An aircraft tire inflation and shaping device

Abstract

The utility model relates to the technical field of aviation tire inflation setting, especially an aviation tire inflation setting device, which is provided with a matching mechanism and a conduction mechanism, so that the inflation condition of the tire can be detected during the aviation tire inflation setting process, the inflation setting precision of the tire is determined, and the processing quality is improved; the device comprises a supporting mechanism; further comprising a limiting mechanism, a plurality of matching mechanisms, a conduction mechanism and a plurality of detection mechanisms, the limiting mechanism is installed on the supporting mechanism, the plurality of matching mechanisms are installed on the supporting mechanism, the conduction mechanism is installed on the supporting mechanism, and the plurality of detection mechanisms are installed on the supporting mechanism; the supporting mechanism supports, the limiting mechanism limits, the matching mechanism matches, the conduction mechanism conducts, and the detection mechanism detects.

Description

Technical Field

[0001] This utility model relates to the technical field of aircraft tire inflation and shaping, and in particular to an aircraft tire inflation and shaping device. Background Technology

[0002] In the tire manufacturing process, tire vulcanization is the last step. High-temperature vulcanized tires will deform as they gradually cool at room temperature, which will seriously affect the quality of the tires. In order to avoid this, tires that have just been vulcanized at high temperature are usually placed on an inflation and shaping device to gradually cool to room temperature so that the shape of the tire will remain unchanged.

[0003] Among existing aircraft tire inflation and shaping devices, such as the novel pneumatic rear-inflation tire shaping device disclosed in utility model patent application number 201921905262.7, this utility model, through the cooperation of a sensor and a trigger switch, adjusts the position of the sensor before inflating and shaping the tire, which can ensure that the tire is inflated and shaped in the optimal outer diameter state, thereby improving the accuracy and quality of shaping.

[0004] However, during the inflation and shaping process of aircraft tires, it is impossible to determine the degree of inflation uniformity by measuring the tire in a single measurement while it is being inflated transversely. Utility Model Content

[0005] To solve the above-mentioned technical problems, this utility model provides an aircraft tire inflation and shaping device that, by setting a bonding mechanism and a transmission mechanism, can detect the inflation status of the tire around its circumference during the inflation and shaping process, determine the tire inflation and shaping accuracy, and improve the processing quality.

[0006] This utility model discloses an aircraft tire inflation and shaping device, which includes a support mechanism; it also includes a limiting mechanism, multiple sets of bonding mechanisms, a transmission mechanism, and multiple sets of detection mechanisms. The limiting mechanism is installed on the support mechanism, the multiple sets of bonding mechanisms are installed on the support mechanism, the transmission mechanism is installed on the support mechanism, and the multiple sets of detection mechanisms are installed on the support mechanism. The supporting mechanism provides support, the limiting mechanism provides positioning, the bonding mechanism provides bonding, the transmission mechanism provides transmission, and the detection mechanism provides detection. By supporting the tire with the supporting mechanism, limiting and clamping it with the limiting mechanism, bonding it with the bonding mechanism, transmitting displacement through the transmission mechanism, and detecting it through the detection mechanism, the inflation status of the tire can be detected around the tire during the inflation and shaping process of the aviation tire, the inflation and shaping accuracy of the tire can be determined, and the processing quality can be improved.

[0007] Preferably, the support mechanism includes a base frame, a support frame, an air pump, and an air duct. The support frame is installed on the upper end of the base frame, the air pump is installed on the base frame, the inlet end of the air duct is connected to the outlet end of the air pump, and the outlet end of the air duct extends into the support frame. The tire is supported by the support frame, and the tire is inflated by turning on the air pump through the air duct.

[0008] Preferably, the limiting mechanism includes a screw, a limiting plate, and a washer. The screw is threadedly mounted on the support frame, the limiting plate is fitted onto the screw, and the washer is fitted onto the screw. The screw and the support frame are threaded together to limit and fix the tire.

[0009] Preferably, the bonding mechanism includes a support rod and a roller. The support rod is rotatably mounted on a support frame, and the roller is rotatably mounted on the support rod. The tire expansion is transmitted to the testing equipment via the support rod through the roller bonding with the tire.

[0010] Preferably, the transmission mechanism includes a lifting frame, a transmission frame, and multiple sets of support rods. The lifting frame is slidably mounted on the support frame, the transmission frame is fitted onto the lifting frame, and the multiple sets of support rods are mounted on the transmission frame via ball joints. Each set of support rods is connected to a set of support rods via ball joints. The support rods are pressed down by rotating, and the lifting frame descends while the support rods are pressed down, which in turn facilitates displacement transmission by coordinating with the rotation of the transmission frame.

[0011] Preferably, the testing mechanism includes a support, a testing device, and a spring. The support is rotatably mounted on the upper end of the base frame via a ball joint, and the testing device is rotatably mounted on the lower end of the transmission frame via a ball joint. The support and the testing device are slidably connected, and the testing device is supported by the spring. The testing device is pressed down by the spring through the lifting frame and the transmission frame.

[0012] Compared with the prior art, the beneficial effects of this utility model are as follows: the tire is supported by a support mechanism, clamped by a limiting mechanism, bonded by a bonding mechanism, displaced by a transmission mechanism, and detected by a detection mechanism. Thus, during the inflation and shaping process of aviation tires, the inflation status of the tires can be detected around the tires, the inflation and shaping accuracy of the tires can be determined, and the processing quality can be improved. Attached Figure Description

[0013] Figure 1 This is a schematic diagram of the isometric structure of this utility model; Figure 2 This is a frontal sectional isometric structural schematic diagram of this utility model; Figure 3 The testing agency of this utility model is Figure 2 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. Support mechanism; 11. Base frame; 12. Support frame; 13. Air pump; 14. Air duct; 2. Limiting mechanism; 21. Screw; 22. Limiting plate; 23. Gasket; 3. Fitting mechanism; 31. Support rod; 32. Roller; 4. Transmission mechanism; 41. Lifting frame; 42. Transmission frame; 43. Support rod; 5. Detection mechanism; 51. Bracket; 52. Detection device; 53. Spring. Detailed Implementation

[0014] 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

[0015] like Figures 1 to 3 As shown, an aircraft tire inflation and shaping device includes a support mechanism 1, a limiting mechanism 2, multiple sets of bonding mechanisms 3, a transmission mechanism 4, and multiple sets of detection mechanisms 5. The limiting mechanism 2 is installed on the support mechanism 1, the multiple sets of bonding mechanisms 3 are installed on the support mechanism 1, the transmission mechanism 4 is installed on the support mechanism 1, and the multiple sets of detection mechanisms 5 are installed on the support mechanism 1. The supporting mechanism 1 provides support, the limiting mechanism 2 provides limiting, the fitting mechanism 3 provides fitting, the conducting mechanism 4 conducts conduction, and the detection mechanism 5 performs detection. The support mechanism 1 includes a base frame 11, a support frame 12, an air pump 13, and an air pipe 14. The support frame 12 is installed on the upper end of the base frame 11, the air pump 13 is installed on the base frame 11, the input end of the air pipe 14 is connected to the output end of the air pump 13, and the output end of the air pipe 14 extends into the support frame 12. The limiting mechanism 2 includes a screw 21, a limiting plate 22, and a washer 23. The screw 21 is installed on the support frame 12 by threaded connection, the limiting plate 22 is fitted on the screw 21, and the washer 23 is fitted on the screw 21. The bonding mechanism 3 includes a support rod 31 and a roller 32. The support rod 31 is rotatably mounted on the support frame 12, and the roller 32 is rotatably mounted on the support rod 31. The transmission mechanism 4 includes a lifting frame 41, a transmission frame 42, and multiple sets of support rods 43. The lifting frame 41 is slidably mounted on the support frame 12, the transmission frame 42 is fitted onto the lifting frame 41, and the multiple sets of support rods 43 are mounted on the transmission frame 42 through ball joints. Each set of support rods 43 is connected to a set of support rods 31 through a ball joint. The testing mechanism 5 includes a bracket 51, a testing device 52, and a spring 53. The bracket 51 is rotatably mounted on the upper end of the base frame 11 via a ball joint, and the testing device 52 is rotatably mounted on the lower end of the transmission frame 42 via a ball joint. The bracket 51 and the testing device 52 are slidably connected, and the testing device 52 is supported by the spring 53. The tire is supported by the support frame 12, and the limit plate 22 limits and fixes the tire by threading the screw 21 with the support frame 12. The tire is inflated by turning on the air pump 13 through the air pipe 14. The tire expands by the roller 32 and is in contact with the tire. The expansion is transmitted to the detection equipment through the support rod 31. The support rod 31 rotates and presses down the support rod 43. At the same time, the lifting frame 41 descends and the displacement is transmitted by the rotation of the transmission frame 42. The lifting frame 41 and the transmission frame 42 press down the spring 53 of the detection device 52 for detection. Thus, during the inflation and shaping process of the aircraft tire, the inflation status of the tire can be detected around the tire, the tire inflation and shaping accuracy can be determined, and the processing quality can be improved.

[0016] like Figures 1 to 3 As shown, this utility model discloses an aviation tire inflation and shaping device. During operation, the tire is supported by a support frame 12, and the tire is fixed by a limiting plate 22 through a screw 21 threadedly engaging with the support frame 12. The tire is inflated by turning on the air pump 13 through the air pipe 14. The tire expands through the roller 32, which is in contact with the tire. The expansion is transmitted to the testing equipment through the support rod 31. The support rod 31 rotates and presses down the support rod 43. At the same time, the lifting frame 41 descends, and the displacement is transmitted through the rotation of the transmission frame 42. The lifting frame 41 and the transmission frame 42 work together to press down the spring 53 of the testing device 52 for testing.

[0017] The air pump 13 and the testing device 52 of this utility model are purchased from the market. 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.

[0018] The main function achieved by this utility model is: during the inflation and shaping process of aircraft tires, by setting up a bonding mechanism and a transmission mechanism, the inflation status of the tires around the tires can be detected, the inflation and shaping accuracy of the tires can be determined, and the processing quality can be improved.

[0019] 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 inflation and shaping device, comprising a support mechanism (1); characterized in that, It also includes a limiting mechanism (2), multiple sets of bonding mechanisms (3), a transmission mechanism (4) and multiple sets of detection mechanisms (5). The limiting mechanism (2) is installed on the support mechanism (1), the multiple sets of bonding mechanisms (3) are installed on the support mechanism (1), the transmission mechanism (4) is installed on the support mechanism (1), and the multiple sets of detection mechanisms (5) are installed on the support mechanism (1). The supporting mechanism (1) provides support, the limiting mechanism (2) provides limiting, the fitting mechanism (3) provides fitting, the transmission mechanism (4) provides transmission, and the detection mechanism (5) performs detection.

2. The aircraft tire inflation and shaping device as described in claim 1, characterized in that, The support mechanism (1) includes a base frame (11), a support frame (12), an air pump (13), and an air duct (14). The support frame (12) is installed on the upper end of the base frame (11), the air pump (13) is installed on the base frame (11), the input end of the air duct (14) is connected to the output end of the air pump (13), and the output end of the air duct (14) extends into the support frame (12).

3. The aircraft tire inflation and shaping device as described in claim 2, characterized in that, The limiting mechanism (2) includes a screw (21), a limiting plate (22) and a washer (23). The screw (21) is installed on the support frame (12) by threaded connection. The limiting plate (22) is fitted on the screw (21) and the washer (23) is fitted on the screw (21).

4. The aircraft tire inflation and shaping device as described in claim 2, characterized in that, The bonding mechanism (3) includes a support rod (31) and a roller (32). The support rod (31) is rotatably mounted on the support frame (12), and the roller (32) is rotatably mounted on the support rod (31).

5. The aircraft tire inflation and shaping device as described in claim 4, characterized in that, The transmission mechanism (4) includes a lifting frame (41), a transmission frame (42) and multiple sets of support rods (43). The lifting frame (41) is slidably mounted on the support frame (12), the transmission frame (42) is fitted on the lifting frame (41), and multiple sets of support rods (43) are mounted on the transmission frame (42) through ball heads. Each set of support rods (43) is connected to a set of support rods (31) through ball heads.

6. The aircraft tire inflation and shaping device as described in claim 5, characterized in that, The testing mechanism (5) includes a bracket (51), a testing device (52) and a spring (53). The bracket (51) is mounted on the upper end of the base frame (11) by ball joint rotation. The testing device (52) is mounted on the lower end of the transmission frame (42) by ball joint rotation. The bracket (51) and the testing device (52) are slidably connected. The testing device (52) is supported by the spring (53).

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