Aircraft tire building machine

Abstract

The utility model relates to the technical field of aviation special one -time law tire forming, in particular to a kind of aviation special one -time law tire forming machine, it is set up clamping mechanism and limiting mechanism to make aviation special one -time law tire forming process, the covering of tire can be more uniform, prevent the depression of support part after tire forming, improve processing quality;Including mounting mechanism;Still including driving mechanism, multiple sets of clamping mechanism and multiple sets of limiting mechanism, driving mechanism is installed on mounting mechanism, multiple sets of clamping mechanism are installed on mounting mechanism, and a set of limiting mechanism is installed on each set of clamping mechanism;The mounting mechanism is installed, driving mechanism is driven, clamping mechanism is clamped, and limiting mechanism is positioned.

Description

Technical Field

[0001] This utility model relates to the technical field of one-step tire forming for aviation, and in particular to a one-step tire forming machine for aviation. Background Technology

[0002] The aviation-specific one-step tire forming machine is a core piece of equipment in aviation tire manufacturing, designed specifically to meet the special requirements of high strength, high precision, and high reliability of aviation tires.

[0003] Among existing aviation-grade one-step tire forming machines, such as the single-drum one-step automatic motorcycle tire forming machine disclosed in utility model patent application number 202023217279.9, this utility model achieves the function of conveniently processing wheel hub processing materials of different sizes by setting limit mechanisms at both the bottom and top ends of the main body. When processing wheel hub processing materials of different sizes, the second servo motor drives the connecting rod to move up and down through the clamping bar. The height of the connecting rod is adjusted according to the size of the wheel hub processing material, and then adjusted by the first spring according to the thickness of the wheel hub processing material, so that the upper and lower support rods can limit the wheel hub processing material, thereby enabling the processing of various types of wheel hubs.

[0004] However, in the one-step tire forming process for aviation, uneven stress on the tire wrapping can cause dents in areas of heavy stress after tire forming, reducing processing quality. Utility Model Content

[0005] To solve the above-mentioned technical problems, this utility model provides an aviation-specific one-step tire forming machine that, by setting a clamping mechanism and a limiting mechanism, can achieve more uniform tire coverage during the one-step tire forming process, prevent the support part from sinking after tire forming, and improve the processing quality.

[0006] This utility model discloses a one-step tire forming machine for aviation, including an installation mechanism; it also includes a drive mechanism, multiple clamping mechanisms and multiple limiting mechanisms. The drive mechanism is installed on the installation mechanism, the multiple clamping mechanisms are installed on the installation mechanism, and each clamping mechanism is equipped with a limiting mechanism. The installation mechanism performs installation, the drive mechanism performs driving, the clamping mechanism performs clamping, and the limiting mechanism performs limiting. By installing and limiting the equipment through the installation mechanism, driving by opening the drive mechanism, clamping the tire through the clamping mechanism, and limiting the clamping mechanism through the limiting mechanism, the tire can be more evenly covered during the one-step tire forming process for aviation-specific tires, preventing dents in the support parts after tire forming and improving processing quality.

[0007] Preferably, the installation mechanism includes a mounting frame and multiple sets of support plates, with the multiple sets of support plates rotatably mounted on the mounting frame; the equipment is installed and fixed by the mounting frame, and supported by the support plates.

[0008] Preferably, the drive mechanism includes a rotating ring, a telescopic cylinder, and multiple sets of support rods. The rotating ring is rotatably mounted on the mounting frame, the telescopic cylinder is rotatably mounted on the mounting frame, and the output end of the telescopic cylinder is connected to the rotating ring. The multiple sets of support rods are rotatably mounted on the rotating ring, and each set of support rods is rotatably connected to a set of support plates. By opening the telescopic cylinder, the rotating ring is driven to rotate, and the rotation of the rotating ring simultaneously drives the support rods to rotate, supporting the support plates and causing them to lift up.

[0009] Preferably, the clamping mechanism includes a clamping plate and two sets of limiting wheels. The clamping plate is rotatably mounted on the support plate, and the two sets of limiting wheels are rotatably mounted on the clamping plate. The clamping plate clamps and limits the tire, and the limiting wheels limit the other set of clamping plates.

[0010] Preferably, the limiting mechanism includes a wheel frame, a spring, and two sets of limiting wheels. The wheel frame is slidably mounted on the clamping plate by the spring, and the two sets of limiting wheels are rotatably mounted on the wheel frame. The spring pulls the wheel frame to make the limiting wheels fit and limit the clamping plate.

[0011] Compared with the prior art, the beneficial effects of this utility model are as follows: the installation mechanism limits the installation of the equipment, the drive mechanism drives the equipment, the clamping mechanism clamps the tire, and the limiting mechanism limits the clamping mechanism. This allows for more uniform tire coverage during the one-time tire forming process for aviation-specific tires, prevents dents in the support parts after tire forming, and improves processing quality. Attached Figure Description

[0012] Figure 1 This is a schematic diagram of the isometric structure of this utility model; Figure 2 This is a first frontal sectional isometric structural schematic diagram of this utility model; Figure 3 This is a second frontal sectional isometric structural schematic diagram of this utility model; Figure 4 The limiting mechanism of this utility model is in Figure 3 Axonometric enlarged structural schematic diagram of the frontal cross-section of section A in the middle; The following are labels in the attached diagram: 1. Mounting mechanism; 11. Mounting frame; 12. Support plate; 2. Drive mechanism; 21. Rotary ring; 22. Telescopic cylinder; 23. Support rod; 3. Clamping mechanism; 31. Clamping plate; 32. Limiting wheel one; 4. Limiting mechanism; 41. Wheel frame; 42. Spring; 43. Limiting wheel two. Detailed Implementation

[0013] 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. Example 1

[0014] like Figures 1 to 4 As shown, an aviation-specific one-step tire forming machine includes an installation mechanism 1, a drive mechanism 2, multiple clamping mechanisms 3, and multiple limiting mechanisms 4. The drive mechanism 2 is installed on the installation mechanism 1, the multiple clamping mechanisms 3 are installed on the installation mechanism 1, and each clamping mechanism 3 is equipped with a limiting mechanism 4. The installation mechanism 1 performs the installation, the driving mechanism 2 performs the driving, the clamping mechanism 3 performs the clamping, and the limiting mechanism 4 performs the limiting. The mounting mechanism 1 includes a mounting frame 11 and multiple sets of support plates 12, which are rotatably mounted on the mounting frame 11. The drive mechanism 2 includes a rotating ring 21, a telescopic cylinder 22, and multiple sets of support rods 23. The rotating ring 21 is rotatably mounted on the mounting frame 11, the telescopic cylinder 22 is rotatably mounted on the mounting frame 11, and the output end of the telescopic cylinder 22 is connected to the rotating ring 21. Multiple sets of support rods 23 are rotatably mounted on the rotating ring 21, and each set of support rods 23 is rotatably connected to a set of support plates 12. The clamping mechanism 3 includes a clamping plate 31 and two sets of limiting wheels 32. The clamping plate 31 is rotatably mounted on the support plate 12, and the two sets of limiting wheels 32 are rotatably mounted on the clamping plate 31. The limiting mechanism 4 includes a wheel frame 41, a spring 42 and two sets of limiting wheels 43. The wheel frame 41 is slidably mounted on the clamping plate 31 via the spring 42, and the two sets of limiting wheels 43 are rotatably mounted on the wheel frame 41. The equipment is installed and fixed by the mounting frame 11 and supported by the support plate 12. The rotating ring 21 is driven to rotate by opening the telescopic cylinder 22. At the same time, the rotating ring 21 drives the support rod 23 to rotate and support the support plate 12, thus raising the support plate 12. The tire is clamped and limited by the clamping plate 31. The first limiting wheel 32 limits the other set of clamping plates 31. At the same time, the spring 42 pulls the wheel frame 41 so that the second limiting wheel 43 fits and limits the clamping plate 31. In this way, the tire can be covered more evenly during the one-time forming process of aviation special tires, preventing the support part from sinking after the tire is formed and improving the processing quality.

[0015] like Figures 1 to 4As shown, this utility model discloses a one-step tire forming machine for aviation. During operation, the equipment is installed and fixed by the mounting frame 11 and supported by the support plate 12. The rotating ring 21 is driven to rotate by opening the telescopic cylinder 22. At the same time, the rotating ring 21 rotates and drives the support rod 23 to rotate, supporting the support plate 12 and raising it. The tire is clamped and limited by the clamping plate 31. The first limiting wheel 32 limits another set of clamping plates 31. At the same time, the spring 42 pulls the wheel frame 41 so that the second limiting wheel 43 fits and limits the clamping plate 31.

[0016] The telescopic cylinder 22 of this utility model is purchased from the market. Technical personnel in this industry only need to install and operate it according to the accompanying instruction manual, without requiring any creative work from those skilled in the art.

[0017] The main function achieved by this utility model is: in the process of forming aviation-specific one-time tires, by setting up a clamping mechanism and a limiting mechanism, the tire can be covered more evenly during the forming process, preventing the support part from sinking after the tire is formed, and improving the processing quality.

[0018] 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 aviation-specific one-step tire forming machine, comprising a mounting mechanism (1); characterized in that, It also includes a drive mechanism (2), multiple clamping mechanisms (3) and multiple limiting mechanisms (4). The drive mechanism (2) is installed on the mounting mechanism (1), the multiple clamping mechanisms (3) are installed on the mounting mechanism (1), and each clamping mechanism (3) is equipped with a limiting mechanism (4). The installation mechanism (1) performs installation, the driving mechanism (2) performs driving, the clamping mechanism (3) performs clamping, and the limiting mechanism (4) performs limiting.

2. A one-shot tyre building machine for aircraft tyres according to claim 1, characterized in that, The mounting mechanism (1) includes a mounting frame (11) and multiple sets of support plates (12), which are rotatably mounted on the mounting frame (11).

3. A one-shot tyre building machine for aircraft tyres according to claim 2, characterised in that, The drive mechanism (2) includes a rotating ring (21), a telescopic cylinder (22) and multiple sets of support rods (23). The rotating ring (21) is rotatably mounted on the mounting frame (11). The telescopic cylinder (22) is rotatably mounted on the mounting frame (11), and the output end of the telescopic cylinder (22) is connected to the rotating ring (21). Multiple sets of support rods (23) are rotatably mounted on the rotating ring (21), and each set of support rods (23) is rotatably connected to a set of support plates (12).

4. The aviation-specific one-step tire forming machine as described in claim 2, characterized in that, The clamping mechanism (3) includes a clamping plate (31) and two sets of limiting wheels (32). The clamping plate (31) is rotatably mounted on the support plate (12), and the two sets of limiting wheels (32) are rotatably mounted on the clamping plate (31).

5. A one-shot tyre building machine for aircraft tyres according to claim 4, characterised in that, The limiting mechanism (4) includes a wheel frame (41), a spring (42) and two sets of limiting wheels (43). The wheel frame (41) is slidably mounted on the clamping plate (31) by the spring (42), and the two sets of limiting wheels (43) are rotatably mounted on the wheel frame (41).

Images