Workbench for detecting and recording defects of aeronautical parts
The workbench addresses the issue of unreliable defect image fixation by using a fixing mechanism with rotating and sliding plates, enabling secure display and retrieval of defect images and records, thus improving defect assessment and documentation efficiency.
Patent Information
- Application Number
- CN202420899670.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-04-28
- Publication Date
- 2024-12-31
- Estimated Expiration
- 2034-04-28
AI Technical Summary
Existing aviation component defect detection and recording workbenches lack a reliable mechanism for fixing and displaying photographs of defective parts, making it difficult for personnel to quickly assess and document defects.
The workbench incorporates a fixing mechanism with rotating and sliding plates, through holes, and limiting grooves to securely hold and display actual pictures and records of defective parts, allowing easy access and observation.
Facilitates secure placement and retrieval of defect images and records, enhancing the efficiency of defect assessment and documentation by providing a stable support for inspection and recording processes.
Smart Images
Figure CN222264802U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aviation component detection, in particular to an aviation component defect detection and recording workbench. Background Art
[0002] Strict maintenance and repair of aircraft and their aviation parts to maintain and improve the feasibility of the aircraft and ensure its safety is a prerequisite and necessary condition for the use of aircraft and an important part of the aviation industry. During the inspection process, staff need to record the overall condition of the aircraft, the use of instruments, and the defects of aviation parts.
[0003] The utility model with the authorization announcement number "CN 217572791 U" discloses "an aviation component defect detection and recording workbench". Through a support plate, half-finger gloves and a splint, these designs can help workers have a sufficiently stable surface for writing and recording during the process of aviation component defect inspection. It is convenient to carry and improves the convenience of workers' recording. It solves the problem that most of the time, workers have no reliable support position for recording defects. If they support with their hands or an irregular plane, the paper will be torn and the recorded content will be damaged.
[0004] However, during the defect detection process of aviation parts, sometimes the actual situation of the defective parts is photographed and printed out. After printing, it needs to be fixed so that relevant personnel can quickly check and understand the defect situation. However, the above-mentioned device does not have a good fixing mechanism for the actual picture of the defective parts. Utility Model Content
[0005] The utility model aims to solve the shortcomings in the prior art and proposes an aviation parts defect detection and recording workbench.
[0006] In order to achieve the above purpose, the utility model adopts the following technical solutions:
[0007] An aviation component defect detection and recording workbench comprises a workbench and a fixing mechanism, wherein three rotating cavities are equidistantly provided on one side of the workbench, a first fixing plate, a second fixing plate and a third fixing plate are rotatably installed in the three rotating cavities of the workbench in sequence through a rotating shaft, and a fixed inclined plate is installed on one side of the first fixing plate, the second fixing plate and the third fixing plate, and a sliding inclined plate is slidably installed inside the fixed inclined plate.
[0008] In addition, a preferred structure is that a through hole is opened in the middle of one side of the sliding inclined plate, and through holes are opened on both sides of the front end surface of the sliding inclined plate and located at the corresponding through holes.
[0009] In addition, a preferred structure is that a limiting plate is installed on the front end surface of the fixed inclined plate, a through hole is opened in the middle of one side of the limiting plate, and limiting through holes are opened on both sides of the front end surface of the limiting plate and located at the corresponding through holes.
[0010] In addition, the preferred structure is that a support block is symmetrically installed on the upper part of the rear end surface of the fixed inclined plate, a fixed shaft is installed in the middle of the support block, and a limiting support rod is rotatably installed on the rear end surface of the fixed inclined plate through the fixed shaft, and the limiting support rod and the fixed inclined plate are connected by fixing bolts.
[0011] In addition, a preferred structure is that a sliding groove is provided inside the fixed inclined plate at the sliding inclined plate, and the sliding inclined plate passes through the sliding groove and is connected to the limited fixed plate.
[0012] In addition, a preferred structure is that the fixing mechanism includes a limiting snap-fit block and a fixing bolt, and a groove is formed on one side of the limiting snap-fit block at the corresponding first fixing plate, second fixing plate and third fixing plate.
[0013] The beneficial effects of the utility model are:
[0014] In the utility model, actual pictures of defective aviation parts and papers on which staff record defective aviation parts can be placed or taken out through a sliding inclined plate and a fixed inclined plate. At the same time, papers on which staff record defective aviation parts can be placed through the limiting grooves, and the limiting through holes can facilitate staff to record on the papers. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 This is a structural schematic diagram of an aviation parts defect detection and recording workbench proposed by the utility model;
[0016] Figure 2 This is a schematic diagram of the structure of the first fixing plate, the second fixing plate and the third fixing plate proposed in the utility model when they are unfolded;
[0017] Figure 3 This is a schematic diagram of the structure of the fixed mechanism, the first fixed plate, the second fixed plate and the third fixed plate proposed in the utility model after being separated.
[0018] In the figure: 1. workbench; 11. rotating cavity; 12. placing groove; 2-1. first fixed plate; 2-2. second fixed plate; 2-3. third fixed plate; 3. fixed inclined plate; 31. limit plate; 32. sliding inclined plate; 33. limit fixed plate; 34. limit support rod; 4. fixing mechanism; 41. limit locking block; 42. fixing bolt. DETAILED DESCRIPTION
[0019] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.
[0020] Reference Figure 1-3 A defect detection and recording workbench for aviation parts includes a workbench 1 and a fixing mechanism 4. Three rotating cavities 11 are equidistantly provided on one side of the workbench 1. A first fixing plate 2-1, a second fixing plate 2-2, and a third fixing plate 2-3 are rotatably installed in the three rotating cavities 11 of the workbench 1 in sequence through a rotating shaft, and a fixed inclined plate 3 is installed on one side of the first fixing plate 2-1, the second fixing plate 2-2, and the third fixing plate 2-3. A sliding inclined plate 32 is slidably installed inside the fixed inclined plate 3. It is worth mentioning that the length of the second fixing plate 2-2 is greater than that of the first fixing plate 2-1, and the length of the third fixing plate 2-3 is greater than that of the second fixing plate 2-2.
[0021] A through hole is provided in the middle of one side of the sliding inclined plate 32, and through holes are provided on both sides of the front end surface of the sliding inclined plate 32 and located at the corresponding through holes, wherein the through holes of the sliding inclined plate 32 are convenient for placing actual pictures of defective parts of aviation parts, and papers on which the staff record the defective parts of aviation parts can also be placed, and at the same time, the through holes of the sliding inclined plate 32 are convenient for taking out actual pictures of defective parts of aviation parts and papers on which the staff record the defective parts of aviation parts.
[0022] At the same time, a limiting plate 31 is installed on the front end face of the fixed inclined plate 3, and a through hole is opened in the middle of one side of the limiting plate 31, and limiting through holes are opened on both sides of the front end face of the limiting plate 31 and located at the corresponding through holes, wherein the through holes of the limiting plate 31 are convenient for placing actual pictures of defective parts of its aviation parts, and papers with records of defective parts of aviation parts by its staff can also be placed. At the same time, the limiting through holes of the limiting plate 31 are convenient for taking out actual pictures of defective parts of its aviation parts and papers with records of defective parts of aviation parts by the staff.
[0023] In addition, a support block is symmetrically installed on the upper part of the rear end surface of the fixed inclined plate 3, a fixed shaft is installed in the middle of the support block, and a limiting support rod 34 is rotatably installed on the rear end surface of the fixed inclined plate 3 through the fixed shaft, and the limiting support rod 34 and the fixed inclined plate 3 are connected by fixing bolts.
[0024] Furthermore, a sliding groove is provided inside the fixed inclined plate 3 at the sliding inclined plate 32, and the sliding inclined plate 32 passes through the sliding groove and is connected to the limited fixed plate 33, and when the sliding inclined plate 32 slides out of the sliding groove of the fixed inclined plate 3, it is rotated under the action of the fixed shaft through the limited support rod 34, and the limited fixed plate 33 of the sliding inclined plate 32 is connected to the limited support rod 34 by a fixing bolt, so that the sliding inclined plate 32 is supported by the limited support rod 34.
[0025] Furthermore, the fixing mechanism 4 includes a limit clamping block 41 and a fixing bolt 42. A groove is provided on one side of the limit clamping block 41 at the corresponding first fixing plate 2-1, the second fixing plate 2-2 and the third fixing plate 2-3, and an installation through hole is provided on one side of the first fixing plate 2-1, the second fixing plate 2-2 and the third fixing plate 2-3 at the corresponding fixing bolt 42. One end of the fixing bolt 42 is rotatably installed with a fixing nut on the limit clamping block 41, the first fixing plate 2-1, the second fixing plate 2-2 and the third fixing plate 2-3 respectively.
[0026] In addition, a limiting groove is opened in the middle of the front end surface of the workbench 1, and a limiting through hole is opened in the middle of the top of the workbench 1 at the limiting groove, wherein the limiting groove is used to place paper for the staff to record defective parts of aviation parts, and the limiting through hole is used to facilitate the staff to record on the paper.
[0027] In this embodiment, the actual pictures of defective aviation parts and the papers on which the staff recorded the defective aviation parts can be placed or taken out through the sliding inclined plate 32 and the fixed inclined plate 3. At the same time, the papers on which the staff recorded the defective aviation parts can be placed through the limiting grooves, and the limiting through holes can facilitate the staff to record on the paper.
[0028] And by rotating the first fixed plate 2-1, the second fixed plate 2-2, and the third fixed plate 2-3 under the action of the corresponding rotating shafts, the sliding inclined plate 32 and the fixed inclined plate 3 are unfolded, which makes it convenient for the staff to observe the actual pictures of the defective parts of their aviation parts and the papers on which the staff record the defective parts of the aviation parts.
[0029] In the utility model, the actual pictures of defective aviation parts and the papers on which the staff recorded the defective aviation parts can be placed or taken out through the sliding inclined plate 32 and the fixed inclined plate 3. At the same time, the papers on which the staff recorded the defective aviation parts can be placed through the limiting grooves, and the limiting through holes can facilitate the staff to record on the papers.
[0030] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes within the technical scope disclosed by the present invention according to the technical scheme and the utility model concept of the present invention, which should be covered by the protection scope of the present invention.
Claims
1. An aviation parts defect detection and recording workbench, comprising a workbench (1) and a fixing mechanism (4), characterized in that: One side of the workbench (1) is provided with three rotating cavities (11) at equal distances, and a first fixed plate (2-1), a second fixed plate (2-2), and a third fixed plate (2-3) are rotatably mounted in the three rotating cavities (11) of the workbench (1) in sequence through rotating shafts, and a fixed inclined plate (3) is mounted on one side of the first fixed plate (2-1), the second fixed plate (2-2), and the third fixed plate (2-3), and a sliding inclined plate (32) is slidably mounted inside the fixed inclined plate (3).
2. The aviation parts defect detection and recording workbench according to claim 1, characterized in that: A through hole is provided in the middle of one side of the sliding inclined plate (32), and through holes are provided on both sides of the front end surface of the sliding inclined plate (32) and located at the positions corresponding to the through hole.
3. The aviation parts defect detection and recording workbench according to claim 1, characterized in that: A limiting plate (31) is installed on the front end surface of the fixed inclined plate (3), a through hole is provided in the middle of one side of the limiting plate (31), and limiting through holes are provided on both sides of the front end surface of the limiting plate (31) and at the positions corresponding to the through holes.
4. The aviation parts defect detection and recording workbench according to claim 3, characterized in that: A support block is symmetrically mounted on the upper portion of the rear end surface of the fixed inclined plate (3), a fixed shaft is mounted in the middle portion of the support block, and a limit support rod (34) is rotatably mounted on the rear end surface of the fixed inclined plate (3) via the fixed shaft, and the limit support rod (34) and the fixed inclined plate (3) are connected via fixing bolts.
5. The aviation parts defect detection and recording workbench according to claim 4, characterized in that: A sliding groove is provided inside the fixed inclined plate (3) at the position of the sliding inclined plate (32), and the sliding inclined plate (32) passes through the sliding groove and is connected to the limited fixed plate (33).
6. The aviation parts defect detection and recording workbench according to claim 1, characterized in that: The fixing mechanism (4) comprises a limiting snap-fit block (41) and a fixing bolt (42); one side of the limiting snap-fit block (41) is provided with a groove at the corresponding first fixing plate (2-1), second fixing plate (2-2) and third fixing plate (2-3).