Workbench for detecting and recording defects of aeronautical parts

Abstract

The utility model discloses an aviation part defect detection recording workbench, and relates to the technical field of part defect detection. The device comprises a base body, and further comprises a conveying belt arranged in a working table, and two groups of detection frames are arranged on the upper end face of the working table at equal intervals; the visual detection equipment is arranged in the center of one group of detection frames, and an ultrasonic detection module is arranged at the lower end of the other group of detection frames; the recording plates are arranged on the left side and the right side of the connecting plate, and recording mechanisms are arranged on the inner sides of the recording plates. According to the utility model, the visual detection device and the ultrasonic detection module are arranged, so that the same group of aeronautical parts can be respectively detected, the equipment has two detection modes, the detection error of the aeronautical parts can be reduced, the detection efficiency of the aeronautical parts can be ensured, and if the aeronautical parts have defects, the equipment can be used for detecting the aeronautical parts. And the arranged micro push rod can push the marking pen to make contact with the aviation parts, and then the defective aviation parts can be marked and recorded.

Description

Technical Field

[0001] The utility model belongs to the technical field of component defect detection, in particular to an aviation component defect detection and recording workbench. Background Art

[0002] Visual inspection is the earliest and most widely used nondestructive testing method in the field of nondestructive testing of aviation parts. Although there are many nondestructive testing methods in aircraft inspection, 80% of the nondestructive testing of aircraft parts still needs to be completed with the help of visual inspection. In recent years, aviation parts have continuously applied the latest scientific and technological achievements, with more advanced performance, more complex materials, and more comprehensive technologies, which has brought great challenges to the inspection and means of aviation parts.

[0003] After the aviation parts are processed and produced, the parts need to be inspected. After searching, a multifunctional aviation parts defect inspection and recording workbench with a publication number of CN206840014U is found. Specifically, the whiteboard 91 is supported by a first folding rod 95, a second folding rod 96 and a connecting shaft 94 after the inspection is completed, and then the staff records the information of the aviation parts on the whiteboard 91. With the rapid development of the times, the efficiency of aviation parts inspection has also been improved. After the aviation parts are inspected, the defects of the parts need to be recorded. In the above scheme, the staff needs to manually record the information on the whiteboard. Although the recording can be done, the work efficiency is relatively low, resulting in a reduction in the intelligence of the workbench, which is difficult to meet the high-speed aviation parts inspection and recording. Utility Model Content

[0004] In view of the above-mentioned shortcomings of the prior art, the utility model provides an aviation component defect detection and recording workbench, which can effectively solve the problems of the prior art.

[0005] In order to solve the above technical problems, the utility model is realized by the following technical solutions:

[0006] The utility model is an aviation parts defect detection and recording workbench, comprising a base body and a workbench arranged on the upper end of the base body, and also comprising:

[0007] The conveyor belt is arranged inside the workbench, and two sets of detection racks are arranged at equal distances on the upper end surface of the workbench;

[0008] The visual inspection equipment is arranged in the center of one set of inspection racks, and an ultrasonic inspection module is arranged at the lower end of another set of inspection racks;

[0009] The recording plate is arranged on the left and right sides of the connecting plate, and a recording mechanism is arranged on the inner side of the recording plate for recording defective aviation parts;

[0010] The inspection mechanism is set at one end of the workbench away from the visual inspection equipment and is used to discharge defective aviation parts.

[0011] Furthermore, an electric push rod is provided on the upper end surface of the other group of detection frames, and a connecting plate is fixed to the output end of the electric push rod, and the lower end surface of the connecting plate is connected to the ultrasonic detection module.

[0012] Furthermore, the recording mechanism includes a connecting frame, a micro push rod, and a marking pen. The connecting frame is slidably connected to the left and right sides of the recording board, the micro push rod is fixed at the central position of the connecting frame, and the marking pen is fixed at the output end of the micro push rod. There are two groups of micro push rods, which are respectively connected to the visual detection equipment and the ultrasonic detection module.

[0013] Furthermore, a positioning groove is provided on the inner wall of the recording plate, and the cross-section of the positioning groove is a trapezoidal structure. The connecting frame slides left and right along the inside of the positioning groove. An adjusting screw rod is provided on one side of the connecting frame, and the adjusting screw rod is connected to the connecting frame and contacts one side of the recording plate.

[0014] Furthermore, the inspection mechanism includes an adjusting push rod and a pushing plate, the adjusting push rod is arranged on one side of the workbench, the pushing plate is fixed to the output end of the adjusting push rod, and the pushing plate is located on the upper end surface of the conveyor belt.

[0015] The utility model has the following beneficial effects:

[0016] The utility model can transport aviation parts by setting a conveyor belt, thereby ensuring the inspection efficiency of aviation parts and components, and further improving the practicability of the equipment. Then, the visual inspection equipment and ultrasonic inspection module can respectively inspect the same group of aviation parts. Since the equipment has two inspection methods, the inspection error of aviation parts can be reduced, and the inspection efficiency of aviation parts can be ensured. If defects occur in aviation parts, the micro push rod can push the marker to contact the aviation parts, and then the defective aviation parts can be marked and recorded. Since the equipment can automatically detect and record, the inspection efficiency of aviation parts can be improved. Then, the position of the connecting frame is adjustable, and it can be adjusted according to the different sizes and diameters of the aviation parts to be inspected, thereby improving the practicability of the equipment. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] In order to more clearly illustrate the technical solutions of the embodiments of the utility model, the drawings required for describing the embodiments are briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0018] Figure 1This is a top view schematic diagram of the aviation parts defect detection and recording workbench of the utility model;

[0019] Figure 2 This is a left side schematic diagram of the aviation parts defect detection and recording workbench of the utility model;

[0020] Figure 3 For this utility model Figure 1 A partial enlarged schematic diagram in the middle;

[0021] Figure 4 It is a top view schematic diagram of the connecting frame of the utility model.

[0022] In the accompanying drawings, the components represented by the reference numerals are listed as follows:

[0023] 1. Base body; 2. Workbench; 3. Conveyor belt; 4. Inspection frame; 5. Visual inspection equipment; 6. Electric push rod; 7. Connecting plate; 8. Ultrasonic detection module; 9. Recording board; 10. Positioning slide; 11. Connecting frame; 12. Adjusting screw rod; 13. Micro push rod; 14. Marking pen; 15. Adjusting push rod; 16. Pushing plate. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0025] See also Figure 1-4 As shown, the utility model is an aviation parts defect detection and recording workbench, comprising a base body 1 and a workbench 2 arranged on the upper end of the base body 1, and also comprising:

[0026] The conveyor belt 3 is arranged inside the workbench 2, and two groups of detection racks 4 are equidistantly arranged on the upper end surface of the workbench 2; the base body 1 is arranged to support the workbench 2, which can prevent the workbench 2 from deviating, and the conveyor belt 3 is arranged inside the workbench 2 to convey the aviation parts, which can ensure the inspection efficiency of the aviation parts and further improve the practicality of the equipment; the visual inspection equipment 5 is arranged in the center of one group of detection racks 4, and the lower end of the other group of detection racks 4 is provided with an ultrasonic inspection module 8; the upper end surface of the other group of detection racks 4 is provided with an electric push rod 6, and the output end of the electric push rod 6 is fixed with a connecting plate 7, and the lower end surface of the connecting plate 7 is connected to the ultrasonic inspection module 8. The visual inspection device 5 provided on the upper end of a set of inspection racks 4 can take pictures of aviation parts, and can be compared with defect-free aviation parts by performing data conversion in the control panel, so as to facilitate subsequent inspections, and the electric push rod 6 provided can adjust the position of the connecting plate 7, and the ultrasonic inspection module 8 provided can contact with aviation parts, so as to push the position of the ultrasonic inspection module 8 to adjust, and the ultrasonic inspection module 8 can contact with the parts to be inspected, detect the defect position and size through ultrasonic waves, analyze and judge the waveform, and send the information to the control panel for the convenience of the staff to control;

[0027] The recording plate 9 is arranged on the left and right sides of the connecting plate 7. A recording mechanism is arranged on the inner side of the recording plate 9 for recording defective aviation parts. The recording mechanism includes a connecting frame 11, a micro push rod 13 and a marking pen 14. The connecting frame 11 is slidably connected to the left and right sides of the recording plate 9. The micro push rod 13 is fixed at the central position of the connecting frame 11. The marking pen 14 is fixed at the output end of the micro push rod 13. The micro push rod 13 is provided with two groups, which are respectively connected to the visual inspection device 5 and the ultrasonic inspection module 8. If there is a defect in the aviation part, the provided micro push rod 13 can push the marking pen 14 to contact the aviation part, so as to mark and record the defective aviation part. Since the device can automatically detect and record, the inspection efficiency of aviation parts can be improved. At the same time, the marking pen 14 is provided with two A group, which can be connected to the visual inspection device 5 and the ultrasonic inspection module 8 respectively, so as to facilitate the equipment to record; a positioning slot 10 is provided on the inner wall of the recording plate 9, and the cross section of the positioning slot 10 is a trapezoidal structure, and the connecting frame 11 slides left and right along the inside of the positioning slot 10, and an adjusting screw 12 is provided on one side of the connecting frame 11, and the adjusting screw 12 is connected to the connecting frame 11 and contacts with one side of the recording plate 9, and then, the positioning slot 10 provided can limit the position of the connecting frame 11, and can avoid the displacement of the connecting frame 11, and the adjusting screw 12 provided can be screwed on the inner side of the connecting frame 11, and then the position of the connecting frame 11 can be limited, and because the angle of the connecting frame 11 can be adjusted, it can be adjusted according to the different sizes and diameters of the aviation parts to be inspected, so that the practicability of the equipment is improved;

[0028] The inspection mechanism is arranged at one end of the workbench 2 away from the visual inspection equipment 5, and is used to discharge defective aviation parts; the inspection mechanism includes an adjusting push rod 15 and a pushing plate 16, the adjusting push rod 15 is arranged on one side of the workbench 2, the pushing plate 16 is fixed to the output end of the adjusting push rod 15, and the pushing plate 16 is located on the upper end surface of the conveyor belt 3, and the arranged adjusting push rod 15 can adjust the position of the pushing plate 16, so that the defective aviation parts can be withdrawn from the conveyor belt 3 and fall into the collection bin for subsequent processing.

[0029] The above are only preferred embodiments of the present invention and do not limit the present invention. Any modification to the technical solutions recorded in the aforementioned embodiments and any equivalent replacement of some of the technical features therein, any modification, equivalent replacement, and improvement made are all within the protection scope of the present invention.

Claims

1. An aviation component defect detection and recording workbench, comprising a base body (1) and a workbench (2) arranged on the upper end of the base body (1), characterized in that: Also includes: A conveyor belt (3) is arranged inside the workbench (2), and two groups of detection racks (4) are arranged at equal distances on the upper end surface of the workbench (2); A visual inspection device (5) is arranged at the center of one set of inspection frames (4), and an ultrasonic inspection module (8) is arranged at the lower end of another set of inspection frames (4); A recording plate (9) is arranged on the left and right sides of the connecting plate (7), and a recording mechanism is arranged on the inner side of the recording plate (9) for recording defective aviation parts; The inspection mechanism is arranged at one end of the workbench (2) away from the visual inspection device (5) and is used to discharge defective aviation parts.

2. The aviation parts defect detection and recording workbench according to claim 1, characterized in that: The upper end surface of the other group of detection frames (4) is provided with an electric push rod (6), and a connecting plate (7) is fixed to the output end of the electric push rod (6), and the lower end surface of the connecting plate (7) is connected to the ultrasonic detection module (8).

3. The aviation parts defect detection and recording workbench according to claim 1, characterized in that: The recording mechanism comprises a connecting frame (11), a micro push rod (13), and a marking pen (14); the connecting frame (11) is slidably connected to the left and right sides of the recording plate (9); the micro push rod (13) is fixed at the central position of the connecting frame (11); the marking pen (14) is fixed at the output end of the micro push rod (13); and two groups of micro push rods (13) are provided, which are respectively connected to the visual detection device (5) and the ultrasonic detection module (8).

4. The aviation parts defect detection and recording workbench according to claim 3, characterized in that: The inner wall of the recording plate (9) is provided with a positioning slot (10), and the cross section of the positioning slot (10) is a trapezoidal structure. The connecting frame (11) slides left and right along the inside of the positioning slot (10). An adjusting screw rod (12) is provided on one side of the connecting frame (11), and the adjusting screw rod (12) is connected to the connecting frame (11) and contacts one side of the recording plate (9).

5. The aviation parts defect detection and recording workbench according to claim 1, characterized in that: The inspection mechanism comprises an adjusting push rod (15) and a pushing plate (16), wherein the adjusting push rod (15) is arranged on one side of the workbench (2), the pushing plate (16) is fixed to the output end of the adjusting push rod (15), and the pushing plate (16) is located on the upper end surface of the conveyor belt (3).

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