Dynamic balance correcting machine for aircraft tire

Abstract

The utility model relates to the technical field of dynamic balance correction, in particular to an aircraft tire dynamic balance correction machine which facilitates auxiliary feeding of tires with different diameters, reduces physical output and improves convenience. Comprising a detection mechanism; the device further comprises a transverse adjusting mechanism, a transverse driving mechanism, a lifting mechanism, a lifting driving mechanism and a limiting mechanism, the transverse adjusting mechanism is installed on the detection mechanism, the transverse driving mechanism is installed on the transverse adjusting mechanism, the lifting mechanism is installed on the transverse adjusting mechanism, the lifting driving mechanism is installed on the lifting mechanism, and the limiting mechanism is installed on the lifting mechanism. The tire is conveniently driven to rotate and the dynamic balance of the tire is conveniently detected through the detection mechanism, the transverse driving mechanism drives the transverse adjusting mechanism to adjust the transverse position of the tire, the lifting driving mechanism drives the lifting mechanism to adjust the height of the tire, and the limiting mechanism limits the tires with different diameters.

Description

Technical Field

[0001] This utility model relates to the technical field of dynamic balance correction, and in particular to a dynamic balance correction machine for aircraft tires. Background Technology

[0002] Dynamic equilibrium refers to the relatively stable equilibrium state maintained among the various elements within a material system under continuous motion and change. This equilibrium is dynamic, meaning that the interactions and changes between the elements are ongoing, but the system as a whole maintains a stable state. To improve the operational stability of aircraft tires, dynamic balance testing is necessary.

[0003] Existing dynamic balancing correction technologies, such as the prior art with application number CN202121700103.0, include a frame, worktable, moving device, connecting shaft, connecting plate, pneumatic gripper, gripping arm, drive cylinder, rubber block, drive assembly, cylinder one and rack, etc. By setting pulleys that are slidably connected in the slide groove, the distance between multiple pulleys can be adjusted, thereby adjusting the tension of the belt.

[0004] However, existing technology is not convenient for testing the dynamic balance of aircraft tires of different diameters. Furthermore, when installing aircraft tires, larger aircraft tires are heavier, and existing technology is not convenient for assisting with loading, which reduces convenience. Utility Model Content

[0005] To solve the above-mentioned technical problems, this utility model provides an aircraft tire dynamic balancing correction machine that facilitates the feeding of tires of different diameters, reduces physical labor consumption, and improves convenience.

[0006] This utility model discloses a dynamic balancing machine for aircraft tires, including a detection mechanism; it also includes a lateral adjustment mechanism, a lateral drive mechanism, a lifting mechanism, a lifting drive mechanism, and a limiting mechanism. The lateral adjustment mechanism is mounted on the detection mechanism, the lateral drive mechanism is mounted on the lateral adjustment mechanism, the lifting mechanism is mounted on the lateral adjustment mechanism, the lifting drive mechanism is mounted on the lifting mechanism, and the limiting mechanism is mounted on the lifting mechanism. The detection mechanism facilitates tire rotation and dynamic balance detection. The lateral drive mechanism drives the lateral adjustment mechanism to adjust the lateral position of the tire, the lifting drive mechanism drives the lifting mechanism to adjust the height of the tire, and the limiting mechanism limits tires of different diameters. The detection mechanism facilitates tire rotation and dynamic balance detection, the lateral drive mechanism drives the lateral adjustment mechanism to adjust the lateral position of the tire, and the lifting drive mechanism drives the lifting mechanism to adjust the height of the tire. This assists the operator in mounting tires of different diameters onto the detection mechanism, reducing physical exertion and improving convenience. The limiting mechanism limits tires of different diameters.

[0007] Preferably, the detection mechanism includes a detector body, a rotating shaft, a first motor, a limiting plate, an auxiliary fixing block, and a threaded fixing plate. The rotating shaft is rotatably mounted on the detector body, the first motor is mounted on the outer wall of the detector body, and the output end of the first motor is connected to the rotating shaft. The limiting plate is mounted on the rotating shaft, the auxiliary fixing block is slidably mounted on the rotating shaft, and the outer end of the rotating shaft is threaded. The threaded fixing plate is mounted on the rotating shaft through a threaded connection. The tire rim is aligned with the rotating shaft, and then the rim is mounted on the rotating shaft. The rim is then limited and fixed by the limiting plate and the auxiliary fixing block. By rotating the threaded fixing plate, the auxiliary fixing block is fixed due to the threaded connection, thereby fixing the rim. The first motor is turned on to drive the rotating shaft to rotate, and the dynamic balance is detected by the detector body.

[0008] Preferably, the lateral adjustment mechanism includes a fixed plate and a sliding plate. The fixed plate is installed on the bottom end of the side wall of the detector body, and the sliding plate is slidably installed on the fixed plate. By opening the lateral drive mechanism, the sliding plate is driven to slide on the fixed plate, thereby adjusting the lateral position of the tire.

[0009] Preferably, the lateral drive mechanism includes a first lead screw, a guide rod, and a second motor. A threaded hole is provided in the fixed plate. One end of the first lead screw is rotatably mounted on the side wall of the sliding plate, and the first lead screw is threadedly engaged with the threaded hole in the fixed plate. One end of the guide rod is mounted on the side wall of the first lead screw, and the other end of the guide rod is slidably mounted inside the fixed plate. The second motor is mounted on the outer wall of the sliding plate, and the output end of the second motor is connected to the first lead screw. By turning on the second motor, the first lead screw is driven to rotate, and then the guide rod is driven to slide on the fixed plate through the threaded connection. The guide rod guides the sliding plate to slide on the fixed plate, thereby adjusting the lateral position of the tire.

[0010] Preferably, the lifting mechanism includes a sliding sleeve and a sliding block. The sliding sleeve is installed on the top of the sliding plate, and the sliding block is slidably installed inside the sliding sleeve. By opening the lifting drive mechanism, the sliding block is driven to slide inside the sliding sleeve, thereby adjusting the height of the tire, which facilitates dynamic balance testing of tires of different diameters.

[0011] Preferably, the lifting drive mechanism includes a second lead screw, two sliders, two connecting rods, and a third motor. A slide rail is provided inside the sliding housing. The second lead screw is rotatably mounted on the inner wall of the sliding housing and located within the slide rail. The two sliders are slidably mounted within the slide rail. The two ends of the second lead screw are provided with threads in opposite directions, and the two sliders engage with the threads in opposite directions on the second lead screw. One end of each connecting rod is rotatably mounted on the two sliders, and the other end is rotatably mounted on the top of the sliding block. The third motor is mounted on the outer wall of the sliding housing, and the output ends of the two third motors are connected to the second lead screw. By activating the third motor, the second lead screw is rotated, which in turn drives the sliders to slide within the slide rail via the threaded connection. This, in turn, drives the sliding block to slide within the sliding housing via the connecting rods, thereby adjusting the tire height and facilitating dynamic balancing tests on tires of different diameters.

[0012] Preferably, the limiting mechanism includes a limiting groove and two limiting rollers. The limiting groove is mounted on the sliding block, and the two limiting rollers are rotatably mounted in the limiting groove via a rotating shaft. The two rotating limiting rollers support and limit tires of different diameters.

[0013] Compared with the prior art, the beneficial effects of this utility model are as follows: the detection mechanism facilitates the rotation of the tire and the detection of the tire's dynamic balance; the lateral drive mechanism drives the lateral adjustment mechanism to adjust the lateral position of the tire; the lifting drive mechanism drives the lifting mechanism to adjust the height of the tire; it assists the operator in installing tires of different diameters on the detection mechanism, reducing physical exertion and improving convenience; and the limiting mechanism limits tires of different diameters. Attached Figure Description

[0014] Figure 1 This is a schematic diagram of the first isometric structure of this utility model;

[0015] Figure 2 This is a schematic diagram of the second isometric structure of this utility model;

[0016] Figure 3 This is a schematic diagram of the third isometric structure of this utility model;

[0017] Figure 4 This is a schematic diagram of the fourth isometric structure of this utility model;

[0018] Figure 5 This is a schematic diagram of the fifth isometric structure of this utility model;

[0019] Figure 6 This is a front view sectional isometric structural schematic diagram of this utility model;

[0020] Figure 7 This is a front cross-sectional structural diagram of the present invention;

[0021] The attached diagram is labeled as follows: 01, Detection mechanism; 11, Detector body; 12, Rotating shaft; 13, First motor; 14, Limiting plate; 15, Auxiliary fixing block; 16, Threaded fixing plate; 02, Lateral adjustment mechanism; 21, Fixing plate; 22, Sliding plate; 03, Lateral drive mechanism; 31, First lead screw; 32, Guide rod; 33, Second motor; 04, Lifting mechanism; 41, Sliding sleeve; 42, Sliding block; 05, Lifting drive mechanism; 51, Second lead screw; 52, Slider; 53, Connecting rod; 54, Third motor; 06, Limiting mechanism; 61, Limiting groove; 62, Limiting roller. Detailed Implementation

[0022] To facilitate understanding of this utility model, a more complete description will be given below with reference to the accompanying drawings. This utility model can be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided to make the disclosure of this utility model more thorough and complete.

[0023] Example 1

[0024] like Figures 1 to 7 As shown, an aircraft tire dynamic balancing correction machine includes a detection mechanism 01, a lateral adjustment mechanism 02, a lateral drive mechanism 03, a lifting mechanism 04, a lifting drive mechanism 05, and a limiting mechanism 06. The lateral adjustment mechanism 02 is installed on the detection mechanism 01, the lateral drive mechanism 03 is installed on the lateral adjustment mechanism 02, the lifting mechanism 04 is installed on the lateral adjustment mechanism 02, the lifting drive mechanism 05 is installed on the lifting mechanism 04, and the limiting mechanism 06 is installed on the lifting mechanism 04.

[0025] The detection mechanism 01 facilitates the rotation of the tire and the detection of the tire's dynamic balance. The lateral drive mechanism 03 drives the lateral adjustment mechanism 02 to adjust the lateral position of the tire. The lifting drive mechanism 05 drives the lifting mechanism 04 to adjust the height of the tire. The limiting mechanism 06 limits tires of different diameters.

[0026] The detection mechanism 01 includes a detector body 11, a rotating shaft 12, a first motor 13, a limiting plate 14, an auxiliary fixing block 15, and a threaded fixing plate 16. The rotating shaft 12 is rotatably mounted on the detector body 11. The first motor 13 is mounted on the outer wall of the detector body 11. The output end of the first motor 13 is connected to the rotating shaft 12. The limiting plate 14 is mounted on the rotating shaft 12. The auxiliary fixing block 15 is slidably mounted on the rotating shaft 12. The outer end of the rotating shaft 12 is provided with threads. The threaded fixing plate 16 is mounted on the rotating shaft 12 through a threaded relationship.

[0027] The lateral adjustment mechanism 02 includes a fixed plate 21 and a sliding plate 22. The fixed plate 21 is installed on the bottom end of the side wall of the detector body 11, and the sliding plate 22 is slidably installed on the fixed plate 21.

[0028] The transverse drive mechanism 03 includes a first lead screw 31, a guide rod 32, and a second motor 33. A threaded hole is provided in the fixed plate 21. One end of the first lead screw 31 is rotatably mounted on the side wall of the sliding plate 22. The first lead screw 31 is threadedly engaged with the threaded hole of the fixed plate 21. One end of the guide rod 32 is mounted on the side wall of the first lead screw 31, and the other end of the guide rod 32 is slidably mounted in the fixed plate 21. The second motor 33 is mounted on the outer wall of the sliding plate 22, and the output end of the second motor 33 is connected to the first lead screw 31.

[0029] Align the tire rim with the rotating shaft 12, then install the rim on the rotating shaft 12. The rim is then fixed by the limiting plate 14 and the auxiliary fixing block 15. By rotating the threaded fixing plate 16, the auxiliary fixing block 15 is fixed due to the threaded relationship, thereby fixing the rim. Turn on the first motor 13 to drive the rotating shaft 12 to rotate, and the dynamic balance is detected by the detector body 11. Turn on the second motor 33 to drive the first lead screw 31 to rotate, and then drive the guide rod 32 to slide on the fixed plate 21 through the threaded relationship. The guide rod 32 guides the sliding plate 22 to slide on the fixed plate 21, thereby adjusting the lateral position of the tire.

[0030] Example 2

[0031] like Figure 2 , Figure 3 and Figure 6 As shown, an aircraft tire dynamic balancing correction machine includes a detection mechanism 01, a lateral adjustment mechanism 02, a lateral drive mechanism 03, a lifting mechanism 04, a lifting drive mechanism 05, and a limiting mechanism 06. The lateral adjustment mechanism 02 is installed on the detection mechanism 01, the lateral drive mechanism 03 is installed on the lateral adjustment mechanism 02, the lifting mechanism 04 is installed on the lateral adjustment mechanism 02, the lifting drive mechanism 05 is installed on the lifting mechanism 04, and the limiting mechanism 06 is installed on the lifting mechanism 04.

[0032] The detection mechanism 01 facilitates the rotation of the tire and the detection of the tire's dynamic balance. The lateral drive mechanism 03 drives the lateral adjustment mechanism 02 to adjust the lateral position of the tire. The lifting drive mechanism 05 drives the lifting mechanism 04 to adjust the height of the tire. The limiting mechanism 06 limits tires of different diameters.

[0033] The lifting mechanism 04 includes a sliding sleeve 41 and a sliding block 42. The sliding sleeve 41 is installed on the top of the sliding plate 22, and the sliding block 42 is slidably installed inside the sliding sleeve 41.

[0034] The lifting drive mechanism 05 includes a second lead screw 51, two sliders 52, two connecting rods 53, and a third motor 54. The sliding sleeve 41 is provided with a slide rail. The second lead screw 51 is rotatably mounted on the inner wall of the sliding sleeve 41 and is located in the slide rail. The two sliders 52 are slidably mounted in the slide rail. The two ends of the second lead screw 51 are provided with threads in opposite directions. The two sliders 52 are engaged with the threads in two directions on the second lead screw 51. One end of the two connecting rods 53 is rotatably mounted on the two sliders 52, and the other end of the two connecting rods 53 is rotatably mounted on the top of the sliding block 42. The third motor 54 is mounted on the outer wall of the sliding sleeve 41, and the output ends of the two third motors 54 are connected to the second lead screw 51.

[0035] The limiting mechanism 06 includes a limiting groove 61 and two limiting rollers 62. The limiting groove 61 is mounted on the sliding block 42, and the two limiting rollers 62 are rotatably mounted in the limiting groove 61 via a rotating shaft.

[0036] By turning on the third motor 54, the second lead screw 51 is driven to rotate. Then, through the threaded connection, the slider 52 is driven to slide in the slide rail. Then, through the connecting rod 53, the sliding block 42 is driven to slide in the sliding sleeve 41, thereby adjusting the height of the tire. This facilitates dynamic balance testing of tires of different diameters. The two rotating limit rollers 62 support and limit the tires of different diameters.

[0037] like Figures 1 to 7 As shown, this utility model discloses a dynamic balancing machine for aircraft tires. During operation, the tire rim is aligned with the rotating shaft 12, and then the rim is mounted on the shaft 12. The rim is then fixed in place by a limiting plate 14 and an auxiliary fixing block 15. Rotating the threaded fixing plate 16, the threaded connection secures the auxiliary fixing block 15, thus fixing the rim. The first motor 13 is activated to rotate the rotating shaft 12, and the dynamic balance is detected by the detector body 11. The second motor 33 is activated to rotate the first lead screw 31, and the dynamic balance is then checked by the threaded connection. The guide rod 32 slides on the fixed plate 21, and the guide rod 32 guides the sliding plate 22 to slide on the fixed plate 21, thereby adjusting the lateral position of the tire. The third motor 54 drives the second lead screw 51 to rotate, and then the slider 52 slides in the slide rail through the threaded connection. Then, the connecting rod 53 drives the sliding block 42 to slide in the sliding sleeve 41, thereby adjusting the height of the tire. This facilitates dynamic balancing tests on tires of different diameters. The two rotating limit rollers 62 support and limit the tires of different diameters.

[0038] The detector body 11, the first motor 13, the second motor 33, and the third motor 54 of this utility model are commercially available. Technical personnel in this industry only need to install and operate them according to the accompanying instruction manual, without requiring any creative work from those skilled in the art.

[0039] The main function achieved by this utility model is to facilitate the feeding of tires of different diameters during the dynamic balance correction process, reduce physical labor consumption, and improve convenience.

[0040] The above description is only a preferred embodiment of the present utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the technical principles of the present utility model, and these improvements and modifications should also be considered within the protection scope of the present utility model.

Claims

1. An aircraft tire dynamic balancing correction machine comprising a detection mechanism (01); characterized by, Also include transverse adjustment mechanism (02), transverse drive mechanism (03), lifting mechanism (04), lifting drive mechanism (05) and limiting mechanism (06), transverse adjustment mechanism (02) is installed on the detection mechanism (01), transverse drive mechanism (03) is installed transverse adjustment mechanism (02) on, lifting mechanism (04) is installed on transverse adjustment mechanism (02), lifting drive mechanism (05) is installed on lifting mechanism (04), limiting mechanism (06) is installed lifting mechanism (04) on; The detection mechanism (01) facilitates the rotation of the tire and the detection of the dynamic balance of the tire, the transverse drive mechanism (03) drives the transverse adjustment mechanism (02) to adjust the transverse position of the tire, the lifting drive mechanism (05) drives the lifting mechanism (04) to adjust the height of the tire, and the limiting mechanism (06) limits the tire of different diameters.

2. An aircraft tire dynamic balancing machine as claimed in claim 1, wherein, The detection mechanism (01) includes a detector body (11), a rotating shaft (12), a first motor (13), a limiting disc (14), an auxiliary fixing block (15) and a threaded fixing disc (16), the rotating shaft (12) is rotatably installed on the detector body (11), the first motor (13) is installed on the outer wall of the detector body (11), the output end of the first motor (13) is connected with the rotating shaft (12), the limiting disc (14) is installed on the rotating shaft (12), the auxiliary fixing block (15) is slidably installed on the rotating shaft (12), the outer end of the rotating shaft (12) is provided with threads, and the threaded fixing disc (16) is installed on the rotating shaft (12) in threaded relationship.

3. An aircraft tire dynamic balancing machine as claimed in claim 2 wherein, The transverse adjustment mechanism (02) includes a fixed plate (21) and a sliding plate (22), the fixed plate (21) is installed on the bottom end of the side wall of the detector body (11), and the sliding plate (22) is slidably installed on the fixed plate (21).

4. An aircraft tire dynamic balancing machine as claimed in claim 3 wherein, The transverse drive mechanism (03) includes a first lead screw (31), a guide rod (32) and a second motor (33), the fixed plate (21) is provided with a threaded hole, one end of the first lead screw (31) is rotatably installed on the side wall of the sliding plate (22), the first lead screw (31) is in threaded cooperation with the threaded hole of the fixed plate (21), one end of the guide rod (32) is installed on the side wall of the first lead screw (31), the other end of the guide rod (32) is slidably installed in the fixed plate (21), and the second motor (33) is installed on the outer wall of the sliding plate (22), the output end of the second motor (33) is connected with the first lead screw (31).

5. An aircraft tire dynamic balancing machine as claimed in claim 3 wherein, The lifting mechanism (04) includes a sliding sleeve box (41) and a sliding block (42), the sliding sleeve box (41) is installed on the top end of the sliding plate (22), and the sliding block (42) is slidably installed in the sliding sleeve box (41).

6. An aircraft tire dynamic balancing machine as claimed in claim 5 wherein, The lifting driving mechanism (05) comprises a second screw rod (51), two sliding blocks (52), two connecting rods (53) and a third motor (54), the inside of the sliding sleeve box (41) is provided with a sliding channel, the second screw rod (51) is rotatably installed on the inner wall of the sliding sleeve box (41), the second screw rod (51) is located in the sliding channel, the two ends of the second screw rod (51) are provided with opposite threads, the two sliding blocks (52) are slidably installed on the second screw rod (51), the two sliding blocks (52) are matched with the two threads on the second screw rod (51), one end of the two connecting rods (53) is rotatably installed on the two sliding blocks (52), the other end of the two connecting rods (53) is rotatably installed on the top end of the sliding block (42), the third motor (54) is installed on the outer wall of the sliding sleeve box (41), and the output ends of the two third motors (54) are connected with the second screw rod (51).

7. An aircraft tire dynamic balancing machine as claimed in claim 5 wherein, The limiting mechanism (06) comprises a limiting groove (61) and two limiting rollers (62), the limiting groove (61) is installed on the sliding block (42), and the two limiting rollers (62) are rotatably installed in the limiting groove (61) through pivots.

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