CN219016111U

CN219016111U - Aviation spare part defect detection device

Info

Publication number: CN219016111U
Application number: CN202222760878.8U
Authority: CN
Inventors: 王勋; 支旭辉; 张转红; 郭同庆; 孙东玉
Original assignee: Guanglian Airlines Xi'an Co ltd
Current assignee: Guanglian Airlines Xi'an Co ltd
Priority date: 2022-10-20
Filing date: 2022-10-20
Publication date: 2023-05-12
Anticipated expiration: 2032-10-20

Abstract

The utility model belongs to the field of aviation detection devices, in particular to an aviation part defect detection device, which comprises a detection device main body and a second transverse frame, wherein a sliding groove is reserved in the middle of the detection device main body, a sliding block is arranged in the sliding groove, a detection box is arranged at the top of the sliding block, a detection plate is arranged in the detection box, a gravity sensor is arranged at the bottom of the detection plate, a first transverse frame is arranged at the outer side of the detection box, a sleeve block is arranged at the end part of the first transverse frame, and an illumination lamp tube is connected in the sleeve block; the utility model can detect the weight, so that the aeronautical parts with unqualified weight can be primarily screened out, and the aeronautical parts can be precisely detected when the production work is carried out under the condition of dim light, thereby being beneficial to timely detecting the defects of the aeronautical parts, and being capable of carrying out omnibearing detection on the aeronautical parts, so that the detection precision is better.

Description

Aviation spare part defect detection device

Technical Field

The utility model relates to the field of aviation detection devices, in particular to an aviation part defect detection device.

Background

In China patent CN202022125900.2, the utility model relates to the technical field of detection equipment, in particular to an aviation part defect detection device, which comprises a workbench and a fixing member, wherein the fixing member is fixedly connected to the front end of the top of the workbench.

The existing aviation detection device is inconvenient to carry out preliminary weighing treatment on aviation parts, so that a follow-up defect detection program is complex, and when the aviation detection device is in a dim environment, an illuminating lamp is inconvenient to fix, an auxiliary support frame is required to illuminate, and the detection efficiency of the aviation parts is affected.

Accordingly, an aviation component defect detection device is proposed to solve the above problems.

Disclosure of Invention

In order to make up the defect of the prior art, the problem that the detection efficiency of the aviation parts is affected because the auxiliary support frame is required to carry out illumination when the illumination lamp is fixed inconveniently under the dim environment because the procedure of carrying out defect detection at the follow-up is complicated due to the fact that the preliminary weighing treatment of the aviation parts is inconvenient is solved.

The technical scheme adopted for solving the technical problems is as follows: the utility model discloses an aviation part defect detection device which comprises a detection device main body and a second transverse frame, wherein a sliding groove is reserved in the middle position of the detection device main body, a sliding block is arranged in the sliding groove, a detection box is arranged at the top of the sliding block, a detection plate is arranged in the detection box, a gravity sensor is arranged at the bottom of the detection plate, a first transverse frame is arranged at the outer side of the detection box, a sleeve block is arranged at the end part of the first transverse frame, an illumination lamp tube is connected in the sleeve block, the second transverse frame is arranged on the right side of the outer wall of the first transverse frame, a transverse rod is fixed in the second transverse frame, a driving sleeve plate is arranged in the middle position of the transverse rod, and a detection module is arranged at the bottom of the driving sleeve plate.

Preferably, the processor is installed on the right side of the outer wall of the detection device main body, the display screen is installed above the processor, and the electric wire is installed on the outer wall of the processor.

Preferably, the central axis of the detection plate coincides with the central axis of the detection box, the detection box forms a sliding structure with the sliding groove through the sliding block, and the sliding block is arranged in a T shape.

Preferably, the sleeve block is in threaded connection with the lighting tube, and the sleeve block is in welded connection with the first transverse frame.

Preferably, the cross rod is in sliding connection with the driving sleeve plate, and the cross rod is in welded connection with the second cross frame.

Preferably, the processor is electrically connected with the electric wire, and the central axis of the processor coincides with the central axis of the display screen.

The utility model has the advantages that:

1. when the aviation parts are placed above the detection plate, the detection box at the bottom of the detection plate monitors the weight of the aviation parts above the detection plate, then the detection box moves rightwards through the action force of sliding of the sliding block in the sliding groove to detect defects in the next step, when the aviation parts are detected, the weight of the aviation parts can be detected firstly through the arrangement, so that the aviation parts with unqualified weight can be primarily screened out, the main body of the detection device can be illuminated by the illumination lamp tube, and when production work is carried out under the condition of dim light, fine defect detection can be carried out on the aviation parts due to the fact that the limitation of headlight is large, so that the defects of the aviation parts can be detected timely, and the detection efficiency is effectively improved;

2. when carrying out the defect detection to aviation spare part, can be according to the sliding tray about to carry out the lateral shifting detection of left and right directions to aviation spare part, reach the purpose of all-round detection, drive detection module through the gliding effort of drive sleeve board outside the horizontal pole and slide back and forth, thereby detect aviation spare part front and back, can carry out all-round detection to aviation spare part like this, make the precision that detects better.

Drawings

In order to more clearly illustrate the embodiments of the utility model or the technical solutions of the prior art, the drawings which are used in the description of the embodiments or the prior art will be briefly described, it being obvious that the drawings in the description below are only some embodiments of the utility model, and that other drawings can be obtained from these drawings without inventive faculty for a person skilled in the art.

FIG. 1 is a schematic perspective view of the whole front view of the present utility model;

FIG. 2 is a schematic perspective view of the whole side view of the present utility model;

FIG. 3 is a schematic perspective view of the cartridge of the present utility model;

FIG. 4 is a schematic diagram of the explosion structure of the cartridge of the present utility model.

In the figure: 1. a detection device body; 2. a sliding groove; 3. a sliding block; 4. a detection box; 5. a detection plate; 6. a gravity sensor; 7. a first cross frame; 8. sleeving blocks; 9. a lighting tube; 10. a second cross frame; 11. a cross bar; 12. driving the sleeve plate; 13. a detection module; 14. a processor; 15. a display screen; 16. an electric wire.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Example 1

Referring to fig. 1 to 4, an aviation component defect detection device includes a detection device main body 1 and a second transverse frame 10, a sliding groove 2 is reserved in the middle position of the detection device main body 1, a sliding block 3 is installed in the sliding groove 2, a detection box 4 is installed at the top of the sliding block 3, a detection plate 5 is installed in the detection box 4, a gravity sensor 6 is installed at the bottom of the detection plate 5, a first transverse frame 7 is installed at the outer side of the detection box 4, a sleeve block 8 is installed at the end of the first transverse frame 7, an illumination lamp 9 is connected to the inner side of the sleeve block 8, a second transverse frame 10 is arranged on the right side of the outer wall of the first transverse frame 7, a transverse rod 11 is fixed in the second transverse frame 10, a driving sleeve plate 12 is installed in the middle position of the transverse rod 11, and a detection module 13 is installed at the bottom of the driving sleeve plate 12.

The axis of pick-up plate 5 coincides with the axis of detection box 4, and detection box 4 constitutes sliding structure through slider 3 and sliding tray 2, and slider 3 adopts "T" font setting, after aviation spare part is placed in pick-up plate 5 top, detection plate 5 bottom detects box 4 and monitors the weight of the aviation spare part of pick-up plate 5 top, then detection box 4 moves to the right side through the gliding effort of slider 3 in sliding tray 2 inside, carry out the defect detection of next step, when carrying out the defect detection through such setting aviation spare part, can at first detect the weight, thereby preliminary screen out the aviation spare part that weight is not up to standard, when carrying out the defect detection subsequently, can carry out the side-to-side movement according to sliding tray 2, thereby carry out lateral movement detection of left and right directions to the aviation spare part, reach the purpose of all-round detection.

The sleeve block 8 is in threaded connection with the illumination lamp tube 9, and the sleeve block 8 is in welded connection with the first transverse frame 7, the illumination lamp tube 9 can illuminate the detection device main body 1, and when production work is carried out under the condition of dim light, fine defect detection can be carried out on aviation parts due to the fact that the limitation of big lamplight is large, so that the defect of the aviation parts can be detected in time, and the detection efficiency is effectively improved.

The horizontal pole 11 is sliding connection with drive sleeve plate 12, and is welded connection between horizontal pole 11 and the second crossbearer 10, when carrying out the defect detection to aviation spare part, through the gliding effort of drive sleeve plate 12 in horizontal pole 11 outside, drive detection module 13 and slide back and forth to detect around carrying out the aviation spare part, can carry out the omnidirectional detection to aviation spare part like this, make the precision that detects better.

Example two

Referring to fig. 1 to 2, a defect detecting device for aviation components is disclosed, wherein a processor 14 is mounted on the right side of the outer wall of a detecting device main body 1, a display 15 is mounted above the processor 14, and an electric wire 16 is mounted on the outer wall of the processor 14.

The processor 14 is electrically connected with the electric wire 16, the central axis of the processor 14 coincides with the central axis of the display screen 15, the detection device main body 1 processes through the processor 14, and the display screen 15 displays detection data of the aviation parts.

Working principle: firstly, after the aviation components are placed above a detection plate 5, a detection box 4 at the bottom of the detection plate 5 monitors the weight of the aviation components above the detection plate 5, then the detection box 4 moves rightwards through the sliding force of a sliding block 3 in a sliding groove 2 to perform defect detection in the next step, when the aviation components are subjected to defect detection through the arrangement, firstly the weight of the aviation components can be detected, so that the aviation components with unqualified weight can be primarily screened out, and then the aviation components can be moved leftwards and rightwards according to the sliding groove 2 during defect detection, so that the aviation components can be transversely moved in the left and right directions to achieve the purpose of omnibearing detection, and an illumination lamp tube 9 can illuminate a detection device main body 1.

Secondly, when carrying out the defect detection to aviation spare part, through the gliding effort of drive sleeve plate 12 in horizontal pole 11 outside, drive detection module 13 and carry out the back-and-forth slip to detect aviation spare part, can carry out the omnidirectional detection to aviation spare part like this, make the precision that detects better, detection device main part 1 handles through processor 14, shows the detection data of aviation spare part through display screen 15.

The foregoing has shown and described the basic principles, principal features and advantages of the utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims.

Claims

1. An aviation spare part defect detection device which is characterized in that: including detection device main part (1) and second crossbearer (10), slider (2) are reserved to the intermediate position of detection device main part (1), and internally mounted of slider (2) has slider (3), detection box (4) are installed at the top of slider (3), and the internally mounted of detection box (4) has pick-up plate (5) to gravity sensor (6) are installed to the bottom of pick-up plate (5), first crossbearer (7) are installed in the outside of detection box (4), and cover piece (8) are installed to the tip of first crossbearer (7) to the internal connection of cover piece (8) has illumination fluorescent tube (9), second crossbearer (10) set up on the outer wall right side of first crossbearer (7), and the internally mounted of second crossbearer (10) has horizontal pole (11), drive sleeve plate (12) are installed to the intermediate position of horizontal pole (11), and detection module (13) are installed to the bottom of drive sleeve plate (12).

2. The aerospace component defect detection apparatus of claim 1, wherein: the right side of the outer wall of the detection device main body (1) is provided with a processor (14), a display screen (15) is arranged above the processor (14), and the outer wall of the processor (14) is provided with an electric wire (16).

3. The aerospace component defect detection apparatus of claim 1, wherein: the central axis of the detection plate (5) coincides with the central axis of the detection box (4), the detection box (4) and the sliding groove (2) form a sliding structure through the sliding block (3), and the sliding block (3) is arranged in a T shape.

4. The aerospace component defect detection apparatus of claim 1, wherein: the sleeve block (8) is in threaded connection with the lighting tube (9), and the sleeve block (8) is in welded connection with the first transverse frame (7).

5. The aerospace component defect detection apparatus of claim 1, wherein: the cross rod (11) is in sliding connection with the driving sleeve plate (12), and the cross rod (11) is in welding connection with the second cross frame (10).

6. The aerospace component defect detection apparatus of claim 2, wherein: the processor (14) is electrically connected with the electric wire (16), and the central axis of the processor (14) coincides with the central axis of the display screen (15).