A transfer detection device for aircraft cables
By designing an aircraft cable adapter detection device including a detection table, adapter, telescopic cylinder and drive motor, the problems of traditional manual detection are solved, and automated detection is realized, and efficiency and accuracy are improved.
Patent Information
- Application Number
- CN202420747417.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-04-11
- Publication Date
- 2025-04-04
- Estimated Expiration
- 2034-04-11
AI Technical Summary
The traditional aircraft cable transfer detection method is manually plugged in, resulting in low detection efficiency and high error rate, which cannot meet the needs of the modern aviation industry.
An aircraft cable adapter detection device is designed, including a detection table, an aircraft cable adapter, a telescopic cylinder and a driving motor. The drive motor and telescopic cylinder are controlled by the operating panel to achieve an automated transfer and detection process.
It improves detection efficiency, reduces error rate, and realizes convenient clamping and automatic plugging detection of aircraft cable adapters, meeting the needs of modern aviation industry.
Smart Images
Figure CN222719697U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aircraft cable detection, in particular to a switching detection device for aircraft cables. Background Art
[0002] Aircraft cable testing is a comprehensive and detailed test of aircraft cables to ensure that their performance, quality and safety meet the requirements. This testing process is crucial in the aviation industry and plays a key role in ensuring the normal operation and flight safety of aircraft. The role of aircraft cable testing is mainly reflected in the following aspects: ensuring cable performance, ensuring flight safety, improving aircraft reliability and meeting aviation standards. In summary, aircraft cable testing plays an indispensable role in the aviation industry and is an important means to ensure aircraft flight safety and stable performance.
[0003] Among them, with the continuous development of aviation technology, the safety and reliability of aircraft cable transfers have received increasing attention. The traditional cable transfer detection method is to manually plug the cable adapter into the upper end of the cable tester for cable transfer detection. However, the method of manually plugging the cable adapter into the upper end of the cable tester for cable transfer detection has the problems of low detection efficiency and high error rate, which can no longer meet the needs of the modern aviation industry. Utility Model Content
[0004] The purpose of the utility model is to provide an aircraft cable transfer detection device to solve the problem that the traditional cable transfer detection method proposed in the above background technology is to manually plug the cable adapter into the upper end of the cable detector for cable transfer detection, but the method of manually plugging the cable adapter into the upper end of the cable detector for cable transfer detection has the problems of low detection efficiency and high error rate.
[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solution: comprising an aircraft cable adapter and a test bench, a protective top cover is fixedly installed on the top of the test bench, and an operation panel is fixedly installed on the front side of the test bench;
[0006] A support frame is fixedly installed on the rear side of the upper end of the detection platform, a telescopic cylinder is fixedly installed through the front middle part of the upper end of the support frame, and a moving platform is fixedly installed on the telescopic part of the lower bottom end of the telescopic cylinder, a limited sliding bar is fixedly installed on the rear side of the upper end of the moving platform, a detection groove is opened in the middle part of the moving platform, and a limited groove is opened through the bottom of the detection groove, and a mounting platform is fixedly installed on the front side of the upper end of the detection platform, and a detection interface for detecting aircraft cable adapters is fixedly installed on the middle part of the upper end surface of the mounting platform, and limited support columns are fixedly installed at the four corners of the lower end surface of the moving platform, a clamping screw is rotatably connected with a rotating shaft through the middle part of the limiting groove, and the outer curved surfaces of the front and rear ends of the clamping screw are threadedly connected with a clamping plate for clamping and fixing the aircraft cable adapter, and a driving motor is fixedly installed in the middle part of the front end of the moving platform.
[0007] Preferably, a display for displaying aircraft cable detection data is fixedly installed on the upper end of the protective top cover, a protective front cover is hinged on the front side of the upper end of the protective top cover, and a power switch, an indicator light, a buzzer and an emergency stop switch are fixedly installed in sequence on the front end surface of the protective front cover.
[0008] Preferably, there are two limit sliding bars, which are symmetrically distributed on the rear side of the upper end of the moving platform, and the upper ends of the limit sliding bars are penetrated and movably connected to the front two sides of the upper end of the supporting frame.
[0009] Preferably, there are several limit grooves, which are symmetrically distributed in sequence at the bottom of the detection groove. The lower end of the aircraft cable adapter is movably connected to the inner wall of the limit groove, so that the aircraft cable adapter is limited by the limit groove.
[0010] Preferably, the detection interface is located directly below the limiting groove, and a buffer pad is bonded to the lower top of the limiting support column.
[0011] Preferably, the threads of the outer curved surfaces at the front and rear ends of the clamping screw are in opposite directions, the outer side of the clamping plate is movably connected to the inner wall of the detection groove, and an anti-slip pad is bonded to the inner side of the clamping plate.
[0012] Preferably, the transmission shaft portion at the rear side of the driving motor and the clamping screw are fixedly connected to each other.
[0013] Compared with the prior art, the beneficial effects of the utility model are:
[0014] 1. The utility model controls the start of the driving motor through the operation panel. When the driving motor is turned on, it drives the clamping screw to rotate. When the clamping screw rotates, it drives the clamping plate to move linearly inward along the inner wall of the detection groove due to the force generated by the threaded connection with the outer curved surface of the front and rear ends of the clamping screw. When the clamping plate moves linearly inward synchronously, the aircraft cable adapter that is movably connected to the inner wall of the limit groove is uniformly clamped and fixed, thereby facilitating the uniform clamping and fixing of the aircraft cable adapter;
[0015] 2. The utility model also controls the opening of the telescopic cylinder through the operation panel when the aircraft cable adapters are uniformly clamped and fixed. When the telescopic cylinder is turned on, it will drive the moving platform to move linearly downward. When the moving platform moves linearly downward, it will drive the clamped and fixed aircraft cable adapters to move linearly downward synchronously. When the aircraft cable adapters move linearly downward synchronously, they will be synchronously plugged into the detection interface, thereby facilitating the unified plug-in detection of the aircraft cable adapters and avoiding the problems of low detection efficiency and high error rate. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] Figure 1 This is a schematic diagram of the overall structure of a transfer detection device for aircraft cables according to the utility model;
[0017] Figure 2 This is a schematic diagram of the local structure of a transfer detection device for aircraft cables of the utility model. Figure 1 ;
[0018] Figure 3 This is a schematic diagram of the local structure of a transfer detection device for aircraft cables of the utility model. Figure 2 .
[0019] In the figure: 1. test table; 2. display; 3. protective front cover; 4. protective top cover; 5. operation panel; 6. support frame; 7. telescopic cylinder; 8. moving table; 9. limit slide bar; 10. test slot; 11. limit slot; 12. aircraft cable adapter; 13. clamping plate; 14. test interface; 15. limit support column; 16. clamping screw; 17. drive motor; 18. mounting table. DETAILED DESCRIPTION
[0020] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0021] See also Figure 1-3The utility model provides a technical solution for an aircraft cable transfer detection device: comprising a detection platform 1 and an aircraft cable adapter 12, a protective top cover 4 is fixedly installed on the top of the detection platform 1, a display 2 for displaying aircraft cable detection data is fixedly installed on the upper end of the protective top cover 4, a protective front cover 3 is hinged on the front side of the upper end of the protective top cover 4, and a power switch, an indicator light, a buzzer and an emergency stop switch are fixedly installed on the front face of the protective front cover 3 in sequence, and an operation panel 5 is fixedly installed on the front side of the detection platform 1;
[0022] A support frame 6 is fixedly installed on the rear side of the upper end of the testing platform 1, and a telescopic cylinder 7 is fixedly installed through the front middle part of the upper end of the supporting frame 6. A moving platform 8 is fixedly installed on the telescopic part of the lower bottom end of the telescopic cylinder 7. A limit slide bar 9 is fixedly installed on the rear side of the upper end of the moving platform 8, and there are two limit slide bars 9, which are symmetrically distributed on the rear side of the upper end of the moving platform 8. The upper ends of the limit slide bars 9 penetrate and fit movably connected to the front two sides of the upper end of the supporting frame 6. A testing groove 10 is provided in the middle of the moving platform 8, and a limiting groove 11 is provided through the bottom of the testing groove 10, and there are several limiting grooves 11, which are symmetrically distributed in sequence with the bottom of the testing groove 10. The lower end of the aircraft cable adapter 12 is fit and movably connected to the inner wall of the limiting groove 11, so that the aircraft cable adapter 12 is limited by the limiting groove 11. A mounting platform is fixedly installed on the front side of the upper end of the testing platform 1 18. A detection interface 14 for detecting the aircraft cable adapter 12 is fixedly installed in the middle of the upper end surface of the mounting platform 18, and the detection interface 14 is located directly below the limit groove 11. Limit support columns 15 are fixedly installed at the four corners of the lower end surface of the moving platform 8, and a buffer pad is bonded to the lower top of the limit support column 15. A clamping screw 16 is rotatably connected through a rotating shaft in the middle of the limit groove 11, and the front and rear end outer curved surface threads of the clamping screw 16 are in opposite directions. The front and rear end outer curved surface threads of the clamping screw 16 are connected with a clamping plate 13 for clamping and fixing the aircraft cable adapter 12, and the outer side of the clamping plate 13 is movably connected to the inner wall of the detection groove 10, and an anti-slip pad is bonded to the inner side of the clamping plate 13. A driving motor 17 is fixedly installed in the middle of the front end of the moving platform 8, and the rear transmission shaft part of the driving motor 17 is fixedly connected to the clamping screw 16.
[0023] Working principle: When in use, the utility model controls the start of the driving motor 17 through the operation panel 5. When the driving motor 17 is turned on, it drives the clamping screw 16 to rotate. When the clamping screw 16 rotates, it drives the clamping plate 13 to move linearly inward along the inner wall of the detection groove 10 due to the force generated by the threaded connection with the outer curved surface of the front and rear ends of the clamping screw 16. When the clamping plate 13 moves linearly inward synchronously, the aircraft cable adapter 12 that is movably connected to the inner wall of the limit groove 11 is uniformly clamped and fixed, thereby facilitating the uniform clamping and fixing of the aircraft cable adapter 12;
[0024] When the aircraft cable adapter 12 is uniformly clamped and fixed, the telescopic cylinder 7 is controlled to be turned on through the operation panel 5. When the telescopic cylinder 7 is turned on, it will drive the moving platform 8 to move linearly downward. When the moving platform 8 moves linearly downward, it will drive the clamped and fixed aircraft cable adapter 12 to move linearly downward synchronously. When the aircraft cable adapter 12 moves linearly downward synchronously, it will be synchronously plugged into the detection interface 14, thereby facilitating the unified plug-in detection of the aircraft cable adapter 12 and avoiding the problems of low detection efficiency and high error rate.
[0025] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.
[0026] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A switching detection device for aircraft cables, comprising an aircraft cable adapter (12), characterized in that: It comprises a testing platform (1), a protective top cover (4) is fixedly installed on the top of the testing platform (1), and an operating panel (5) is fixedly installed on the front side of the testing platform (1); A support frame (6) is fixedly installed on the rear side of the upper end of the detection platform (1); a telescopic cylinder (7) is fixedly installed through the front middle part of the upper end of the support frame (6); a moving platform (8) is fixedly installed on the telescopic part of the lower end of the telescopic cylinder (7); a limit sliding rod (9) is fixedly installed on the rear side of the upper end of the moving platform (8); a detection groove (10) is provided in the middle of the moving platform (8); a limit groove (11) is provided through the bottom of the detection groove (10); and a mounting platform (18) is fixedly installed on the front side of the upper end of the detection platform (1). A detection interface (14) for detecting an aircraft cable adapter (12) is fixedly installed in the middle of the upper end surface of the mounting platform (18), and limited support columns (15) are fixedly installed at the four corners of the lower end surface of the moving platform (8). A clamping screw (16) is rotatably connected to the middle of the limit groove (11) through a rotating shaft, and the front and rear outer curved surfaces of the clamping screw (16) are threadedly connected to a clamping plate (13) for clamping and fixing the aircraft cable adapter (12), and a driving motor (17) is fixedly installed in the middle of the front end of the moving platform (8).
2. The aircraft cable transfer detection device according to claim 1, characterized in that: A display (2) for displaying aircraft cable detection data is fixedly installed on the upper end of the protective top cover (4), a protective front cover (3) is hingedly connected to the front side of the upper end of the protective top cover (4), and a power switch, an indicator light, a buzzer and an emergency stop switch are fixedly installed in sequence on the front face of the protective front cover (3).
3. The aircraft cable transfer detection device according to claim 2, characterized in that: There are two limit slide bars (9), which are symmetrically distributed on the rear side of the upper end of the moving platform (8). The upper ends of the limit slide bars (9) penetrate and fit movably connected to the front two sides of the upper end of the support frame (6).
4. The aircraft cable transfer detection device according to claim 3, characterized in that: The limiting grooves (11) are in a plurality and are symmetrically distributed in sequence on the bottom of the detection groove (10); the lower end of the aircraft cable adapter (12) is movably connected to the inner wall of the limiting groove (11), so that the aircraft cable adapter (12) is limited by the limiting groove (11).
5. The aircraft cable transfer detection device according to claim 4, characterized in that: The detection interface (14) is located directly below the limiting groove (11), and a buffer pad is bonded to the lower top of the limiting support column (15).
6. The aircraft cable transfer detection device according to claim 5, characterized in that: The front and rear ends of the clamping screw (16) have outer curved threads facing opposite directions, the outer side of the clamping plate (13) is movably connected to the inner wall of the detection groove (10), and an anti-slip pad is bonded to the inner side of the clamping plate (13).
7. The aircraft cable transfer detection device according to claim 6, characterized in that: The rear transmission shaft portion of the driving motor (17) and the clamping screw (16) are fixedly connected to each other.