled at one end of the base mechanism close to the ultrasonic phased array probe 1. The schematic diagram of the overall structure of the present invention is as Figure 4 shown.
[0036] The base mechanism includes a base support frame 3 and a base mounting frame 4. The base support frame 3 is disposed on one side of the ultrasonic phased array probe 1. The base mounting frame 4 is disposed on one side of the base support frame 3 and is fixedly connected to the base support frame 3 by screws. The base mounting frame 4 and the base support frame 3 together form a semi-enclosed frame structure. The ultrasonic phased array probe 1 is located inside the semi-enclosed frame structure. The base support frame 3 is configured as an L-shaped support frame structure, and a guiding groove is correspondingly provided on the side of the base support frame 3 opposite to the base mounting frame 4. The base mechanism is cooperated by the base support frame 3 and the base mounting frame 4 to form a semi-enclosed base structure, thereby providing installation support for the adjustment mechanism. Among them, the base support frame 3 is used as the main structure of the base and provides installation support for the base mounting frame 4. The base mounting frame 4 is used to jointly form a semi-enclosed base structure with the base support frame 3, thereby providing installation support for the adjustment mechanism. The guiding groove is used as a guiding installation structure inside the base mechanism, thereby providing installation support for the adjustment mechanism. The cross-sectional view of the present utility model is as shown in Figure 5 shown.
[0037] The adjustment mechanism includes a transverse movement component and a radial movement component. The transverse movement component is assembled inside the base support frame 3 and the base mounting frame 4. The radial movement component is assembled inside the transverse movement component. The ultrasonic phased array probe 1 is assembled at one end of the radial movement component and is disposed inside the transverse movement component through the radial movement component. The adjustment mechanism is cooperated by the transverse movement component and the radial movement component to provide installation support for the ultrasonic phased array probe 1 and adjust the position of the ultrasonic phased array probe 1. Among them, the transverse movement component is used to adjust the transverse position of the radial movement component and the ultrasonic phased array probe 1. The radial movement component is used to adjust the radial position of the ultrasonic phased array probe 1. The schematic diagram of the cooperation between the adjustment mechanism and the base mechanism of the present utility model is as shown in Figure 6 shown.
[0038] The lateral movement component includes a lateral support frame 5, a lateral mounting frame 6, and a guiding convex edge 7. The lateral support frame 5 is arranged inside the base mounting frame 4 and is slidably connected to the base mounting frame 4. The lateral mounting frame 6 is arranged on the side of the lateral support frame 5 away from the base mounting frame 4 and is fixedly connected to the lateral support frame 5 by screws. The lateral mounting frame 6 is slidably connected to the base support frame 3. There are two groups of guiding convex edges 7, and the two groups of guiding convex edges 7 are respectively arranged on the outer sides of the lateral support frame 5 and the lateral mounting frame 6 and are fixedly connected to the corresponding lateral support frame 5 or lateral mounting frame 6. The lateral support frame 5 and the lateral mounting frame 6 are respectively slidably connected to the corresponding base mounting frame 4 and base support frame 3 through the guiding convex edges 7 and guiding grooves. The lateral movement component cooperates with the lateral support frame 5, the lateral mounting frame 6, and the guiding convex edge 7 to adjust the lateral positions of the radial movement component and the ultrasonic phased array probe 1. Among them, the lateral support frame 5 is used to provide installation support for the radial movement component and the ultrasonic phased array probe 1. The lateral mounting frame 6 is used to jointly form a frame structure with the lateral support frame 5 and provide sliding support for the radial movement component and the ultrasonic phased array probe 1 under the action of the guiding convex edge 7. The guiding convex edge 7 is used as a sliding installation structure on the side of the lateral support frame 5 and the lateral mounting frame 6 to slidably connect the lateral support frame 5 and the lateral mounting frame 6 to the base mounting frame 4 and the base support frame 3.
[0039] It further includes a lateral locking screw 8. The lateral locking screw 8 is arranged on the outer side of the base support frame 3 and penetrates through the base support frame 3 and is threadedly connected to the base support frame 3. The lateral locking screw 8 abuts against the lateral mounting frame 6. Among them, the lateral locking screw 8 is used as a locking structure for the lateral movement component, and the lateral movement component can be locked by rotating the lateral locking screw 8 to make it abut against the lateral mounting frame 6.
[0040] The radial movement component includes a moving slider 9, a moving screw 10 and a moving handle 11. The moving slider 9 is arranged inside the transverse support frame 5 and is slidably connected to the transverse support frame 5. The ultrasonic phased array probe 1 is arranged on the side of the moving slider 9 away from the transverse support frame 5 and is fixedly connected to the moving slider 9 by screws. The transverse support frame 5 is provided with a guide groove corresponding to the moving slider 9. On the side of the moving slider 9 close to the transverse support frame 5, a guide block is provided corresponding to the guide groove. The moving slider 9 is slidably connected to the transverse support frame 5 through the guide block and the guide groove. The moving screw 10 is arranged on the side of the transverse support frame 5 close to the moving slider 9 and is rotatably connected to the transverse support frame 5 through a limit fixing sleeve. The moving slider 9 is sleeved on the moving screw 10 through a moving sliding sleeve and is slidably connected to the moving screw 10. The moving handle 11 is arranged at one end of the moving screw 10 away from the moving slider 9 and is fixedly connected to the moving screw 10. The radial movement component cooperates with the moving slider 9, the moving screw 10 and the moving handle 11 to adjust the radial position of the ultrasonic phased array probe 1. Among them, the moving slider 9 is used to provide installation support for the ultrasonic phased array probe 1 and slidably connect the ultrasonic phased array probe 1 to the transverse support frame 5, so as to adjust the radial position of the ultrasonic phased array probe 1. The moving screw 10 is used to drive the moving slider 9 to slide up and down along the transverse support frame 5 by rotating between it and the transverse support frame 5. The moving handle 11 is used as a handle structure on the moving screw 10, and the moving screw 10 can be rotated through the moving handle 11, so as to realize the adjustment operation of the radial position of the ultrasonic phased array probe 1. The schematic diagram of the cooperation between the radial movement component of the present utility model and the base mechanism is as Figure 7 shown.
[0041] It further includes a radial locking screw 12. The radial locking screw 12 is arranged outside the base mounting frame 4 and penetrates through the base mounting frame 4 and the transverse support frame 5 and is threadedly connected to the base mounting frame 4 and the transverse support frame 5. The radial locking screw 12 abuts against the moving screw 10. Among them, the radial locking screw 12 is used as a locking structure of the radial movement component, and the radial movement component can be locked by rotating the radial locking screw 12 to make it abut against the moving screw 10.
[0042] The contact mechanism includes a flare locking screw 13, a gear hinge 14, a contact plate 15, and a coding component. There are two sets of flare locking screws 13, and each set of flare locking screws 13 consists of two locking screws arranged side by side at intervals. The two sets of flare locking screws 13 are oppositely arranged at one end of the base support frame 3 and the base mounting frame 4 close to the ultrasonic phased array probe 1 and penetrate the base support frame 3 or the base mounting frame 4 to be threadedly connected to the corresponding base support frame 3 or base mounting frame 4. There are two sets of gear hinges 14, and each set of gear hinges 14 consists of two symmetrically arranged hinge structures. The gear ends of the two sets of gear hinges 14 are respectively arranged in the middle of the two sets of flare locking screws 13 and are rotatably connected to the corresponding flare locking screws 13. The gear ends of the two hinge structures in each set of gear hinges 14 are meshed and connected to each other. The gear hinge 14 is rotatably connected to the corresponding base support frame 3 or base mounting frame 4 through the flare locking screw 13. There are two sets of contact plates 15, and the two sets of contact plates 15 are respectively arranged at the hinge ends of the two sets of gear hinges 14 and are fixedly connected to the corresponding gear hinges 14. One of the sets of contact plates 15 is provided with a mounting opening corresponding to the coding component, and the coding component is arranged at the mounting opening of the corresponding contact plate 15. The contact mechanism is combined with the flare locking screw 13, the gear hinge 14, the contact plate 15, and the coding component to form the contact structure of the probe boot device to achieve the positioning between the probe boot device and the inner arc area of the material to be measured. Among them, the flare locking screw 13 is used to provide rotational support for the gear hinge 14 to rotatably connect the gear hinge 14 to the base mechanism, and the installation angle of the gear hinge 14 can be locked by tightening the flare locking screw 13, so as to lock the flare angle between the two sets of contact plates 15. The gear hinge 14 is used to provide installation support for the contact plate 15 and to achieve the synchronous movement of the two sets of contact plates 15 through the meshing connection of the two gear ends. The contact plate 15 is used to form the contact structure of the probe boot device to achieve the positioning between the probe boot device and the inner arc area of the material to be measured under the action of the hinge structure. The coding component is used to form the encoder 17 part in the probe boot device. The schematic diagram of the cooperation between the contact mechanism of the present invention and the base mechanism is as Figure 8 shown.
[0043] The coding component includes a coding mounting member 16 and an encoder 17. The coding mounting member 16 is arranged at the hinge end of one of the sets of gear hinges 14 and is fixedly connected to the corresponding gear hinge 14 through a fixing screw. The encoder 17 is arranged at the end of the coding mounting member 16 away from the gear hinge 14 and is fixedly connected to the coding mounting member 16 through a mounting rod. The encoder 17 is arranged at the mounting opening of the corresponding contact plate 15. The coding component is combined with the coding mounting member 16 and the encoder 17 to form the encoder 17 part in the probe boot device. Among them, the coding mounting member 16 is used to mount the encoder 17 on one of the sets of gear hinges 14, and the encoder 17 is used to convert angular displacement or linear displacement into an electrical signal.
[0044] The process of the present probe boot device for detecting the arc area of a composite material part from the inner arc is as follows:
[0045] a. Install an applicable ultrasonic arc surface phased array probe on this boot assembly and connect the probe to an ultrasonic phased array instrument;
[0046] b. Install the corresponding encoder 17 on this boot assembly and connect it to the ultrasonic phased array instrument;
[0047] c. Fix the composite material profile part to be detected in a water tank, power on the instrument, and open the appropriate detection setting file in the instrument;
[0048] d. Contact plate 15 angular adjustment: Loosen the angular locking screw 13, lean this boot assembly against the inner arc flanging surface of the arc area of the composite material part to be detected, make the two contact plates 15 tightly adhere to the flanges on both sides of the arc, and then tighten the angular locking screw 13;
[0049] e. Horizontally adjust the ultrasonic arc surface phased array probe to the optimal position through the horizontal movement assembly: Loosen the horizontal locking screw 8, gently push the horizontal movement assembly, observe the display of the ultrasonic instrument S, and when it shows a vertically symmetric arc shape, tighten the horizontal locking screw 8. At this time, the symmetric center line of the probe arc surface coincides with the symmetric center line of the part arc;
[0050] f. Radially adjust the ultrasonic arc surface phased array probe to the optimal position through the radial movement assembly: Loosen the radial locking screw 12, rotate the adjustment handle for adjustment until the display of S shows a vertical line shape, and then tighten the radial locking screw 12. At this time, the center of the probe arc coincides with the center of the part arc;
[0051] g. Operate this boot assembly to move and scan for detection along the length direction of the part arc.
[0052] Among them, by designing the installation of the encoder 17, the wheel contact point of the encoder 17 is aligned with the center of the probe width, so that the end detection blind area is zero.
[0053] Among them, the ultrasonic phased array instrument and the detection setting file can both use general equipment and files in this field.
[0054] Among them, phased array probes with different sizes and radii of arc surfaces can be installed, such as: GE 115-000-501, GE115-000-531, 00-011509-IPEX, 00-010925-IPEX. The replacement and disassembly are convenient, which expands the application range of this boot assembly and realizes the detection of different inner arc radii (0.17 - 0.40 inches) of the composite material profile structure.
[0055] Detection of the arc region
[0056] Among them, the opening angle of the contact plate 15 can be adjusted to increase or decrease simultaneously on both sides through the double-gear hinge 14 mechanism.
[0057] Among them, the water distance of the probe can be adjusted along the central symmetry line of the probe to the optimal position and locked. The adjustment is convenient, so that the arc center of the probe coincides with the arc center of the part, ensuring that the sound beam is perpendicular to the arc surface of the part.
[0058] 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, so that the central symmetry line of the probe coincides with the central symmetry line of the arc of the part.
[0059] Among them, the opening angle of the contact plate 15 can be continuously adjusted on both sides according to the opening angle of the part and locked. The opening angle adjustment range is 70 - 142 degrees. The adjustment is convenient, and the center line of the probe remains basically unchanged to expand the use range of the boot assembly.
[0060] Working principle:
[0061] By installing and designing the encoder 17, the contact point of the encoder 17 wheel is aligned with the center of the probe width, so that the blind area at the end is 0. By fixing the encoder 17 on the boot, it is ensured that the roller of the encoder 17 can rub against the inner arc surface of the part and is perpendicular to this surface. The roller contact point is on the center line of the probe width. The distance between the encoder 17 roller and the center line of the inner arc surface of the part is 0.8" - 1.2". The radial adjustment of the probe is realized through the guide groove and screw structure. The probe moves up and down along the radial guide groove so that the arc center of the probe moves along the center line of the probe to coincide with the arc center of the part. Push the lateral movement assembly to make the probe move laterally along the guide groove so that the symmetric center line of the probe arc coincides with the center line of the part arc. Use the gear hinge 14 structure to fix the rotating shaft to fix the contact plate 15 assembly on the base mechanism. The center line connection of the fixed rotating shafts of the gear hinge 14 on each side is parallel to the guide groove and symmetrically distributed with respect to the symmetric center line of the probe arc, so that the opening angle of the contact plate 15 can increase or decrease simultaneously on both sides, and is fixed to a single opening angle, and the position of the opening angle center line remains basically unchanged.
[0062] The beneficial effects of the present utility model are as follows: phased array probes with arc surfaces of different sizes and radii can be installed to expand the usage range of the boot assembly. It is possible to synchronize the encoder wheel to be perpendicular to the part surface and align the wheel contact point with the center of the probe width, achieving a zero blind zone for end detection. The water distance of the probe can be adjusted to the optimal position and fixed along the center symmetry line of the probe, so that the center of the probe arc coincides with the center of the part arc to ensure that the sound beam is perpendicular to the part arc surface. The lateral position of the probe can be adjusted to the optimal position and fixed along the direction perpendicular to the symmetry line of the probe, so that the center symmetry line of the probe coincides with the center symmetry line of the part arc. The opening angle of the contact plate can be adjusted and fixed simultaneously on both sides according to the opening angle of the part, basically keeping the center line of the probe unchanged to expand the usage range of the boot assembly and achieving no blind zone for end detection.
[0063] The above has described in detail one embodiment of the present utility model, but the content is only the preferred embodiment of the present utility model and cannot be considered as limiting the implementation scope of the present utility model. All equivalent changes and improvements made according to the scope of the application of the present utility model should still fall within the patent coverage scope of the present utility model.
Claims
1. A built-in composite material arc area detection probe boot device, comprising an ultrasonic phased array probe (1) and a probe mounting seat (2), wherein the ultrasonic phased array probe (1) is mounted on one end of the probe mounting seat (2), characterized in that: It also comprises a base mechanism for providing mounting support for the ultrasonic phased array probe (1), an adjustment mechanism for adjusting the position of the ultrasonic phased array probe (1), and a contact mechanism for achieving relative positioning between a probe boot device and the inner side of a material arc region; the base mechanism is arranged on the outer side of the ultrasonic phased array probe (1), the adjustment mechanism is arranged between the base mechanism and the ultrasonic phased array probe (1), and the contact mechanism is assembled at one end of the base mechanism close to the ultrasonic phased array probe (1).
2. A built-in composite material arc area detection probe boot device as claimed in claim 1, characterized in that: The base mechanism comprises a base support frame (3) and a base mounting frame (4); the base support frame (3) is arranged on one side of the ultrasonic phased array probe (1); the base mounting frame (4) is arranged on one side of the base support frame (3) and is fixedly connected to the base support frame (3) by screws; the base mounting frame (4) and the base support frame (3) together form a semi-enclosed frame structure; and the ultrasonic phased array probe (1) is located on the inner side of the semi-enclosed frame structure.
3. A built-in composite material arc area detection probe boot device as claimed in claim 2, characterized in that: The base support frame (3) is configured as an L-shaped support frame structure, and a guide groove is correspondingly provided on a side of the base support frame (3) opposite to the base mounting frame (4).
4. A built-in composite material arc area detection probe boot device as claimed in claim 3, characterized in that: The adjustment mechanism comprises a lateral moving component and a radial moving component, the lateral moving component is mounted on the inner side of the base support frame (3) and the base mounting frame (4), the radial moving component is mounted on the inner side of the lateral moving component, and the ultrasonic phased array probe (1) is mounted on one end of the radial moving component and is arranged on the inner side of the lateral moving component through the radial moving component.
5. A built-in composite material arc area detection probe boot device as claimed in claim 4, characterized in that: The transverse moving assembly comprises a transverse supporting frame (5), a transverse mounting frame (6) and a guide protrusion (7); the transverse supporting frame (5) is arranged on the inner side of the base mounting frame (4) and is slidably connected to the base mounting frame (4); the transverse mounting frame (6) is arranged on a side of the transverse supporting frame (5) away from the base mounting frame (4) and is fixedly connected to the transverse supporting frame (5) by screws; the transverse mounting frame (6) is slidably connected to the base supporting frame (3); two groups of guide protrusions (7) are provided; the two groups of guide protrusions (7) are respectively arranged on the outer sides of the transverse supporting frame (5) and the transverse mounting frame (6) and are fixedly connected to the corresponding transverse supporting frame (5) or the transverse mounting frame (6); the transverse supporting frame (5) and the transverse mounting frame (6) are respectively slidably connected to the corresponding base mounting frame (4) and the base supporting frame (3) by the guide protrusions (7) and the guide grooves.
6. A built-in composite material arc area detection probe boot device as claimed in claim 5, characterized in that: It also includes a transverse locking screw (8), which is arranged on the outside of the base support frame (3) and passes through the base support frame (3) and is threadedly connected to the base support frame (3), and the transverse locking screw (8) abuts against the transverse mounting frame (6).
7. A built-in composite material arc area detection probe boot device as claimed in claim 6, characterized in that: The radial moving assembly comprises a moving slider (9), a moving screw (10) and a moving handle (11); the moving slider (9) is arranged on the inner side of the transverse support frame (5) and is slidably connected to the transverse support frame (5); the ultrasonic phased array probe (1) is arranged on a side of the moving slider (9) away from the transverse support frame (5) and is fixedly connected to the moving slider (9) by screws; the transverse support frame (5) is provided with a guide groove corresponding to the moving slider (9); and the side of the moving slider (9) close to the transverse support frame (5) is provided with a guide groove corresponding to the guide groove. The movable slider (9) is slidably connected to the transverse support frame (5) through a guide block and a guide groove, the movable screw rod (10) is arranged on a side of the transverse support frame (5) close to the movable slider rod (9) and is rotatably connected to the transverse support frame (5) through a limiting fixing sleeve, the movable slider rod (9) is sleeved on the movable screw rod (10) through a movable sliding sleeve and is slidably connected to the movable screw rod (10), and the movable handle (11) is arranged on an end of the movable screw rod (10) away from the movable slider rod (9) and is fixedly connected to the movable screw rod (10).
8. A built-in composite material arc area detection probe boot device as claimed in claim 7, characterized in that: It also includes a radial locking screw (12), which is arranged on the outside of the base mounting frame (4) and passes through the base mounting frame (4) and the lateral support frame (5) and is threadedly connected to the base mounting frame (4) and the lateral support frame (5), and the radial locking screw (12) abuts against the moving screw (10).
9. A built-in composite material arc area detection probe boot device as claimed in claim 8, characterized in that: The contact mechanism comprises an angle locking screw (13), a gear hinge (14), a contact plate (15) and a coding assembly. The angle locking screw (13) is provided with two groups, each group of the angle locking screw (13) is composed of two locking screws arranged side by side and spaced apart. The two groups of the angle locking screws (13) are relatively arranged on the base support frame (3) and the base mounting frame (4) at one end close to the ultrasonic phased array probe (1) and penetrate the base support frame (3) or the base mounting frame (4) and are threadedly connected to the corresponding base support frame (3) or the base mounting frame (4). The gear hinge (14) is provided with two groups, each group of the gear hinge (14) is composed of two symmetrically arranged hinge structures. The two groups of gear hinges (14) are provided with two groups of gear hinges (14). The gear ends of the chain (14) are respectively arranged at the middle of the two groups of the angle locking screws (13) and are rotatably connected to the corresponding angle locking screws (13); the gear ends of the two hinge structures in each group of the gear hinges (14) are meshed and connected with each other; the gear hinges (14) are rotatably connected to the corresponding base support frame (3) or the base mounting frame (4) through the angle locking screws (13); two groups of contact plates (15) are provided; the two groups of contact plates (15) are respectively arranged at the hinge ends of the two groups of gear hinges (14) and are fixedly connected to the corresponding gear hinges (14); one group of the contact plates (15) is provided with an installation opening corresponding to the coding component; the coding component is provided at the installation opening of the corresponding contact plate (15).
10. A built-in composite material arc area detection probe boot device as claimed in claim 9, characterized in that: The encoding component comprises an encoding mounting member (16) and an encoder (17), wherein the encoding mounting member (16) is arranged at a hinge end of one group of the gear hinges (14) and is fixedly connected to the corresponding gear hinge (14) via a fixing screw, and the encoder (17) is arranged at an end of the encoding mounting member (16) away from the gear hinge (14) and is fixedly connected to the encoding mounting member (16) via a mounting support rod, and the encoder (17) is arranged at a mounting opening of the corresponding contact plate (15).
Citation Information
Patent Citations
Reference test block for ultrasonic detection of composite-material R corner structure
CN106404920A