Brake assembly dismounting device with cleaning function

Abstract

The application discloses a brake assembly dismounting equipment with a cleaning function, and relates to the technical field of aircraft brake disc dismounting. The equipment integrates the functions of dismounting, lifting and cleaning, can synchronously complete the dismounting and cleaning of the aircraft brake disc, significantly improves the maintenance efficiency, reduces the operation time and cost, and is suitable for the dismounting requirements of brake discs and tires of different models through the adjustable dismounting assembly and the lifting assembly, so that the universality and operation safety are improved. The cleaning assembly cooperates with the rotating assembly to realize omnibearing automatic cleaning, effectively removes dust and chippings, and avoids secondary pollution.

Description

TECHNICAL FIELD

[0001] The application relates to the technical field of dismounting of airplane brake discs, and particularly relates to a brake assembly dismounting device with a cleaning function. BACKGROUND

[0002] The airplane brake disc is an important safety component of an airplane, and the performance thereof is directly related to the take-off and landing safety of the airplane. In the long-term use of the airplane, the brake disc will be worn, stained with dust and chippings, and the like, so that the brake disc needs to be dismounted, cleaned, inspected and maintained regularly.

[0003] However, the traditional brake assembly dismounting device has a single function, and often only has the dismounting function, so that the brake disc cannot be cleaned synchronously in the dismounting process, and the brake disc after dismounting needs an additional cleaning process, thereby increasing the maintenance time and cost.

[0004] In addition, the traditional device is difficult to adapt to the dismounting requirements of brake discs and tires of different types of airplanes, and when facing diversified airplane types, the dismounting efficiency is low, and even the brake disc and the tire can be damaged due to improper operation. In addition, the traditional device is not flexible in moving and positioning, and cannot quickly and accurately reach the dismounting position of the airplane brake assembly, thereby affecting the overall working efficiency. SUMMARY

[0005] The application aims to provide a brake assembly dismounting device with a cleaning function to solve the problems in the prior art.

[0006] To achieve the above-mentioned purpose, the application provides the following technical scheme: a brake assembly dismounting device with a cleaning function, comprising a dismounting device main body and a controller, wherein the dismounting device main body comprises a support table, a moving assembly is installed at the bottom of the support table, a fixing table is installed on the support table, a dismounting assembly is installed on the fixing table, a lifting assembly is installed on the support table, and a cleaning assembly is installed between the lifting assemblies.

[0007] The moving assembly can drive the dismounting device main body to move.

[0008] The dismounting assembly can dismount the airplane tire.

[0009] The lifting assembly can lift the airplane brake disc.

[0010] The cleaning assembly can clean the dust and chippings on the airplane brake disc.

[0011] Further, the fixing table is provided with a limiting hole, and a dismounting assembly is arranged in the limiting hole, the dismounting assembly comprises an adjusting motor and a limiting plate, the limiting plate is arranged in a limiting groove, the adjusting motor is arranged on the other side of the fixing table, the output end of the adjusting motor is connected with the limiting plate, a sliding groove is arranged on the side of the limiting plate away from the adjusting motor, a dismounting motor is arranged on the other side of the limiting plate, two groups of limiting grooves are arranged on the side of the limiting plate connected with the dismounting motor, two groups of sliding blocks are arranged on the output end shell of the dismounting motor, and the sliding blocks are slidably connected with the limiting grooves.

[0012] Further, the sliding groove is internally provided with an adjusting cylinder and a bearing, the bearing is slidably arranged in the sliding groove, the adjusting cylinder is fixedly arranged in the sliding groove, the output end of the adjusting cylinder is connected with the bearing, and a dismounting device is arranged between the bearings.

[0013] Further, when the adjusting cylinder works, the position of the bearing can be adjusted, and the position of the dismounting motor and the dismounting device is indirectly adjusted.

[0014] When the dismounting motor rotates, the dismounting device can be driven to rotate, and the nut on the aircraft tire can be dismounted.

[0015] Further, the supporting table is provided with a driving groove and two groups of limiting grooves, the driving groove is located between the two groups of limiting grooves, an adjusting motor is arranged in the supporting table, an adjusting screw rod is arranged on the output end of the adjusting motor, the adjusting screw rod is arranged in the driving groove, and the lifting assembly is arranged above the two groups of limiting grooves.

[0016] Further, the lifting assembly comprises a bearing table, a plurality of lifting cylinders are arranged on the bearing table, a supporting frame is arranged on the output end of the plurality of lifting cylinders, a cleaning assembly, a rotating assembly and a bearing plate are arranged between the supporting frames, the bearing plate is arc-shaped, a plurality of rollers are arranged on the bearing plate, a groove is arranged on the bearing plate, the output end of the rotating assembly is located between the grooves, and the rotating assembly can drive the aircraft brake pad to rotate.

[0017] Further, the cleaning assembly comprises a recycling bin and two groups of air suction pumps, the air suction end of the air suction pump is arranged between the grooves, and the air exhaust end of the air suction pump is connected with the recycling bin.

[0018] Further, the rotating assembly comprises a rotating motor and a plurality of rotating wheels, the plurality of rotating wheels are respectively arranged at the bottom of the bearing plate through bearings, a belt pulley is arranged on the same end of the plurality of rotating wheels, a belt pulley is also arranged on the output end of the rotating motor, a belt is arranged between the two groups of belt pulleys, and a rubber layer is arranged on the side of the rotating wheel in contact with the aircraft brake disc.

[0019] Further, the moving assembly comprises a plurality of universal wheels, and the plurality of universal wheels are respectively installed at four corners of the fixed table.

[0020] Further, the controller is installed on one side of the dismounting device body, the controller is connected with the dismounting device body through wires, and the controller is provided with a control panel.

[0021] Compared with the prior art, the present application has the following beneficial effects:

[0022] 1. The device integrates dismounting, lifting and cleaning functions, can synchronously complete dismounting and cleaning of the airplane brake disc, significantly improves the maintenance efficiency, reduces the operation time and cost, adjusts the dismounting assembly and the lifting assembly, adapts to the dismounting requirements of different types of brake discs and tires, improves the universality and operation safety, the cleaning assembly cooperates with the rotating assembly to realize omnibearing automatic cleaning, effectively removes dust and debris, avoids secondary pollution, the moving assembly is flexible and convenient, is convenient for quick positioning and moving, the overall structure is reasonable, operation is simple, and the device is suitable for efficient maintenance of the airplane brake system.

[0023] 2. When the dismounting assembly is used, the operator first starts the adjusting motor through the controller, the adjusting motor drives the limiting plate to move in the limiting hole, so that the position of the dismounting assembly is adjusted, the dismounting position of the airplane tire is accurately aligned, the sliding groove and the sliding block on the limiting plate are matched, the stability and accuracy of the dismounting motor movement are ensured, when the limiting plate moves to the appropriate position, the dismounting motor is started, the output end of the dismounting motor starts to rotate, the airplane tire is dismounted from the airplane by using a specific dismounting tool, in the dismounting process, the sliding block slides in the limiting groove, so that the dismounting motor does not deviate when rotating, the smooth progress of the dismounting work is ensured, at the same time, the operator needs to closely observe the dismounting condition, adjusts the adjusting motor and the dismounting motor through the controller according to the actual condition, so as to adapt to the dismounting requirements of different types of airplane tires, after the dismounting is completed, the dismounted airplane tire is properly placed, and subsequent cleaning and maintenance work is prepared.

[0024] 3、The lifting assembly can lift the aircraft tires and brake discs, and assist in disassembly. Specifically, the operator first operates the controller to start the lifting cylinder, the output ends of the multiple lifting cylinders are synchronously extended upwards, the supporting frame is pushed upwards, since the supporting frame is provided with the cleaning assembly, the rotating assembly and the bearing plate, these components will ascend together with the supporting frame, the arc-shaped design of the bearing plate can better fit the shape of the aircraft brake disc, during the ascending process, the rollers on the bearing plate will first contact the aircraft brake disc, thereby playing the roles of buffering and supporting, avoiding the hard collision of the bearing plate on the brake disc, when the bearing plate is lifted to closely fit the aircraft brake disc, whether the brake disc is disassembled or not can be determined according to the use condition of the brake disc, then the rotating assembly starts to work, the output end of the rotating assembly is located between the slots, and can directly act on the aircraft brake disc to drive the brake disc to slowly rotate, during the rotating process, the cleaning assembly continuously cleans the brake disc to timely remove the dust and debris on the surface of the brake disc. BRIEF DESCRIPTION OF DRAWINGS

[0025] Figure 1 It is a structural schematic diagram of the whole application;

[0026] Figure 2 It is a structural schematic diagram of the plane of the application;

[0027] Figure 3 It is a structural schematic diagram of the part of the application;

[0028] Figure 4 It is a structural schematic diagram of the part of the lifting assembly of the application;

[0029] Figure 5 It is a connection structure schematic diagram of the limiting plate and the disassembly motor of the application;

[0030] Figure 6 It is an enlarged schematic diagram of "A" in the application; Figure 1

[0031] Figure 7 It is an enlarged schematic diagram of "B" in the application. Figure 4

[0032] In the figure: 1, disassembly equipment main body; 11, supporting table; 12, fixed table; 121, limiting hole; 13, adjusting motor; 131, adjusting screw; 2, moving assembly; 21, universal wheel; 3, disassembly assembly; 31, adjusting motor; 32, limiting plate; 33, disassembly motor; 34, adjusting cylinder; 35, bearing; 36, disassembler; 4, lifting assembly; 41, bearing table; 42, lifting cylinder; 43, supporting frame; 44, bearing plate; 5, cleaning assembly; 51, recovery bin; 52, air suction pump; 6, rotating assembly; 61, rotating motor; 62, rotating wheel; 7, controller. DETAILED DESCRIPTION​​

[0033] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0034] Example: Figures 1-7 As shown, the present invention provides a technical solution for a brake component disassembly device with cleaning function, including a disassembly device body 1 and a controller 7. The disassembly device body 1 includes a support platform 11, a movable component 2 installed at the bottom of the support platform 11, a fixed platform 12 installed on the support platform 11, a disassembly component 3 installed on the fixed platform 12, a lifting component 4 installed on the support platform 11, and a cleaning component 5 installed between the lifting components 4.

[0035] The movable component 2 can drive the disassembly device body 1 to move;

[0036] Disassembly component 3 enables the removal of aircraft tires;

[0037] Lifting assembly 4 can lift the aircraft brake disc;

[0038] Cleaning component 5 can clean dust and debris from aircraft brake discs;

[0039] Therefore, when using this device, the main body 1 of the disassembly equipment can first be moved to a suitable position next to the aircraft tire using the moving component 2. Then, the disassembly component 3 is activated by the controller 7 to remove the aircraft tire from the aircraft. Afterward, the lifting component 4 is controlled by the controller 7 to start working. The lifting component 4 slowly raises the aircraft brake disc to a height that is easy to clean and further operate. During the lifting process, it is important to ensure that the brake disc is stable to avoid shaking or tilting that could damage the brake disc. At this time, the rotating component 6 can drive the aircraft brake disc, and at the same time, the cleaning component 5 begins to clean the brake disc from all directions. The cleaning component 5 can quickly suck up the dust and debris on the surface of the brake disc to prevent them from adhering to the brake disc again. Meanwhile, the rotation speed of the rotating component 6 can be adjusted according to the cleaning needs. The device allows for flexible adjustments. When encountering difficult-to-clean areas, the rotating component 6 will appropriately reduce its speed, allowing the cleaning component 5 more time and force to clean. Conversely, when cleaning easier areas, the rotating component 6 will increase its speed to accelerate the cleaning process. This ensures both cleaning effectiveness and improved work efficiency. As the rotating component 6 continuously drives the aircraft brake disc to rotate, the cleaning component 5 continuously cleans, gradually removing dust and debris from the aircraft brake disc. The entire cleaning process is efficient and precise, laying a solid foundation for subsequent maintenance and upkeep of the aircraft brake disc. After cleaning, operators can further inspect and adjust the brake disc as needed. After disassembling the aircraft brake disc, a new aircraft brake disc can also be installed using this device.

[0040] like Figure 1 , Figure 3 and Figures 5-6 As shown in this embodiment, specifically, a limiting hole 121 is provided on the fixed platform 12, and a disassembly assembly 3 is installed in the limiting hole 121. The disassembly assembly 3 includes an adjusting motor 31 and a limiting plate 32. The limiting plate 32 is installed inside the limiting groove. The adjusting motor 31 is installed on the other side of the fixed platform 12. The output end of the adjusting motor 31 is connected to the limiting plate 32. A sliding groove is provided on the side of the limiting plate 32 away from the adjusting motor 31. A disassembly motor 33 is installed on the other side of the limiting plate 32. Two sets of limiting grooves are provided on the side of the limiting plate 32 connected to the disassembly motor 33. Two sets of sliders are installed on the outer shell of the output end of the disassembly motor 33. The sliders are slidably connected to the limiting groove.

[0041] When using the disassembly assembly 3, the operator first starts the adjustment motor 31 via the controller 7. The adjustment motor 31 drives the limiting plate 32 to move within the limiting hole 121, thereby adjusting the position of the disassembly assembly 3 to accurately align it with the disassembly part of the aircraft tire. The sliding groove and slider on the limiting plate 32 cooperate to ensure the stability and accuracy of the movement of the disassembly motor 33. After the limiting plate 32 moves to the appropriate position, the disassembly motor 33 is started, and the output end of the disassembly motor 33 begins to rotate. Using a specific disassembly tool, the aircraft tire is removed from the aircraft. During the disassembly process, the slider slides within the limiting groove to ensure that the disassembly motor 33 does not deviate when rotating, ensuring the smooth progress of the disassembly work. At the same time, the operator should closely observe the disassembly situation and make fine adjustments to the adjustment motor 31 and the disassembly motor 33 via the controller 7 according to the actual situation to adapt to the disassembly requirements of different models of aircraft tires. After the disassembly is completed, the disassembled aircraft tire is properly placed in preparation for subsequent cleaning and maintenance work.

[0042] like Figures 5-6 As shown, in this embodiment, specifically, an adjusting cylinder 34 and a bearing 35 are installed inside the slide groove. The bearing 35 is slidably installed inside the slide groove, and the adjusting cylinder 34 is fixedly installed inside the slide groove. The output end of the adjusting cylinder 34 is connected to the bearing 35. A disassembly device 36 is installed between the bearings 35, and the output end of the disassembly motor 33 is connected to the disassembly device 36.

[0043] This device is applicable to different aircraft models when removing aircraft tires. During tire removal, the position of the tire remover 36 can be adjusted to match different tire sizes. In practice, the operator first activates the adjusting cylinder 34 via the controller 7, based on the aircraft tire's model and size. The output of the adjusting cylinder 34 pushes the bearing 35 to slide within a groove. Since the tire remover 36 is installed between the bearings 35, the sliding of the bearings 35 moves the tire remover 36, thus adjusting its position. During adjustment, the operator must carefully observe the relative position of the tire remover 36 to ensure it is accurately aligned with the tire's removal area. Once the tire remover 36 is adjusted to the appropriate position, the tire removal motor 33 is activated. The output of the motor 33 drives the tire remover 36 to rotate, allowing the tire to be removed from the aircraft. Simultaneously, the lifting assembly 4 supports the tire and assists in separating it from the coupling.

[0044] like Figure 1 As shown, in this embodiment, specifically, when the cylinder 34 is working, it can adjust the position of the bearing 35, thereby indirectly adjusting the positions of the disassembly motor 33 and the disassembly device 36.

[0045] When the disassembly motor 33 rotates, it can drive the disassembly tool 36 to rotate, thereby removing the nuts on the aircraft tires.

[0046] When the adjusting cylinder 34 is working, the operator can precisely control the extension and retraction of the output end of the adjusting cylinder 34 through the controller 7. The output end pushes the bearing 35 to slide smoothly along the slide groove. Because the bearing 35 is connected to the disassembly device 36, it can indirectly drive the disassembly device 36 and the disassembly motor 33 connected to it to move to the designated position to adapt to the disassembly requirements of different aircraft tires. During the adjustment process, the sliding condition of the bearing 35 should be monitored at all times to ensure that it slides smoothly in the slide groove and avoid jamming or deviating from the track.

[0047] When the disassembly motor 33 rotates, its output end transmits power to the disassembly device 36. The disassembly device 36 rotates rapidly and, using its special structure and shape, tightly grips the nut on the aircraft tire. As the disassembly device 36 continues to rotate, the nut gradually loosens and is eventually removed from the tire.

[0048] like Figures 1-3 As shown, in this embodiment, specifically, the support platform 11 is provided with a drive groove and two sets of limiting grooves. The drive groove is located between the two sets of limiting grooves. An adjustment motor 13 is installed inside the support platform 11. An adjustment screw 131 is installed at the output end of the adjustment motor 13. The adjustment screw 131 is installed inside the drive groove. A lifting assembly 4 is installed above the drive groove and the two sets of limiting grooves.

[0049] The lifting assembly 4 of this device can move on the support platform 11 during use to facilitate the disassembly of aircraft tires and brake discs. Specifically, the operator first starts the adjusting motor 13 via the controller 7. The output of the adjusting motor 13 drives the adjusting screw 131 to rotate within the drive groove. Since the adjusting screw 131 is connected to the lifting assembly 4, its rotation causes the lifting assembly 4 to move along the drive groove. Simultaneously, the limiting groove limits and guides the lifting assembly 4, ensuring its stability during movement and preventing deviation or wobbling. When moving the lifting assembly 4, the operator needs to adjust the position of the aircraft tires and brake discs according to the situation. The position of the disc is precisely controlled by adjusting the rotation direction and number of revolutions of the motor 13, so that the lifting assembly 4 is accurately moved to the appropriate position. When the lifting assembly 4 moves to the bottom of the aircraft brake disc, the controller 7 is operated again to start the lifting assembly 4 to slowly raise the aircraft brake disc to a height that is easy to clean and further operate. During the raising process, the condition of the brake disc must be observed in real time to ensure that it rises smoothly and avoids damage to the brake disc due to excessive or uneven lifting speed. When the brake disc is raised to the predetermined height, the lifting assembly 4 stops rising and remains stable. At this time, the cleaning assembly 5 and the rotating assembly 6 begin to work together to clean the brake disc.

[0050] like Figures 1-4 and Figure 7As shown, in this embodiment, specifically, the lifting assembly 4 includes a support platform 41, on which multiple sets of lifting cylinders 42 are installed. Support frames 43 are installed at the output ends of the multiple sets of lifting cylinders 42. A cleaning assembly 5, a rotating assembly 6, and a bearing plate 44 are installed between the support frames 43. The bearing plate 44 is arc-shaped, and rollers are installed on the bearing plate 44. Slots are opened on the bearing plate 44. The output end of the rotating assembly 6 is located between the slots. The rotating assembly 6 can drive the aircraft brake pads to rotate.

[0051] The lifting assembly 4 can lift the aircraft tires and brake discs to assist in disassembly. In specific use, the operator first operates the controller 7 to start the lifting cylinder 42. The output ends of multiple lifting cylinders 42 extend upwards simultaneously, pushing the support frame 43 to move upwards. Since the support frame 43 is equipped with the cleaning assembly 5, the rotating assembly 6, and the bearing plate 44, these components will rise together with the support frame 43. The arc design of the bearing plate 44 can better fit the shape of the aircraft brake disc. During the rising process, the rollers on the bearing plate 44 will first contact the aircraft brake disc, playing a role in buffering and supporting, and avoiding the bearing plate 44 causing a hard collision with the brake disc. When the bearing plate 44 rises to fit tightly with the aircraft brake disc, the brake disc can be disassembled depending on its usage. Then the rotating assembly 6 starts to work. Its output end is located between the slots and can directly act on the aircraft brake disc, driving the brake disc to rotate slowly. During the rotation, the cleaning assembly 5 continuously cleans the brake disc, removing dust and debris from the surface of the brake disc in a timely manner.

[0052] like Figure 7 As shown, in this embodiment, specifically, the cleaning component 5 includes a recycling bin 51 and two sets of suction pumps 52. The suction end of the suction pump 52 is installed between the slots, and the exhaust end of the suction pump 52 is connected to the recycling bin 51.

[0053] The cleaning component 5 generates powerful suction through two sets of suction pumps 52 to suck up dust and debris from the surface of the aircraft brake disc. The suction end of the suction pump 52 is located between the slots, which can accurately approach the surface of the brake disc to maximize the suction of dust and debris. When the suction pump 52 is started, air carrying dust and debris enters from the suction end, and then is transported to the exhaust end through the pipe, and finally discharged into the recovery chamber 51. The recovery chamber 51 centrally stores the sucked-up dust and debris for convenient subsequent cleaning and processing.

[0054] like Figure 1 , Figure 4 and Figure 7As shown, in this embodiment, specifically, the rotating assembly 6 includes a rotating motor 61 and multiple sets of rotating wheels 62. The multiple sets of rotating wheels 62 are respectively mounted on the bottom of the support plate 44 through bearings 35. A pulley is installed at the same end of the multiple sets of rotating wheels 62. A pulley is also installed at the output end of the rotating motor 61. A belt is installed between the two sets of pulleys. A rubber layer is provided on the side of the rotating wheel 62 that contacts the aircraft brake disc.

[0055] When using the rotating component 6 of this device, the operator first starts the rotating motor 61 via the controller 7. The pulley at the output end of the rotating motor 61 begins to rotate, transmitting power to the pulleys at the same end of multiple rotating wheels 62 via a belt, thereby driving the multiple rotating wheels 62 to rotate synchronously. Since the side of the rotating wheel 62 that contacts the aircraft brake disc is provided with a rubber layer, the rubber layer has good friction and flexibility, which can tightly adhere to the aircraft brake disc when the rotating wheel 62 rotates, driving the brake disc to rotate smoothly. During the rotation of the brake disc, the cleaning component 5 works continuously, cleaning the dust and debris on the surface of the brake disc in a timely manner. At the same time, the operator can adjust the speed of the rotating motor 61 via the controller 7 according to the working condition of the cleaning component 5 and the cleanliness of the brake disc surface, thereby adjusting the rotation speed of the rotating wheel 62. When there is a lot of dust and stubborn debris on the surface of the brake disc, the rotation speed is reduced to allow the cleaning component 5 more time to clean. When the surface of the brake disc is relatively clean, the rotation speed is increased to speed up the cleaning process.

[0056] like Figures 1-2 As shown, in this embodiment, specifically, the moving component 2 includes multiple sets of casters 21, which are respectively installed at the four corners of the fixed platform 12;

[0057] The moving component 2 can move the entire support platform 11. The operator can push the entire support platform 11 with the handle to move the device to the appropriate position so as to disassemble the aircraft tires and brake discs.

[0058] like Figure 1 As shown, in this embodiment, specifically, the controller 7 is installed on one side of the disassembly equipment body 1, the controller 7 is connected to the disassembly equipment body 1 through a wire, and the controller 7 is equipped with a control panel;

[0059] Because the controller 7 of the device is connected to the main body 1 of the disassembly equipment, it can precisely control each component of the equipment. The operator can easily start or stop the moving component 2, disassembly component 3, lifting component 4, cleaning component 5 and rotating component 6 through the control panel on the controller 7. There are different buttons and adjustment knobs on the control panel, which correspond to the operation of each component.

[0060] Working Principle: When using this device, the moving component 2 first moves the main body 1 of the disassembly equipment to a suitable position next to the aircraft tire. The controller 7 then activates the disassembly component 3 to remove the aircraft tire from the aircraft. Afterwards, the controller 7 controls the lifting component 4 to begin operation. The lifting component 4 slowly raises the aircraft brake disc to a height suitable for cleaning and further operation. During the raising process, it is crucial to ensure the brake disc remains stable to avoid shaking or tilting that could damage it. At this time, the rotating component 6 drives the aircraft brake disc, while the cleaning component 5 begins a comprehensive cleaning of the brake disc. The cleaning component 5 quickly removes dust and debris from the surface of the brake disc, preventing them from re-adhering. Simultaneously, the rotation speed of the rotating component 6 can be adjusted according to the cleaning speed. The rotation speed of the rotating component 6 is flexibly adjusted to meet the needs of cleaning. When encountering difficult-to-clean areas, the rotation speed of the rotating component 6 will be reduced appropriately, allowing the cleaning component 5 more time and force to clean. When cleaning easier areas, the rotation speed of the rotating component 6 will be increased to speed up the cleaning process. This ensures both cleaning effectiveness and work efficiency. As the rotating component 6 continues to drive the aircraft brake disc to rotate, the cleaning component 5 continuously cleans, gradually removing dust and debris from the aircraft brake disc. The entire cleaning process is efficient and precise, laying a good foundation for the subsequent maintenance and upkeep of the aircraft brake disc. After cleaning, the operator can further inspect and adjust the brake disc as needed. After the aircraft brake disc is disassembled, a new aircraft brake disc can also be installed using this device.

[0061] It will be apparent to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the invention can be implemented in other specific forms without departing from its spirit or essential characteristics. Therefore, the embodiments should be considered in all respects as exemplary and non-limiting, and the scope of the invention is defined by the appended claims rather than the foregoing description. Thus, all variations falling within the meaning and scope of equivalents of the claims are intended to be included within the present invention. No reference numerals in the claims should be construed as limiting the scope of the claims.

Claims

1. A brake assembly disassembly device with a cleaning function, comprising a disassembly device body (1) and a controller (7), characterized in that: The main body (1) of the disassembly equipment includes a support platform (11), a moving component (2) is installed at the bottom of the support platform (11), a fixed platform (12) is installed on the support platform (11), a disassembly component (3) is installed on the fixed platform (12), a lifting component (4) is installed on the support platform (11), and a cleaning component (5) is installed between the lifting components (4). The moving component (2) is capable of driving the disassembly device body (1) to move; The disassembly assembly (3) is capable of removing the aircraft tires; The lifting assembly (4) is capable of lifting the aircraft brake disc; The cleaning component (5) can clean dust and debris from the aircraft brake disc; The fixed platform (12) has a limiting hole (121) and a disassembly assembly (3) is installed in the limiting hole (121). The disassembly assembly (3) includes an adjusting motor (31) and a limiting plate (32). The limiting plate (32) is installed inside the limiting groove. The adjusting motor (31) is installed on the other side of the fixed platform (12). The output end of the adjusting motor (31) is connected to the limiting plate (32). A sliding groove is provided on the side of the limiting plate (32) away from the adjusting motor (31). A disassembly motor (33) is installed on the other side of the limiting plate (32). Two sets of limiting grooves are provided on the side of the limiting plate (32) connected to the disassembly motor (33). Two sets of sliders are installed on the outer shell of the output end of the disassembly motor (33). The sliders are slidably connected to the limiting groove. An adjusting cylinder (34) and a bearing (35) are installed inside the slide groove. The bearing (35) is slidably installed inside the slide groove. The adjusting cylinder (34) is fixedly installed inside the slide groove. The output end of the adjusting cylinder (34) is connected to the bearing (35). A disassembly device (36) is installed between the bearings (35). The output end of the disassembly motor (33) is connected to the disassembly device (36).

2. The brake assembly disassembly device with cleaning function according to claim 1, characterized in that: When the adjusting cylinder (34) is working, it can adjust the position of the bearing (35) and indirectly adjust the position of the disassembly motor (33) and the disassembly device (36); When the disassembly motor (33) rotates, it can drive the disassembly device (36) to rotate and disassemble the nuts on the aircraft tires.

3. The brake assembly disassembly device with cleaning function according to claim 2, characterized in that: The support platform (11) is provided with a drive groove and two sets of limiting grooves. The drive groove is located between the two sets of limiting grooves. An adjustment motor (13) is installed inside the support platform (11). An adjustment screw (131) is installed at the output end of the adjustment motor (13). The adjustment screw (131) is installed inside the drive groove. The lifting assembly (4) is installed above the drive groove and the two sets of limiting grooves.

4. A brake assembly disassembly device with cleaning function according to claim 3, characterized in that: The lifting assembly (4) includes a support platform (41), on which multiple sets of lifting cylinders (42) are installed. Support frames (43) are installed at the output ends of the multiple sets of lifting cylinders (42). A cleaning assembly (5), a rotating assembly (6), and a bearing plate (44) are installed between the support frames (43). The bearing plate (44) is arc-shaped and has rollers installed on it. The bearing plate (44) has slots. The output end of the rotating assembly (6) is located between the slots. The rotating assembly (6) can drive the aircraft brake pads to rotate.

5. A brake assembly disassembly device with cleaning function according to claim 4, characterized in that: The cleaning component (5) includes a recycling bin (51) and two sets of suction pumps (52). The suction end of the suction pump (52) is installed between the slots, and the exhaust end of the suction pump (52) is connected to the recycling bin (51).

6. A brake assembly disassembly device with a cleaning function according to claim 5, characterized in that: The rotating assembly (6) includes a rotating motor (61) and multiple sets of rotating wheels (62). The multiple sets of rotating wheels (62) are respectively mounted on the bottom of the support plate (44) via bearings (35). A pulley is installed at the same end of the multiple sets of rotating wheels (62). A pulley is also installed at the output end of the rotating motor (61). A belt is installed between the two sets of pulleys. A rubber layer is provided on the side of the rotating wheel (62) that contacts the aircraft brake disc.

7. A brake assembly disassembly device with a cleaning function according to claim 6, characterized in that: The moving component (2) includes multiple sets of casters (21), which are respectively installed at the four corners of the fixed platform (12).

8. A brake assembly disassembly device with cleaning function according to claim 7, characterized in that: The controller (7) is installed on one side of the disassembly equipment body (1). The controller (7) is connected to the disassembly equipment body (1) via a wire. The controller (7) is equipped with a control panel.

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