Aviation part dismounting tool

Abstract

The utility model relates to the technical field of dismounting tools, in particular to an aviation part dismounting tool which comprises a dismounting operation table, a center supporting sleeve is fixedly installed at the center position of the upper surface of the dismounting operation table, a supporting rotary table is arranged above the center supporting sleeve, and a protruding column is fixedly installed at the center position of the bottom face of the supporting rotary table. A plurality of gear teeth are fixedly installed on the annular side face of the supporting rotary table, a driving motor is fixedly installed on the bottom face of the dismounting operation table, a gear is fixedly installed at the tail end of an output shaft of the driving motor, and the gear and the gear teeth are meshed with each other. A left clamping assembly and a right clamping assembly are fixedly installed on the upper surface of the dismounting operation table, each clamping assembly comprises a vertical beam fixedly installed on the dismounting operation table, an air cylinder is fixedly installed on each vertical beam, and a clamping protruding block is arranged on a telescopic shaft of each air cylinder. The clamping and orientation adjusting device facilitates clamping and orientation adjusting operation and is convenient to use.

Description

Technical Field

[0001] The utility model relates to the technical field of disassembly tooling, and particularly to an aviation component disassembly tooling. Background Technique

[0002] With the rapid development of the global aviation industry, aircraft manufacturing and maintenance technologies have increasingly become important indicators to measure a country's industrial strength. As an important link in the industrial chain, aircraft maintenance technology directly affects aviation safety, operation efficiency, and cost control. During the aircraft maintenance process, the disassembly and installation of aviation components are basic and frequent tasks, and their efficiency and accuracy directly affect the overall quality of maintenance work.

[0003] When performing the disassembly operation of aviation components, it is usually carried out on a corresponding disassembly platform, and corresponding disassembly tooling is generally installed on the disassembly platform. However, when most disassembly tooling is in use, it can only play the role of clamping and fixing aviation components, and cannot realize the steering adjustment operation of the aviation components placed on the tooling. During the specific disassembly process, it is necessary to disassemble the components at multiple positions on the aviation components. At this time, if the tooling cannot rotate, the staff needs to walk frequently along the circumferential direction of the tooling and find the disassembly position accurately before they can perform the disassembly operation. This walking process will take a lot of time, affect the disassembly efficiency, and bring inconvenience to users. In view of this, we have proposed an aviation component disassembly tooling. Content of the Utility Model

[0004] The purpose of the utility model is to provide an aviation component disassembly tooling to solve the defects proposed in the above background technique.

[0005] To achieve the above purpose, the utility model provides the following technical solution:

[0006] An aviation component disassembly tooling, including a disassembly operation table, a central support sleeve is fixedly installed at the center position of the upper surface of the disassembly operation table, a support turntable is arranged above the central support sleeve, a convex column arranged vertically is fixedly installed at the center position of the bottom surface of the support turntable, the convex column passes through the central support sleeve and is rotatably connected with the central support sleeve, a plurality of ring-shaped teeth arranged at equal intervals in a ring are fixedly installed on the circumferential side surface of the support turntable, a driving motor is fixedly installed on the bottom surface of the disassembly operation table, a gear is fixedly installed at the end of the output shaft of the driving motor, the gear meshes with the ring-shaped teeth, and two symmetrically arranged clamping components are fixedly installed on the upper surface of the disassembly operation table. The clamping component includes a vertical beam fixedly installed vertically on the disassembly operation table, a cylinder is fixedly installed on the vertical beam, and a clamping convex block is arranged on the telescopic shaft of the cylinder.

[0007] Preferably, a plurality of support legs arranged in a matrix are fixedly installed on the bottom surface of the disassembly operation table, and the height of the support legs is 120 cm to 150 cm.

[0008] Preferably, a protective ring is fixedly installed on the upper surface of the disassembly operation table. The protective ring is sleeved outside the support turntable, and a top protective cover plate is fixedly installed on the top of the protective ring. The top protective cover plate is annular and is sleeved above the support turntable.

[0009] Preferably, exposure holes are provided on both the protective ring and the top protective cover plate, and the gear is located at the position of the exposure holes.

[0010] Preferably, an anti-slip layer is provided on the upper surface of the support turntable, and the anti-slip layer is used to increase the friction force.

[0011] Preferably, a bottom plate is fixedly installed on the bottom side plate body of the vertical beam, and the bottom plate is fixedly installed on the disassembly operation table.

[0012] Preferably, an inclined plate is fixedly installed between the vertical beam and the bottom plate, and a triangle is formed among the inclined plate, the bottom plate and the vertical beam.

[0013] Preferably, a bolt plate is fixedly installed at the end of the telescopic shaft of the cylinder, and the clamping convex block is fixedly installed on the side surface of the bolt plate.

[0014] Compared with the prior art, the beneficial effects of the present utility model are as follows:

[0015] 1. The present utility model performs a support operation through the provided disassembly operation table, and a support turntable is provided on the disassembly operation table. The driving motor can be used to drive the support turntable to rotate, so as to realize the direction adjustment operation of the aviation components on the support turntable. In addition, through the provided clamping assembly, after the direction adjustment, the cylinder can be used to drive the clamping convex block to clamp the aviation components. The operation is simple and convenient to use, achieving the effects of clamping and direction adjustment.

[0016] 2. Through the provided protective ring and top protective cover plate, the present utility model can protect the teeth near the side part of the disassembly operation table, avoiding the situation that the clothes of the staff are caught in the teeth and causing harm to the staff. Description of the Drawings

[0017] Figure 1 is a schematic diagram of the overall structure of the present utility model;

[0018] Figure 2 is a schematic diagram of a partial structure of the present utility model;

[0019] Figure 3 Schematic diagram of the clamping assembly of the present utility model;

[0020] Figure 4 Partial schematic diagram of the clamping assembly of the present utility model;

[0021] The meanings of each label in the figure are as follows:

[0022] 1. Disassembly operation table; 10. Support leg; 11. Central support sleeve; 12. Protection ring; 13. Top protection cover plate; 14. Exposure hole;

[0023] 2. Support turntable; 20. Gear teeth; 21. Anti-slip layer; 22. Convex column; 23. Gear; 24. Driving motor;

[0024] 3. Clamping assembly; 30. Vertical beam; 31. Bottom plate; 32. Inclined plate; 33. Cylinder; 34. Bolt plate; 35. Clamping convex block. Specific embodiments

[0025] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all of the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without making creative efforts belong to the scope of protection of the present utility model.

[0026] Please refer to Figures 1-4 , the present utility model provides a technical solution: an aviation component disassembly tooling, including a disassembly operation table 1, a central support sleeve 11 is fixedly installed at the center position of the upper surface of the disassembly operation table 1, a support turntable 2 is arranged above the central support sleeve 11, a vertically arranged convex column 22 is fixedly installed at the center position of the bottom surface of the support turntable 2, the convex column 22 passes through the central support sleeve 11 and is rotatably connected with the central support sleeve 11, a plurality of gear teeth 20 arranged in a ring at equal intervals are fixedly installed on the circumferential side surface of the support turntable 2, a driving motor 24 is fixedly installed on the bottom surface of the disassembly operation table 1, a gear 23 is fixedly installed at the end of the output shaft of the driving motor 24, and the gear 23 meshes with the gear teeth 20, so as to realize the operation of the driving motor 24 to drive the support turntable 2 to rotate for orientation adjustment operation;

[0027] Specifically, two symmetrically arranged clamping assemblies 3 are fixedly installed on the upper surface of the disassembly operation table 1. The clamping assembly 3 includes a vertical beam 30 fixedly installed on the disassembly operation table 1 in a vertical state, a cylinder 33 is fixedly installed on the vertical beam 30, and a clamping convex block 35 is arranged on the telescopic shaft of the cylinder 33, so as to realize the operation of the cylinder 33 to drive the clamping convex block 35 to clamp on the aviation component to complete the clamping and fixing operation.

[0028] In this embodiment, a plurality of support legs 10 arranged in a matrix are fixedly installed on the bottom surface of the disassembly operation table 1. The height of the support legs 10 is 120 cm to 150 cm, so as to realize stable support operation by using the support legs 10.

[0029] Specifically, a protective ring 12 is fixedly installed on the upper surface of the disassembly operation table 1. The protective ring 12 is sleeved outside the support turntable 2. A top protective cover plate 13 is fixedly installed on the top of the protective ring 12. The top protective cover plate 13 is annular and is sleeved above the support turntable 2, so as to protect the tooth 20 part and prevent the clothes of the staff from being caught in the tooth 20 part and causing harm to the staff.

[0030] Furthermore, exposure holes 14 are provided on both the protective ring 12 and the top protective cover plate 13. The gear 23 is located at the exposure hole 14 part, so that the gear 23 can normally engage with the tooth 20.

[0031] In addition, an anti-slip layer 21 is provided on the upper surface of the support turntable 2. The anti-slip layer 21 can be made by setting anti-slip stripes. The anti-slip layer 21 is used to increase the friction force, so that the aviation component is not easy to slip when placed on the support turntable 2.

[0032] It should be noted that a bottom plate 31 is fixedly installed on the bottom side plate of the vertical beam 30. The bottom plate 31 is fixedly installed on the disassembly operation table 1 through a plurality of fastening bolts, which is convenient for fixed installation operation; an inclined plate 32 is fixedly installed between the vertical beam 30 and the bottom plate 31. A triangle is formed among the inclined plate 32, the bottom plate 31 and the vertical beam 30, so as to realize stable support operation for the vertical beam 30.

[0033] It should be noted that a bolt plate 34 is fixedly installed at the end of the telescopic shaft of the cylinder 33. The clamping convex block 35 is fixedly installed on the side surface of the bolt plate 34 through a plurality of fastening bolts, which is convenient for fixed installation and disassembly operations and realizes the replacement of the types of the clamping convex blocks 35.

[0034] When the aviation component disassembly tool of the present utility model is in use, the aviation component is placed on the support turntable 2, and then the cylinder 33 is started to work. When the cylinder 33 works, the telescopic shaft on it extends to drive the clamping convex block 35 to move forward, so as to realize clamping on the aviation component by using the clamping convex block 35, complete clamping and fixing, and then carry out disassembly operation;

[0035] When commutation is required, start the cylinder 33 and make it work. When the cylinder 33 works, the telescopic shaft thereon shortens and drives the clamping convex block 35 to move backward. At this time, the clamping convex block 35 no longer clamps the aviation component. Connect the driving motor 24 to an external power source and make it work. When the driving motor 24 works, the output shaft thereon rotates to drive the gear 23 to rotate. Since the gear 23 meshes with the tooth 20, it can further drive the support turntable 2 to rotate. After the support turntable 2 rotates, the orientation of the aviation component is adjusted. After the adjustment, continue to use the clamping convex block 35 for clamping operation.

[0036] The above shows and describes the basic principles, main features and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited by the above embodiments. The above embodiments and the descriptions in the specification are only preferred examples of the present invention and are not used to limit the present invention. Without departing from the spirit and scope of the present invention, the present invention will have various changes and improvements, and these changes and improvements all fall within the scope of the present invention claimed. The scope of protection required by the present invention is defined by the appended claims and their equivalents.

Claims

1. An aviation component disassembly tool, comprising a disassembly operation platform (1), characterized in that: A central support sleeve (11) is fixedly mounted at the center position of the upper surface of the disassembly operation table (1), a support turntable (2) is arranged above the central support sleeve (11), a vertically arranged convex column (22) is fixedly mounted at the center position of the bottom surface of the support turntable (2), the convex column (22) passes through the central support sleeve (11) and is rotatably connected to the central support sleeve (11), a plurality of gear teeth (20) arranged in an annular shape and at equal intervals are fixedly mounted on the annular side surface of the support turntable (2), and the bottom surface of the disassembly operation table (1) is provided with a plurality of gear teeth (20) arranged in an annular shape and at equal intervals. A drive motor (24) is fixedly mounted on the upper surface, a gear (23) is fixedly mounted on the output shaft end of the drive motor (24), the gear (23) and the gear teeth (20) are meshed with each other, and two symmetrical clamping assemblies (3) are fixedly mounted on the upper surface of the disassembly operation table (1). The clamping assembly (3) comprises a vertical beam (30) fixedly mounted on the disassembly operation table (1) in a vertical shape, a cylinder (33) is fixedly mounted on the vertical beam (30), and a clamping protrusion (35) is provided on the telescopic shaft of the cylinder (33).

2. The aviation component disassembly tool according to claim 1, characterized in that: A plurality of support legs (10) arranged in a matrix are fixedly mounted on the bottom surface of the disassembly operation table (1), and the height of the support legs (10) is 120 cm to 150 cm.

3. The aviation component disassembly tool according to claim 1, characterized in that: A protective ring (12) is fixedly mounted on the upper surface of the disassembly operation table (1), the protective ring (12) being sleeved on the outside of the support turntable (2), and a top protective cover plate (13) is fixedly mounted on the top of the protective ring (12), the top protective cover plate (13) being ring-shaped and sleeved on the top of the support turntable (2).

4. The aviation component disassembly tool according to claim 3, characterized in that: The protection ring (12) and the top protection cover plate (13) are both provided with an exposure hole (14), and the gear (23) is located at the exposure hole (14).

5. The aviation component disassembly tool according to claim 1, characterized in that: An anti-slip layer (21) is provided on the upper surface of the supporting turntable (2), and the anti-slip layer (21) is used to increase friction.

6. The aviation component disassembly tool according to claim 1, characterized in that: A bottom plate (31) is fixedly mounted on the bottom side plate of the vertical beam (30), and the bottom plate (31) is fixedly mounted on the disassembly operation table (1).

7. The aviation component disassembly tool according to claim 6, characterized in that: An inclined plate (32) is fixedly installed between the vertical beam (30) and the bottom plate (31), and a triangle is formed between the inclined plate (32), the bottom plate (31) and the vertical beam (30).

8. The aviation component disassembly tool according to claim 1, characterized in that: A bolt plate (34) is fixedly mounted on the end of the telescopic shaft of the cylinder (33), and the clamping protrusion (35) is fixedly mounted on the side surface of the bolt plate (34).

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