Aircraft air intake detection equipment
By designing a detection device for the air intake duct of the aircraft, using lifting and rotating mechanisms and detection mechanisms, the problems of low risk and reliability of traditional manual inspections are solved, and the detection effect of high accuracy and safety is achieved.
Patent Information
- Application Number
- CN202211005043.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-08-22
- Publication Date
- 2025-04-25
- Estimated Expiration
- 2042-08-22
AI Technical Summary
Traditional manual inspection of aircraft air intake has problems of low risk and reliability, resulting in inaccurate inspection results.
An aircraft intake duct detection device is designed, using a lifting mechanism and a rotating mechanism, entering the intake duct through a fixed ring and a detection mechanism, and comprehensive inspection is performed using a camera and searchlight, and video is transmitted to the display.
It improves the safety and reliability of aircraft intake duct detection, ensures the accuracy and comprehensiveness of the detection results, and reduces the risk of manual inspection.
Smart Images

Figure CN115465471B_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of aircraft air inlet ducts, in particular to aircraft air inlet duct detection equipment. Background Art
[0002] The air inlet not only supplies a certain flow of air to the engine, but also the air flow field of the inlet must ensure the normal operation of the compressor and the combustion chamber. The Mach number of the turbojet engine compressor inlet flow velocity is about 0.4, which has strict restrictions on the unevenness of the flow field. During flight, the air inlet must achieve deceleration and pressurization of the high-speed airflow, converting the kinetic energy of the airflow into pressure energy. As the flight speed increases, the pressurization effect of the air inlet becomes greater and greater, and the pressurization effect during supersonic flight can greatly exceed that of the compressor, so the air inlet of a supersonic aircraft plays an important role in improving flight performance;
[0003] The aircraft needs to be inspected before takeoff. During the aircraft inspection, the aircraft air intake inspection is one of the key points of ground inspection. Check whether there is any damage on the surface of the aircraft air intake, mainly including checking whether the rivets are intact, whether there are any loose parts, whether there are any foreign objects, etc.
[0004] The traditional method is to conduct manual visual inspection by ground crew, who stand on a ladder and shine a flashlight into the air inlet to observe whether there is any damage on the surface of the air inlet. This method is not only dangerous, but also has inaccurate inspection results and low reliability. In view of the above problems, the inventor proposes an aircraft air inlet inspection device to solve the above problems. Summary of the invention
[0005] In order to solve the problem of inaccurate manual inspection results and low reliability, the present invention aims to provide an aircraft air intake inspection device.
[0006] To solve the above technical problems, the present invention adopts the following technical solutions: an aircraft air inlet detection device, comprising a first fixed plate, a second fixed plate and an air inlet, wherein a roller is fixedly provided on the lower surface of the first fixed plate, a support rod is slidably provided on the upper surface of the second fixed plate, a fixed frame is fixedly provided on the upper end of the support rod, a pair of connecting rods are fixedly provided on one side of the fixed frame, a fixing ring is fixedly provided on the end of the connecting rod away from the fixing frame, a rotating ring is rotatably provided on the fixing ring, a lifting mechanism is provided on the first fixed plate and the second fixed plate, a rotating mechanism is provided on the support rod, a detection mechanism is provided on the rotating ring, the first fixed plate and the second fixed plate are of the same size, the upper end of the support rod is located at the center of the fixed frame, and the connecting rod is located at the edge of the rotating ring.
[0007] Preferably, the lifting mechanism comprises a fixed block and a limit block, the fixed block and the limit block are fixedly connected to the upper surface of the first fixed plate and the lower surface of the second fixed plate, the limit block is provided with a driving groove, the fixed block is rotatably provided with a first rotating rod, the driving groove is slidably provided with a driving rod, and the driving rod is rotatably provided with a second rotating rod, a central axis is inserted in the middle of the first rotating rod, the central axis is rotatably connected to the second rotating rod, the first rotating rod is rotatably connected to the driving rod at one end away from the fixed block, and the second rotating rod is rotatably connected to the fixed block at one end away from the driving rod, and the first fixed plate The upper surface is fixedly provided with a mounting block, and one side of the mounting block is fixedly provided with a cylinder, and the cylinder is rotatably connected to the driving rod, and the first rotating rod and the second rotating rod are each provided with two pairs, and the first rotating rod and the second rotating rod are equal in length, and the driving rod is in contact with the inner wall of the driving groove.
[0008] Preferably, a moving groove is provided on the upper surface of the second fixed plate, a moving block is slidably provided in the moving groove, the upper surface of the moving block is fixedly connected to the lower end of the support rod, a first threaded rod is rotatably provided in the moving groove, the first threaded rod is threadedly connected to the moving block, one end of the first threaded rod passes through the second fixed plate, a rotating handle is fixedly provided on one end of the first threaded rod, a display is fixed on the fixed frame, a guardrail is fixedly provided on the upper surface of the second fixed plate, the moving block is in contact with the inner wall of the moving groove, and the support rod is located at the center of the moving block.
[0009] Preferably, the rotating mechanism includes a rotating shaft, which is rotatably connected to the support rod, a motor is fixedly provided on one side of the support rod, and the output end of the motor is fixedly connected to the rotating shaft, a rotating gear is fixedly provided on one end of the rotating shaft away from the support rod, a plurality of circular rods are fixedly provided on one side of the rotating ring, the rotating gears are meshed with the circular rods, a rotating groove is provided on the inner side of the fixed ring, the rotating ring is fitted with the inner wall of the rotating groove, the rotating shaft is located in the middle of the support rod, and the circular rods are distributed in a ring shape.
[0010] Preferably, the detection mechanism includes a fixed column, which is fixedly connected to the rotating ring, the fixed column passes through the rotating ring, a limiting groove is provided on the fixed column, a second threaded rod is rotatably provided in the limiting groove, a movable column is slidably provided in the limiting groove, the movable column is threadedly connected to the second threaded rod, one end of the second threaded rod passes through the fixed column, a driving ring is fixedly provided at one end of the second threaded rod, a protective box is fixedly provided at one end of the movable column, a camera is fixed in the protective box, a searchlight is fixed on the protective box, the movable column is in contact with the inner wall of the limiting groove, the fixed column is located at the edge of the rotating ring, a connecting groove is provided on the protective box, and the camera is opposite to the connecting groove.
[0011] Compared with the prior art, the present invention has the following beneficial effects:
[0012] The ground crew stands on the upper surface of the second fixed plate and drives the lifting mechanism through the cylinder. The lifting mechanism drives the second fixed plate to rise, so that the fixed ring is parallel to the air inlet duct, and moves the support rod. The support rod drives the fixed frame to move, and the fixed frame drives the connecting rod to move. The connecting rod drives the fixed ring to move into the air inlet duct. The fixed ring drives the detection mechanism to enter the air inlet duct, and the inner wall of the air inlet duct is detected by the detection mechanism. The detection mechanism transmits the video to the display, and then drives the rotating ring to rotate through the rotating mechanism. The rotating ring drives the detection mechanism to rotate, and the detection mechanism conducts a comprehensive inspection of the inner wall of the air inlet duct. BRIEF DESCRIPTION OF THE DRAWINGS
[0013] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.
[0014] Figure 1 It is a schematic diagram of the structure of the present invention.
[0015] Figure 2 It is a schematic diagram of the cross-sectional structure of the air intake duct of the present invention.
[0016] Figure 3 It is a schematic diagram of the lifting mechanism structure of the present invention.
[0017] Figure 4 It is a schematic diagram of the structure of the moving block of the present invention.
[0018] Figure 5 It is a schematic diagram of the structure of the rotating mechanism of the present invention.
[0019] Figure 6 It is a schematic diagram of the cross-sectional structure of the fixing column of the present invention.
[0020] Figure 7 It is a schematic diagram of the cross-sectional structure of the protection box of the present invention.
[0021] In the figure: 1. first fixed plate; 11. second fixed plate; 12. air inlet; 13. roller; 14. support rod; 15. fixed frame; 16. connecting rod; 17. fixed ring; 18. rotating ring; 2. lifting mechanism; 21. fixed block; 22. limit block; 23. driving groove; 24. first rotating rod; 25. driving rod; 26. second rotating rod; 27. central axis; 28. mounting block; 29. cylinder; 3. moving groove; 31. moving block; 32. first threaded rod; 33. rotating handle; 34. display; 35. guardrail; 4. rotating mechanism; 41. round rod; 42. rotating shaft; 43. rotating gear; 44. motor; 45. rotating groove; 5. detection mechanism; 51. fixed column; 52. limit groove; 53. second threaded rod; 54. moving column; 55. protection box; 56. driving ring; 57. camera; 58. searchlight. DETAILED DESCRIPTION
[0022] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.
[0023] like Figure 1-7 As shown, the present invention provides: an aircraft air inlet detection device, comprising a first fixing plate 1, a second fixing plate 11 and an air inlet 12, a roller 13 is fixedly provided on the lower surface of the first fixing plate 1, a support rod 14 is slidably provided on the upper surface of the second fixing plate 11, a fixing frame 15 is fixedly provided on the upper end of the support rod 14, a pair of connecting rods 16 are fixedly provided on one side of the fixing frame 15, a fixing ring 17 is fixedly provided on one end of the connecting rod 16 away from the fixing frame 15, a rotating ring 18 is rotatably provided on the fixing ring 17, a lifting mechanism 2 is provided on the first fixing plate 1 and the second fixing plate 11, a rotating mechanism 4 is provided on the support rod 14, a detection mechanism 5 is provided on the rotating ring 18, the first fixing plate 1 and the second fixing plate 11 are of the same size, the upper end of the support rod 14 is located at the center of the fixing frame 15, and the connecting rod 16 is located at the edge of the rotating ring 18.
[0024] By adopting the above technical solution, the ground crew stands on the upper surface of the second fixed plate 11, and drives the lifting mechanism 2 to operate through the cylinder 29. The lifting mechanism 2 drives the second fixed plate 11 to rise, so that the fixing ring 17 is parallel to the air inlet 12, and moves the support rod 14. The support rod 14 drives the fixing frame 15 to move, and the fixing frame 15 drives the connecting rod 16 to move. The connecting rod 16 drives the fixing ring 17 to move into the air inlet 12, and the fixing ring 17 drives the detection mechanism 5 to enter the air inlet 12. The inner wall of the air inlet 12 is detected by the detection mechanism 5, and the detection mechanism 5 transmits the video to the display 34. The rotating ring 18 is driven to rotate by the rotating mechanism 4, and the rotating ring 18 drives the detection mechanism 5 to rotate. The detection mechanism 5 performs a comprehensive inspection on the inner wall of the air inlet 12.
[0025] The lifting mechanism 2 includes a fixed block 21 and a limiting block 22, which are fixedly connected to the upper surface of the first fixed plate 1 and the lower surface of the second fixed plate 11. A driving groove 23 is opened on the limiting block 22. A first rotating rod 24 is rotatably provided on the fixed block 21, and a driving rod 25 is slidably provided in the driving groove 23. A second rotating rod 26 is rotatably provided on the driving rod 25. A central axis 27 is inserted in the middle of the first rotating rod 24, and the central axis 27 is rotatably connected to the second rotating rod 26. The end of the first rotating rod 24 away from the fixed block 21 is rotatably connected to the driving rod 25, and the end of the second rotating rod 26 away from the driving rod 25 is rotatably connected to the fixed block 21. A mounting block 28 is fixedly provided on the upper surface of the first fixed plate 1, and a cylinder 29 is fixedly provided on one side of the mounting block 28. The cylinder 29 is rotatably connected to the driving rod 25. Two pairs of the first rotating rod 24 and the second rotating rod 26 are provided. The first rotating rod 24 and the second rotating rod 26 are equal in length, and the driving rod 25 fits the inner wall of the driving groove 23.
[0026] By adopting the above technical solution, the cylinder 29 drives the driving rod 25 to move, and the driving rod 25 drives to move along the driving groove 23 on the limit block 22, and the driving rod 25 drives the second rotating rod 26 to rotate, the middle part of the second rotating rod 26 rotates along the central axis 27, and the upper end drives the first rotating rod 24 to rotate, and the first rotating rod 24 drives another driving rod 25 to move along the driving groove 23, so that the second fixed plate 11 rises, and the rising of the second fixed plate 11 drives another second rotating rod 26 to rotate, the lower end of the second rotating rod 26 drives another first rotating rod 24 to rotate, and the lower end of the first rotating rod 24 rotates along the fixed block 21.
[0027] A moving groove 3 is provided on the upper surface of the second fixed plate 11, and a moving block 31 is slidably provided in the moving groove 3. The upper surface of the moving block 31 is fixedly connected to the lower end of the support rod 14. A first threaded rod 32 is rotatably provided in the moving groove 3. The first threaded rod 32 is threadedly connected to the moving block 31. One end of the first threaded rod 32 passes through the second fixed plate 11, and a rotating handle 33 is fixedly provided on one end of the first threaded rod 32. A display 34 is fixed on the fixed frame 15. A guardrail 35 is fixedly provided on the upper surface of the second fixed plate 11. The moving block 31 is in contact with the inner wall of the moving groove 3, and the support rod 14 is located at the center of the moving block 31.
[0028] By adopting the above technical solution, by rotating the rotating handle 33, the rotating handle 33 drives the first threaded rod 32 to rotate, the first threaded rod 32 drives the moving block 31 to move along the moving groove 3, the movement of the moving block 31 drives the support rod 14 to move, the support rod 14 drives the fixing frame 15 to move, the fixing frame 15 drives the connecting rod 16 to move, and the connecting rod 16 drives the fixing ring 17 to move into the air inlet duct 12.
[0029] The rotating mechanism 4 includes a rotating shaft 42, which is rotatably connected to the support rod 14. A motor 44 is fixedly arranged on one side of the support rod 14, and the output end of the motor 44 is fixedly connected to the rotating shaft 42. A rotating gear 43 is fixedly arranged on the end of the rotating shaft 42 away from the support rod 14. A plurality of circular rods 41 are fixedly arranged on one side of the rotating ring 18, and the rotating gears 43 are meshed with the circular rods 41. A rotating groove 45 is opened on the inner side of the fixed ring 17, and the rotating ring 18 is fitted with the inner wall of the rotating groove 45. The rotating shaft 42 is located in the middle of the support rod 14, and the circular rods 41 are distributed in a ring shape.
[0030] By adopting the above technical solution, the motor 44 drives the rotating shaft 42 to rotate, the rotating shaft 42 drives the rotating gear 43 to rotate, the rotating gear 43 drives the circular rod 41 to rotate, the circular rod 41 drives the rotating ring 18 to rotate, the rotating ring 18 rotates along the rotating groove 45 on the fixed ring 17, the rotating ring 18 drives the fixed column 51 to rotate, the fixed column 51 drives the movable column 54 to rotate, the movable column 54 drives the protective box 55 to rotate, the protective box 55 drives the camera 57 to rotate, so as to inspect the inner wall of the air intake duct 12.
[0031] The detection mechanism 5 includes a fixed column 51, which is fixedly connected to the rotating ring 18. The fixed column 51 passes through the rotating ring 18. A limiting groove 52 is provided on the fixed column 51. A second threaded rod 53 is rotatably provided in the limiting groove 52. A movable column 54 is slidably provided in the limiting groove 52. The movable column 54 is threadedly connected to the second threaded rod 53. One end of the second threaded rod 53 passes through the fixed column 51. A driving ring 56 is fixedly provided at one end of the second threaded rod 53. A protective box 55 is fixedly provided at one end of the movable column 54. A camera 57 is fixed in the protective box 55. A searchlight 58 is fixed on the protective box 55. The movable column 54 is in contact with the inner wall of the limiting groove 52. The fixed column 51 is located at the edge of the rotating ring 18. A connecting groove is provided on the protective box 55. The camera 57 is directly opposite to the connecting groove.
[0032] By adopting the above technical solution, the inner wall of the air intake duct 12 is illuminated by the searchlight 58, which is convenient for the camera 57 to observe. The second threaded rod 53 is driven to rotate by rotating the driving ring 56, and the second threaded rod 53 drives the moving column 54 to move along the limiting groove 52. The moving column 54 drives the protective box 55 to move, so that the camera 57 enters deep inside the air intake duct 12 to conduct a comprehensive inspection of the inner wall of the air intake duct 12.
[0033] Working principle: First, the ground staff stands on the upper surface of the second fixed plate 11, and drives the driving rod 25 to move through the cylinder 29. The driving rod 25 drives the driving groove 23 on the limit block 22, and the driving rod 25 drives the second rotating rod 26 to rotate. The middle part of the second rotating rod 26 rotates along the central axis 27, and the upper end drives the first rotating rod 24 to rotate. The first rotating rod 24 drives another driving rod 25 to move along the driving groove 23, so that the second fixed plate 11 rises, and the second fixed plate 11 rises and drives another second rotating rod 26 to rotate. The lower end of the second rotating rod 26 drives another first rotating rod 24 to rotate, and the lower end of the first rotating rod 24 rotates along the fixed block 21. Then, by rotating the rotating handle 33, the rotating handle 33 drives the first threaded rod 32 to rotate, and the first threaded rod 32 drives the moving block 31 to move along the moving groove 3. The movement of the moving block 31 drives the support rod 14 to move, the support rod 14 drives the fixed frame 15 to move, and the fixed frame 15 drives the connecting rod 1 6 moves, the connecting rod 16 drives the fixed ring 17 to move into the air inlet 12, and then the searchlight 58 is used to illuminate the inner wall of the air inlet 12, so that the camera 57 can observe it, and the second threaded rod 53 is driven to rotate by rotating the driving ring 56, and the second threaded rod 53 drives the moving column 54 to move along the limiting groove 52, and the moving column 54 drives the protection box 55 to move, so that the camera 57 enters the deep inside of the air inlet 12 to fully detect the inner wall of the air inlet 12, and then the motor 44 drives the rotating shaft 42 to rotate, the rotating shaft 42 drives the rotating gear 43 to rotate, the rotating gear 43 drives the circular rod 41 to rotate, the circular rod 41 drives the rotating ring 18 to rotate, the rotating ring 18 rotates along the rotating groove 45 on the fixed ring 17, the rotating ring 18 drives the fixed column 51 to rotate, the fixed column 51 drives the moving column 54 to rotate, the moving column 54 drives the protection box 55 to rotate, and the protection box 55 drives the camera 57 to rotate to inspect the inner wall of the air inlet 12.
[0034] Obviously, those skilled in the art can make various changes and modifications to the present invention without departing from the spirit and scope of the present invention. Thus, if these modifications and variations of the present invention fall within the scope of the claims of the present invention and their equivalents, the present invention is also intended to include these modifications and variations.
Claims
1. An aircraft air inlet detection device, comprising a first fixing plate, a second fixing plate and an air inlet, characterized in that: A roller is fixedly provided on the lower surface of the first fixed plate, a support rod is slidably provided on the upper surface of the second fixed plate, a fixed frame is fixedly provided on the upper end of the support rod, a pair of connecting rods are fixedly provided on one side of the fixed frame, a fixing ring is fixedly provided on the end of the connecting rod away from the fixing frame, a rotating ring is rotatably provided on the fixing ring, a lifting mechanism is provided on the first fixed plate and the second fixed plate, a rotating mechanism is provided on the support rod, and a detection mechanism is provided on the rotating ring; The rotating mechanism includes a rotating shaft, the rotating shaft is rotatably connected to the support rod, a motor is fixedly provided on one side of the support rod, the output end of the motor is fixedly connected to the rotating shaft, a rotating gear is fixedly provided on one end of the rotating shaft away from the support rod, a plurality of circular rods are fixedly provided on one side of the rotating ring, the rotating gears are meshed with the circular rods, a rotating groove is provided on the inner side of the fixed ring, and the rotating ring is in contact with the inner wall of the rotating groove; The detection mechanism includes a fixed column, which is fixedly connected to a rotating ring. The fixed column passes through the rotating ring. A limiting groove is provided on the fixed column. A second threaded rod is rotatably provided in the limiting groove. A movable column is slidably provided in the limiting groove. The movable column is threadedly connected to the second threaded rod. One end of the second threaded rod passes through the fixed column. A driving ring is fixedly provided at one end of the second threaded rod. A protective box is fixedly provided at one end of the movable column. A camera is fixedly provided in the protective box. A searchlight is fixedly provided on the protective box.
2. An aircraft air inlet detection device as claimed in claim 1, characterized in that: The lifting mechanism includes a fixed block and a limit block, wherein the fixed block and the limit block are fixedly connected to the upper surface of the first fixed plate and the lower surface of the second fixed plate, the limit block is provided with a driving groove, the fixed block is rotatably provided with a first rotating rod, a driving rod is slidably provided in the driving groove, and a second rotating rod is rotatably provided on the driving rod, a central axis is inserted in the middle of the first rotating rod, and the central axis is rotatably connected to the second rotating rod, the first rotating rod is rotatably connected to the driving rod at one end away from the fixed block, and the second rotating rod is rotatably connected to the fixed block at one end away from the driving rod, and a mounting block is fixedly provided on the upper surface of the first fixed plate, and a cylinder is fixedly provided on one side of the mounting block, and the cylinder is rotatably connected to the driving rod.
3. The aircraft air inlet detection device according to claim 1, characterized in that: A moving groove is provided on the upper surface of the second fixed plate, a moving block is slidably provided in the moving groove, the upper surface of the moving block is fixedly connected to the lower end of the support rod, a first threaded rod is rotatably provided in the moving groove, the first threaded rod is threadedly connected to the moving block, one end of the first threaded rod passes through the second fixed plate, a rotating handle is fixedly provided on one end of the first threaded rod, a display is fixed on the fixed frame, and a guardrail is fixedly provided on the upper surface of the second fixed plate.
4. The aircraft air inlet detection device according to claim 1, characterized in that: The movable column is fitted with the inner wall of the limiting groove, the fixed column is located at the edge of the rotating ring, a connecting groove is opened on the protection box, and the camera is directly opposite to the connecting groove.
5. The aircraft air inlet detection device according to claim 1, characterized in that: The rotating shaft is located in the middle of the supporting rod, and the circular rods are distributed in a ring shape.
6. The aircraft air inlet detection device according to claim 3, characterized in that: The moving block is in contact with the inner wall of the moving groove, and the supporting rod is located at the center of the moving block.
7. The aircraft air inlet detection device according to claim 2, characterized in that: The first rotating rod and the second rotating rod are each provided with two pairs, the first rotating rod and the second rotating rod are equal in length, and the driving rod is in contact with the inner wall of the driving groove.
8. The aircraft air inlet detection device according to claim 1, characterized in that: The first fixing plate and the second fixing plate are of the same size, the upper end of the support rod is located at the center of the fixing frame, and the connecting rod is located at the edge of the rotating ring.
Citation Information
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