Aircraft tire maintenance device
By designing an aviation tire maintenance device including a clamping mechanism, the problems of inconvenience in removing large-weight aviation tires, easy damage to bottom plate parts and high labor consumption in the prior art are solved, and convenient tire removal and maintenance efficiency are improved.
Patent Information
- Application Number
- CN202420301043.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-02-19
- Publication Date
- 2025-03-14
- Estimated Expiration
- 2034-02-19
AI Technical Summary
When the existing aviation tire maintenance device removes the large-weight aviation tire from the storage shaft, it is inconvenient and easy to damage the bottom plate parts, and requires a lot of manpower.
An aviation tire maintenance device including a clamping mechanism is designed. The clamping mechanism is composed of a jaw, a support plate, a pulley and a servo motor. The threaded rod is driven by the servo motor, the first and second moving blocks are moved, and the push frame and the support plate are pushed to achieve clamping and smooth removal of the tire.
It is achieved to facilitate removal of high-weight aviation tires from the storage shaft, reducing damage to bottom plate parts, reducing manpower consumption and improving maintenance efficiency.
Smart Images

Figure CN222607495U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the field of tire maintenance devices, in particular to an aviation tire maintenance device. Background Art
[0002] Aircraft tires will directly affect the stability and safety of aircraft operation. Proper maintenance and care can ensure flight safety and reduce maintenance costs. Therefore, aircraft tires need to be maintained frequently using maintenance devices.
[0003] According to the patent document: CN202222924577.4, a tire maintenance device applied to the aviation industry is proposed, which belongs to the field of tire maintenance devices and includes: a base plate; a rotating pushing mechanism, which is arranged on the top of the base plate; an aviation industry tire, which is sleeved on the rotating pushing mechanism, and the rotating pushing mechanism is used to realize the rotation of the aviation industry tire; a limiting mechanism, which is arranged on the top of the base plate; a pushing mechanism, which is arranged on the top of the base plate; a U-shaped spray pipe, which is arranged on the pushing mechanism, and the pushing mechanism is used to realize the movement of the U-shaped spray pipe; and a water supply mechanism, which is arranged on the top of the base plate, and the water supply mechanism is connected to the U-shaped spray pipe. The utility model can spray water on the aviation industry tire through the U-shaped spray pipe, so as to clean and maintain the aviation industry tire, which can solve the problem that the tire maintenance device in the prior art needs to be manually cleaned with a high-pressure water gun when cleaning and maintaining the tire, and the manual hand-held high-pressure water gun cleaning has low efficiency.
[0004] However, one of the above technologies is used in the tire maintenance device for the aviation industry. Although it is convenient to clean the tire surface, due to the heavy weight of the aviation industry tire itself and the limited space on the bottom plate for the tire to move, it is necessary to avoid the tire from damaging other parts on the bottom plate during the process of removing the tire from the storage shaft, which consumes a lot of manpower. Therefore, it is urgent to propose an aviation tire maintenance device to address the above problems. Utility Model Content
[0005] One of the above technologies is a tire maintenance device applied to the aviation industry. However, there are problems such as it is inconvenient to take heavy aircraft tires, the limited floor space makes the tires easily damage floor components, and it takes a lot of manpower to take them. In order to make up for the deficiencies of the prior art, the utility model proposes an aircraft tire maintenance device.
[0006] The technical solution adopted by the utility model to solve its technical problems is: an aviation tire maintenance device described in the utility model comprises a bottom plate, a vertical plate, a tire main body and a storage shaft; a clamping mechanism is arranged on the bottom plate, the clamping mechanism comprises two groups of claws, the claws are located directly below the tire main body, the bottom ends of the claws are rotatably connected to the grooves, the grooves are arranged on the support plate, a plurality of groups of pulleys are fixedly connected to the bottom end of the support plate, the pulleys are slidably connected to the slide grooves, a connecting plate is fixedly connected to one side of the support plate, a group of bottom ends of the support plates are fixedly connected to a second moving block, the second moving block is arranged inside a cavity, the cavity is arranged inside the bottom plate, a first moving block and a second moving block are threadedly connected to the cavity, a push frame is fixedly connected to the top end of the first moving block, a through groove and a slide groove are arranged on the bottom plate, the left side of the threaded rod is rotatably connected to the inner wall of the cavity, the right side of the cavity is fixedly connected to a servo motor, and a notch is arranged on the vertical plate.
[0007] Preferably, the first moving block and the second moving block are both fixedly connected to limiting blocks on both the front and rear sides, the limiting blocks are slidably connected inside the limiting grooves, and the limiting grooves are provided on the inner wall of the through grooves.
[0008] Preferably, a cushion block is fixedly connected to the right side of the inner wall of the through groove, and the cushion block is made of rubber material.
[0009] Preferably, a fixing groove is provided on one side of the top end of the push frame close to the tire body, and the fixing groove is designed to be arc-shaped.
[0010] Preferably, the claw is provided with a step, and a rubber plate is fixedly connected to the step.
[0011] Preferably, a plurality of drainage holes are provided on the bottom end of the inner wall of the cavity, and the drainage holes are connected to the outside.
[0012] Beneficial effects of the utility model:
[0013] 1. The utility model realizes the function of facilitating the removal of the tire body from the storage shaft through the structural design of the clamping mechanism, solving the problems of the above-mentioned technologies that heavy aviation tires are inconvenient to take, the limited floor space makes it easy for the tires to damage the floor components, and the labor-intensive removal;
[0014] 2. The utility model realizes that the limit groove and the limit block can guide the first moving block and the second moving block when they move on the threaded rod through the structural design of the limit groove and the limit block, ensuring that the first moving block and the second moving block can move stably on the threaded rod, and through the contact between the limit block and the inner wall of the limit groove, the bearing capacity of the support plate can also be improved. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] In order to more clearly illustrate the embodiments of the utility model 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 utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.
[0016] Figure 1 It is a three-dimensional structural schematic diagram of the utility model;
[0017] Figure 2 It is a structural schematic diagram of the left side of the utility model;
[0018] Figure 3 It is a structural schematic diagram of the clamping mechanism of the utility model;
[0019] Figure 4 It is a schematic diagram of the cross-sectional structure of the utility model;
[0020] Figure 5 It is a structural schematic diagram of the clamping claw of the utility model.
[0021] In the figure: 1, bottom plate; 20, vertical plate; 21, tire body; 22, storage shaft; 23, first moving block; 24, push frame; 25, second moving block; 26, cavity; 27, threaded rod; 28, servo motor; 30, support plate; 31, connecting plate; 32, groove; 33, claw; 34, notch; 35, pulley; 36, through groove; 37, slide groove; 38, pad; 39, limit groove; 40, limit block; 41, drainage hole; 42, fixing groove; 43, rubber plate; 44, step. DETAILED DESCRIPTION
[0022] 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.
[0023] See also Figure 1 - Figure 5As shown, an aircraft tire maintenance device includes a bottom plate 1, a vertical plate 20, a tire body 21 and a storage shaft 22; a clamping mechanism is arranged on the bottom plate 1, and the clamping mechanism includes two groups of claws 33, the claws 33 are located directly below the tire body 21, and the bottom ends of the claws 33 are rotatably connected to the grooves 32, and the grooves 32 are arranged on the support plate 30, and the support plate 30 is rectangular in design, and multiple groups of pulleys 35 are welded and fixed on the bottom end of the support plate 30, and the pulleys 35 are slidably connected to the slide grooves 37, and the slide grooves 37 are long rectangular in design, and a connecting plate 31 is welded and fixed on one side of the support plate 30, and the connecting plate 31 is rectangular in design and the bottom end does not contact with the bottom plate 1 to avoid displacement. The second moving block 25 is welded and fixed at the bottom end of a group of support plates 30, and the second moving block 25 is arranged inside the cavity 26. The cavity 26 is cylindrical in design, and the cavity 26 is opened inside the bottom plate 1. The first moving block 23 and the second moving block 25 are threadedly connected on the cavity 26. The top of the first moving block 23 is welded and fixed with a push frame 24. A through groove 36 and a slide groove 37 are opened on the bottom plate 1. The left side of the threaded rod 27 is rotatably connected to the inner wall of the cavity 26. The right side of the cavity 26 is fixedly connected with a servo motor 28. A notch 34 is opened on the vertical plate 20. The notch 34 is rectangular in design to avoid a group of claws 33 from abutting against the vertical plate 20.
[0024] During operation, one of the above technologies is applied to the tire maintenance device of the aviation industry. Although it is convenient to clean the tire surface, due to the heavy weight of the aviation industry tire itself and the limited space for the tire to move on the bottom plate, in the process of removing the tire from the storage shaft, it is necessary to avoid the tire from causing damage to other parts on the bottom plate, which inevitably requires more manpower. Through the structural design of the clamping mechanism, the function of facilitating the removal of the tire main body 21 from the storage shaft 22 is achieved. When the tire main body 21 placed on the storage shaft 22 is to be removed, the threaded rod 27 is first driven to rotate by the servo motor 28, and the first moving block 23 and the second moving block 25 threadedly connected to the threaded rod 27 will move in the same direction on the threaded rod 27. A push frame 24 is fixed on the top of the first moving block 23 and the push frame 24 is close to the tire main body 21. When the first moving block 23 moves, the push frame 24 will push the tire main body 21. The tire body 21 is moved along the bottom plate 1 until the tire body 21 is no longer inserted on the placement shaft 22. At the same time, the top of the second moving block 25 drives the support plate 30 to move on the bottom plate 1, and the two groups of support plates 30 are located directly below the tire body 21. When the tire body 21 is no longer inserted on the placement shaft 22, the tire body 21 will fall on the plane formed by the two groups of support plates 30 and the connecting plate 31 under the action of gravity, and the bottom end of the tire body 21 will push the claws 33 to rotate when falling, so that the two groups of claws 33 can grasp the left and right sides of the tire body 21, so as to clamp and fix the tire body 21, so as to facilitate the tire body 21 to be smoothly removed from the placement shaft 22, wherein the two groups of support plates 30 are connected together by the connecting plate 31, and multiple groups of pulleys 35 are fixed on the bottom ends of the support plates 30 to improve the bearing capacity of the support plates 30, and the through grooves 36 are connected to the inside of the cavity 26.
[0025] Furthermore, the first moving block 23 and the second moving block 25 are both welded and fixed with a limit block 40 on both the front and rear sides. The limit block 40 is designed in a rectangular shape. The limit block 40 is slidably connected to the inside of the limit groove 39. The limit groove 39 is designed in a long rectangular shape and its size is adapted to the limit block 40. The limit groove 39 is provided on the inner wall of the through groove 36.
[0026] During operation, through the structural design of the limit groove 39 and the limit block 40, the guiding function of the first moving block 23 and the second moving block 25 when moving on the threaded rod 27 is realized, so as to ensure that the first moving block 23 and the second moving block 25 can move stably on the threaded rod 27, and through the contact between the limit block 40 and the inner wall of the limit groove 39, the bearing capacity of the support plate 30 can also be improved.
[0027] Furthermore, a pad 38 is glued and fixed on the right side of the inner wall of the through groove 36, and the pad 38 is made of rubber;
[0028] During operation, the cushion block 38 is made of rubber material and is used to buffer the second moving block 25 and the inner wall of the through slot 36 to avoid abutment between the second moving block 25 and the through slot 36 .
[0029] Furthermore, a fixing groove 42 is provided on one side of the top of the push frame 24 close to the tire body 21, and the fixing groove 42 is designed in an arc shape;
[0030] During operation, the fixing groove 42 is designed to be arc-shaped, so that the fixing groove 42 can better fit with the left side of the tire body 21 , and the fixing groove 42 is in contact with the tire body 21 .
[0031] Furthermore, a step 44 is provided on the claw 33, and the step 44 is rectangular in design. A rubber plate 43 is glued and fixed on the step 44, and the size of the rubber plate 43 is consistent with that of the step 44;
[0032] During operation, the rubber plate 43 is used to increase the friction between the two groups of claws 33 and the tire body 21 , so that the claws 33 can better clamp the tire body 21 .
[0033] Furthermore, a plurality of drainage holes 41 are provided on the bottom end of the inner wall of the cavity 26, and the drainage holes 41 are connected to the outside;
[0034] During operation, the drain hole 41 is connected to the outside to drain the cleaning water flowing into the cavity 26 .
[0035] Working principle: One of the above technologies is used in a tire maintenance device for the aviation industry. Although it is convenient for cleaning the tire surface, due to the heavy weight of the aviation industry tire itself and the limited space on the bottom plate for the tire to move, in the process of removing the tire from the storage shaft, it is necessary to avoid the tire from causing damage to other parts on the bottom plate, which inevitably requires more manpower. Through the structural design of the clamping mechanism, the function of facilitating the removal of the tire body 21 from the storage shaft 22 is achieved. When the tire body 21 placed on the storage shaft 22 is to be removed, the threaded rod 27 is first driven to rotate by the servo motor 28, and the first moving block 23 and the second moving block 25 threadedly connected to the threaded rod 27 will move in the same direction on the threaded rod 27. A push frame 24 is fixed on the top of the first moving block 23 and the push frame 24 is close to the tire body 21. When the first moving block 23 moves, the push frame 24 will push the tire The tire body 21 is moved along the bottom plate 1 until the tire body 21 is no longer inserted on the placement shaft 22. At the same time, the top of the second moving block 25 drives the support plate 30 to move on the bottom plate 1, and the two groups of support plates 30 are located directly below the tire body 21. When the tire body 21 is no longer inserted on the placement shaft 22, the tire body 21 will fall on the plane formed by the two groups of support plates 30 and the connecting plate 31 under the action of gravity, and the bottom end of the tire body 21 will push the claws 33 to rotate when falling, so that the two groups of claws 33 can grasp the left and right sides of the tire body 21, so as to clamp and fix the tire body 21, so as to facilitate the tire body 21 to be smoothly removed from the placement shaft 22, wherein the two groups of support plates 30 are connected together by the connecting plate 31, and multiple groups of pulleys 35 are fixed on the bottom ends of the support plates 30 to improve the bearing capacity of the support plates 30, and the through grooves 36 are connected to the inside of the cavity 26.
[0036] The above description is only a preferred embodiment of the utility model and is not intended to limit the utility model. Although the utility model is described in detail with reference to the above embodiments, those skilled in the art can still modify the technical solutions recorded in the above embodiments or replace some of the technical features therein by equivalents. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the utility model shall be included in the protection scope of the utility model.
Claims
1. An aircraft tire maintenance device, comprising a base plate (1), a vertical plate (20), a tire body (21) and a storage shaft (22); characterized in that: The bottom plate (1) is provided with a clamping mechanism, the clamping mechanism comprising two groups of claws (33), the claws (33) being located directly below the tire body (21), the bottom ends of the claws (33) being rotatably connected to the grooves (32), the grooves (32) being provided on the support plate (30), the bottom ends of the support plates (30) being fixedly connected to a plurality of groups of pulleys (35), the pulleys (35) being slidably connected to the slide grooves (37), a connecting plate (31) being fixedly connected to one side of the support plate (30), a group of the bottom ends of the support plates (30) being fixedly connected to the second moving blocks (25 ), the second moving block (25) is arranged inside the cavity (26), the cavity (26) is opened inside the bottom plate (1), the first moving block (23) and the second moving block (25) are threadedly connected to the cavity (26), the top of the first moving block (23) is fixedly connected to the push frame (24), the bottom plate (1) is provided with a through groove (36) and a slide groove (37), the left inner wall of the cavity (26) is rotatably connected to a threaded rod (27), the right side of the cavity (26) is fixedly connected to a servo motor (28), and the vertical plate (20) is provided with a notch (34).
2. The aircraft tire maintenance device according to claim 1, characterized in that: The first moving block (23) and the second moving block (25) are both fixedly connected to limiting blocks (40) on both the front and rear sides. The limiting blocks (40) are slidably connected inside the limiting groove (39). The limiting groove (39) is provided on the inner wall of the through groove (36).
3. The aircraft tire maintenance device according to claim 2, characterized in that: A cushion block (38) is fixedly connected to the right side of the inner wall of the through slot (36), and the cushion block (38) is made of rubber material.
4. The aircraft tire maintenance device according to claim 3, characterized in that: A fixing groove (42) is provided on one side of the top end of the push frame (24) close to the tire body (21), and the fixing groove (42) is designed to be arc-shaped.
5. The aircraft tire maintenance device according to claim 4, characterized in that: The claw (33) is provided with a step (44), and a rubber plate (43) is fixedly connected to the step (44).
6. The aircraft tire maintenance device according to claim 5, characterized in that: A plurality of drainage holes (41) are provided on the bottom end of the inner wall of the cavity (26), and the drainage holes (41) are connected to the outside.
Citation Information
Patent Citations
Tire maintenance device applied to aviation industry
CN218890906U