Aircraft tire inflation leakage detection equipment
By introducing a flip and cleaning mechanism into the aviation tire inflation leakage detection equipment, horizontal detection and cleaning of the detection liquid is achieved, which solves the problem of detection liquid interfering with the detection result and improves the accuracy of the detection.
Patent Information
- Application Number
- CN202422457329.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-11
- Publication Date
- 2025-08-05
- Estimated Expiration
- 2034-10-11
AI Technical Summary
During the inspection process of existing aviation tire inflation leakage detection equipment, the liquid flowing from above interferes with the detection results below the material, resulting in inaccurate detection.
The flip mechanism and cleaning mechanism are adopted to realize horizontal inspection method, and the materials are cleaned after the inspection is completed to reduce the impact of excess detection liquid.
The impact of the detection fluid on the detection results is reduced through lateral detection methods and the accuracy of the detection is improved.
Smart Images

Figure CN223192485U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aviation tire inflation leakage detection, in particular to aviation tire inflation leakage detection equipment. Background Art
[0002] Tires are annular elastic rubber products that roll on the ground and are assembled on various vehicles or machinery.
[0003] Existing aircraft tire inflation leakage detection equipment, such as the one disclosed in Chinese utility model patent application number CN202222276984.9, has a device for quickly detecting aircraft tire inflation leakage. The second threaded rod moves within the threaded sleeve to adjust the distance between the fastening sleeve and the limit plate, facilitating the fixing of tires of different sizes. The drive motor drives the driven gear to rotate, thereby driving the threaded sleeve to rotate, facilitating all-round detection of the tire.
[0004] However, during the inspection process of aircraft tire inflation leakage in the prior art inspection equipment, liquid flowing down from above may interfere with the inspection of the material below, thereby making the inspection result inaccurate. Utility Model Content
[0005] In order to solve the above technical problems, the present invention provides an aircraft tire inflation leakage detection device that adopts a horizontal detection method during the aircraft tire inflation leakage detection process by setting a flip mechanism and a cleaning mechanism, and cleans the material after the detection, thereby reducing the impact of excess detection liquid on the detection results.
[0006] The utility model provides an aircraft tire inflation leakage detection device, comprising a detection mechanism; a frame mechanism, a flip mechanism, a rotating mechanism, a clamping mechanism and a cleaning mechanism, wherein the flip mechanism is mounted on the frame mechanism, the rotating mechanism is mounted on the flip mechanism, the clamping mechanism is mounted on the rotating mechanism, the detection mechanism is mounted on the left end of the frame mechanism, and the cleaning mechanism is mounted on the rear end of the frame mechanism;
[0007] The frame mechanism is used for loading, the flipping mechanism is used for flipping, the rotating mechanism is used for rotating, the clamping mechanism is used for clamping, the detecting mechanism is used for detecting, and the cleaning mechanism is used for cleaning; the material is loaded by placing it on the frame mechanism, the material is clamped by opening the clamping mechanism, the material is flipped and placed horizontally by opening the flipping mechanism, the material is rotated by opening the rotating mechanism, and the material is detected by opening the detecting mechanism, and the detection liquid on the material is cleaned by opening the cleaning mechanism, so that during the aviation tire inflation leakage detection process, a horizontal detection method is adopted, and the material after detection is completed is cleaned, thereby reducing the influence of excess detection liquid on the detection result.
[0008] Preferably, the frame mechanism includes a water tank frame, a plate frame and a filter screen, the plate frame is installed on the upper end of the water tank frame, and the filter screen is slidably installed on the upper end of the water tank frame; the material is loaded by placing it on the filter screen and sliding the filter screen.
[0009] Preferably, the flipping mechanism includes a flipping frame, a worm gear, a motor 1 and a worm. The flipping frame is rotatably mounted on the water tank frame, the worm gear is mounted on the front end of the flipping frame, the motor 1 is mounted on the water tank frame, the worm is connected to the output end of the motor 1, and the worm and the worm gear are threadedly engaged; by turning on the worm gear of the motor 1 to transmit the transmission, the worm rotates, and while the worm rotates, it is threadedly engaged with the worm gear so that the worm gear drives the flipping frame to rotate.
[0010] Preferably, the rotating mechanism includes a turntable, a slave gear, a second motor and a main gear. The turntable is rotatably mounted on a flip frame, the slave gear is mounted on the turntable, the second motor is mounted in the flip frame, and the output end of the second motor extends to the outside of the turntable. The main gear is connected to the output end of the second motor, and the main gear is engaged with the slave gear. The main gear is rotated by turning on the second motor, and the main gear is engaged with the slave gear while the main gear rotates, so that the slave gear drives the turntable to rotate.
[0011] Preferably, the clamping mechanism includes a threaded rack, a threaded block, a screw, four groups of pressure rods and four groups of connecting rods. The threaded rack is mounted on the turntable through threads, the threaded block is slidably mounted on the threaded rack, the screw is rotatably mounted in the threaded rack, and the screw is threadedly matched with the threaded block. The four groups of pressure rods are rotatably mounted on the threaded rack, each group of pressure rods is rotatably connected to a group of connecting rods, and the four groups of connecting rods are rotatably connected to the threaded block; the threaded block is moved by rotating the screw and threading it with the threaded block, and while the threaded block moves, it cooperates with the connecting rod to support the pressure rod to limit the material, and the threaded rack is moved by rotating the threaded rack and threading it with the turntable to press the material.
[0012] Preferably, the detection mechanism includes a pump, a nozzle and a water pipe, the pump is installed at the left end of the water tank frame, the nozzle is rotatably installed on the water tank frame, and the pump output end and the nozzle input end are connected through a water pipe; the material is detected by turning on the pump to spray the detection liquid through the water pipe and the nozzle.
[0013] Preferably, the cleaning mechanism includes an air pump, an air outlet and an air duct. The air pump is installed at the rear end of the water tank rack, the air outlet is installed on the water tank rack, and the air pump output end and the air outlet input end are connected through a water pipe; the air pump is used to blow air through the air duct and the air outlet to clean the detection liquid on the material.
[0014] Compared with the prior art, the beneficial effects of the present invention are as follows: by placing the material on the frame mechanism for loading, by opening the clamping mechanism to clamp the material, by opening the flipping mechanism to flip the material to place it horizontally, by opening the rotating mechanism to rotate the material, and at the same time by opening the detection mechanism to detect the material, by opening the cleaning mechanism to clean the detection liquid on the material, so that during the aviation tire inflation leakage detection process, a horizontal detection method is adopted, and the material after detection is completed is cleaned, thereby reducing the influence of excess detection liquid on the detection results. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 This is a first axonometric structural diagram of the present invention;
[0016] Figure 2 This is a second axonometric structural diagram of the present invention;
[0017] Figure 3 This is a schematic diagram of the front-view cross-section axonometric structure of the present invention;
[0018] Figure 4 This is a schematic diagram of the left-side sectional axonometric structure of the present invention;
[0019] Figure 5 This is a schematic diagram of the axonometric structure of the utility model in top view;
[0020] Markings in the accompanying drawings: 1. Frame mechanism; 11. Water tank frame; 12. Plate frame; 13. Screen; 2. Turning mechanism; 21. Turning frame; 22. Worm gear; 23. Motor 1; 24. Worm; 3. Rotating mechanism; 31. Turntable; 32. Slave gear; 33. Motor 2; 34. Main gear; 4. Clamping mechanism; 41. Threaded frame; 42. Threaded block; 43. Screw; 44. Pressure rod; 45. Connecting rod; 5. Detection mechanism; 51. Pump; 52. Nozzle; 53. Water pipe; 6. Cleaning mechanism; 61. Air pump; 62. Air outlet; 63. Air duct. DETAILED DESCRIPTION
[0021] To facilitate understanding of the present invention, a more comprehensive description of the present invention will be provided below with reference to the accompanying drawings. The present invention can be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided to provide a more thorough and comprehensive understanding of the present invention.
[0022] Example 1
[0023] like Figures 1 to 5As shown, it includes a detection mechanism 5, a frame mechanism 1, a flip mechanism 2, a rotating mechanism 3, a clamping mechanism 4 and a cleaning mechanism 6. The flip mechanism 2 is mounted on the frame mechanism 1, the rotating mechanism 3 is mounted on the flip mechanism 2, the clamping mechanism 4 is mounted on the rotating mechanism 3, the detection mechanism 5 is mounted on the left end of the frame mechanism 1, and the cleaning mechanism 6 is mounted on the rear end of the frame mechanism 1;
[0024] The frame mechanism 1 performs loading, the flipping mechanism 2 performs flipping, the rotating mechanism 3 performs rotation, the clamping mechanism 4 performs clamping, the detecting mechanism 5 performs detection, and the cleaning mechanism 6 performs cleaning;
[0025] The frame mechanism 1 includes a water tank frame 11, a plate frame 12 and a leakage net 13. The plate frame 12 is mounted on the upper end of the water tank frame 11, and the leakage net 13 is slidably mounted on the upper end of the water tank frame 11.
[0026] The turning mechanism 2 includes a turning frame 21, a worm gear 22, a motor 23 and a worm 24. The turning frame 21 is rotatably mounted on the water tank frame 11. The worm gear 22 is mounted on the front end of the turning frame 21. The motor 23 is mounted on the water tank frame 11. The worm 24 is connected to the output end of the motor 23, and the worm 24 and the worm gear 22 are threaded together.
[0027] The rotating mechanism 3 includes a turntable 31, a slave gear 32, a second motor 33, and a main gear 34. The turntable 31 is rotatably mounted on the turning frame 21. The slave gear 32 is mounted on the turntable 31. The second motor 33 is mounted inside the turning frame 21, and the output end of the second motor 33 extends to the outside of the turntable 31. The main gear 34 is connected to the output end of the second motor 33 and meshes with the slave gear 32.
[0028] The clamping mechanism 4 includes a threaded frame 41, a threaded block 42, a screw 43, four groups of pressure rods 44 and four groups of connecting rods 45. The threaded frame 41 is mounted on the turntable 31 by threads, the threaded block 42 is slidably mounted on the threaded frame 41, the screw 43 is rotatably mounted in the threaded frame 41, and the screw 43 and the threaded block 42 are threadedly matched. The four groups of pressure rods 44 are rotatably mounted on the threaded frame 41, each group of pressure rods 44 is rotatably connected to a group of connecting rods 45, and the four groups of connecting rods 45 are rotatably connected to the threaded block 42.
[0029] The detection mechanism 5 includes a pump 51, a nozzle 52 and a water pipe 53. The pump 51 is installed at the left end of the water tank frame 11, and the nozzle 52 is rotatably installed on the water tank frame 11. The output end of the pump 51 is connected to the input end of the nozzle 52 through the water pipe 53.
[0030] The cleaning mechanism 6 includes an air pump 61, an air outlet 62 and an air duct 63. The air pump 61 is installed at the rear end of the water tank frame 11, and the air outlet 62 is installed on the water tank frame 11. The output end of the air pump 61 is connected to the input end of the air outlet 62 through the water pipe 53.
[0031] The material is placed on the screen 13 and the sliding screen 13 is used for loading. The screw 43 is rotated to engage with the threaded block 42 to move the threaded block 42. The threaded block 42 moves and cooperates with the connecting rod 45 to support the pressure rod 44 to limit the material. The threaded frame 41 is rotated to engage with the turntable 31 to move the threaded frame 41 to press the material. The motor 23 is turned on to drive the worm 24 to rotate the worm 24. The worm 24 rotates and engages with the worm wheel 22 to drive the turning frame 21 to rotate, so that the material is turned over and placed horizontally. By turning on the second motor 33 to transmit the power to the main gear 34 so that the main gear 34 rotates, the main gear 34 engages with the slave gear 32 while rotating, so that the slave gear 32 drives the turntable 31 to rotate. At the same time, by turning on the pump 51, the test liquid is sprayed out through the water pipe 53 in cooperation with the nozzle 52 to test the material. The air pump 61 blows air through the air duct 63 in cooperation with the air port 62 to clean the test liquid on the material. In this way, during the aircraft tire inflation leakage test, a horizontal test method is adopted, and the material after the test is completed is cleaned, thereby reducing the influence of excess test liquid on the test result.
[0032] like Figures 1 to 5 As shown, the present invention is an aircraft tire inflation leakage detection device. When working, the material is placed on the leakage screen 13 and the leakage screen 13 is slid to load the material. The threaded block 42 is moved by rotating the screw 43 and threadedly engaged with the threaded block 42. While the threaded block 42 moves, it cooperates with the connecting rod 45 to support the pressure rod 44 to limit the material. The threaded frame 41 is rotated and threadedly engaged with the turntable 31 to move the threaded frame 41 to press the material. The worm 24 is rotated by turning on the motor 1 23 to drive the worm 24. As the worm 24 rotates, it engages with the worm wheel 22 in a threaded manner, so that the worm wheel 22 drives the turning frame 21 to rotate, so that the material is turned over and placed horizontally. By turning on the second motor 33, the main gear 34 is driven to rotate the main gear 34. While the main gear 34 rotates, it engages with the slave gear 32, so that the slave gear 32 drives the turntable 31 to rotate. At the same time, by turning on the pump 51, the detection liquid is sprayed out through the water pipe 53 and the nozzle 52 to detect the material. The air pump 61 is used to blow air through the air duct 63 and the air port 62 to clean the detection liquid on the material.
[0033] The motor 1 23, the motor 2 33, the pump 51 and the air pump 61 of the present invention are purchased on the market. The technicians in this industry only need to install and operate them according to the accompanying instruction manuals without the need for the technicians in this field to make creative efforts.
[0034] The main functions achieved by the utility model are: during the aircraft tire inflation leakage detection process, by setting a turning mechanism and a cleaning mechanism, the aircraft tire inflation leakage detection process can adopt a horizontal detection method, and the material after the detection is completed can be cleaned, thereby reducing the influence of excess detection liquid on the detection results.
[0035] The above is only a preferred embodiment of the present invention. It should be pointed out that for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the technical principles of the present invention. These improvements and modifications should also be regarded as the scope of protection of the present invention.
Claims
1. An aircraft tire inflation leakage detection device, comprising a detection mechanism (5); characterized in that: The device further comprises a frame mechanism (1), a turning mechanism (2), a rotating mechanism (3), a clamping mechanism (4) and a cleaning mechanism (6), wherein the turning mechanism (2) is mounted on the frame mechanism (1), the rotating mechanism (3) is mounted on the turning mechanism (2), the clamping mechanism (4) is mounted on the rotating mechanism (3), the detecting mechanism (5) is mounted on the left end of the frame mechanism (1), and the cleaning mechanism (6) is mounted on the rear end of the frame mechanism (1); The frame mechanism (1) performs loading, the flipping mechanism (2) performs flipping, the rotating mechanism (3) performs rotation, the clamping mechanism (4) performs clamping, the detecting mechanism (5) performs detection, and the cleaning mechanism (6) performs cleaning.
2. The aircraft tire inflation leakage detection device according to claim 1, characterized in that: The frame mechanism (1) comprises a water tank frame (11), a plate frame (12) and a leakage net (13); the plate frame (12) is mounted on the upper end of the water tank frame (11); and the leakage net (13) is slidably mounted on the upper end of the water tank frame (11).
3. The aircraft tire inflation leakage detection device according to claim 2, characterized in that: The turning mechanism (2) comprises a turning frame (21), a worm gear (22), a motor (23) and a worm (24); the turning frame (21) is rotatably mounted on the water tank frame (11); the worm gear (22) is mounted on the front end of the turning frame (21); the motor (23) is mounted on the water tank frame (11); the worm (24) is connected to the output end of the motor (23); and the worm (24) and the worm gear (22) are threadedly engaged.
4. The aircraft tire inflation leakage detection device according to claim 3, characterized in that: The rotating mechanism (3) comprises a turntable (31), a slave gear (32), a second motor (33) and a main gear (34); the turntable (31) is rotatably mounted on the turning frame (21); the slave gear (32) is mounted on the turntable (31); the second motor (33) is mounted in the turning frame (21); and the output end of the second motor (33) extends to the outside of the turntable (31); the main gear (34) is connected to the output end of the second motor (33), and the main gear (34) is meshed with the slave gear (32).
5. The aircraft tire inflation leakage detection device according to claim 4, characterized in that: The clamping mechanism (4) comprises a threaded frame (41), a threaded block (42), a screw (43), four groups of pressure rods (44) and four groups of connecting rods (45). The threaded frame (41) is mounted on the turntable (31) through a thread, the threaded block (42) is slidably mounted on the threaded frame (41), the screw (43) is rotatably mounted in the threaded frame (41), and the screw (43) and the threaded block (42) are threadedly matched. The four groups of pressure rods (44) are rotatably mounted on the threaded frame (41), each group of pressure rods (44) is rotatably connected to a group of connecting rods (45), and the four groups of connecting rods (45) are rotatably connected to the threaded block (42).
6. The aircraft tire inflation leakage detection device according to claim 2, characterized in that: The detection mechanism (5) comprises a pump (51), a nozzle (52) and a water pipe (53). The pump (51) is mounted on the left end of the water tank frame (11). The nozzle (52) is rotatably mounted on the water tank frame (11). The output end of the pump (51) and the input end of the nozzle (52) are connected via the water pipe (53).
7. The aircraft tire inflation leakage detection device according to claim 2, characterized in that: The cleaning mechanism (6) comprises an air pump (61), an air outlet (62) and an air duct (63). The air pump (61) is mounted on the rear end of the water tank frame (11), the air outlet (62) is mounted on the water tank frame (11), and the output end of the air pump (61) is connected to the input end of the air outlet (62) via a water pipe (53).
Citation Information
Patent Citations
Device for rapidly detecting inflation leakage of aircraft tire
CN218271230U