Airplane wheel structure with airtight one-way conduction capability

By installing components such as valve seats, valves, and push rods on aircraft wheels, one-way airtightness is achieved, solving the problem of increased maintenance time and cost caused by installing temperature and pressure sensors and other components in existing technologies, and achieving convenient installation and good maintainability.

CN121062384APending Publication Date: 2025-12-05GUIZHOU XINAN AVIATION MACHINING CO LTD
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Patent Information

Application Number
CN202511221530.3
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-08-29
Publication Date
2025-12-05

AI Technical Summary

Technical Problem

Existing aircraft wheel designs increase repair time and maintenance costs, and are complex to operate when installing components such as temperature and pressure sensors.

Method used

Design a wheel structure with airtight unidirectional conduction capability. By setting components such as valve seat, valve, push rod and spring on the wheel assembly, airtight unidirectional conduction is achieved, and a convenient installation interface is provided to connect components such as temperature and pressure sensors.

Benefits of technology

It enables convenient installation and easy maintenance of aircraft wheels, reduces maintenance time and costs, and ensures airtightness and real-time monitoring functions.

✦ Generated by Eureka AI based on patent content.

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Patent Text Reader

Abstract

The invention relates to the technical field of aircraft wheels, in particular to an aircraft wheel structure with airtight one-way conduction capability, which comprises an aircraft wheel assembly, a valve body sealing ring, a valve body seat, an end face sealing ring, an ejector rod, a valve, a self-locking nut and a spring, an air hole is formed in the airplane wheel assembly to enable an inner cavity of the valve body seat to be communicated with one side, where a tire is installed, of the airplane wheel, a connector is arranged on the outer side of the valve body seat, a valve body sealing ring is arranged between the airplane wheel assembly and the valve body seat, an ejector rod, a valve and a spring are arranged in the inner cavity of the valve body seat, and the inner side of the ejector rod penetrates through an inner hole of the valve and extends into the inner cavity of the valve body seat. The self-locking nut is installed on the ejector rod through threads and abuts against the end face of the valve, the ejector rod is sleeved with the spring, the two ends of the spring abut against the valve and the airplane wheel assembly respectively, the valve is pushed through the spring so that the valve can be tightly attached to the valve body base, and an end face sealing ring is arranged at the matching position of the valve and the valve body base and has the airtight one-way conduction capacity. Installation is convenient and maintainability is good.
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Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of aircraft wheels, in particular to a wheel structure with air tightness and one-way conduction capability. BACKGROUND

[0002] With the continuous development of intelligence, the functions of the aircraft are more and more diversified, and the performance requirements are continuously improved, and the functions and performance requirements of the aircraft parts are continuously increased. In order to monitor the temperature, tire pressure and other parameters of the aircraft wheel in real time, the interface requirements of the temperature and pressure sensors, tire pressure sensors and other parts of the aircraft wheel are proposed. The existing design of the aircraft wheel can provide installation interface, but at the same time increases the maintenance time and cost of the aircraft, and the operation is complex. SUMMARY

[0003] In order to solve the problems mentioned in the background, the present application provides a wheel structure with air tightness and one-way conduction capability.

[0004] The present application discloses the following technical scheme: a wheel structure with air tightness and one-way conduction capability, comprising a wheel assembly, a valve body sealing ring, a valve body seat, an end face sealing ring, a top rod, a valve, a self-locking nut and a spring, the valve body seat is installed on the wheel assembly, a gas hole is provided on the wheel assembly to communicate the inner cavity of the valve body seat with one side of the tire installed on the wheel, an interface is provided on the outer side of the valve body seat, a valve body sealing ring is provided between the wheel assembly and the valve body seat, the inner cavity of the valve body seat is provided with a top rod, a valve and a spring, the inside of the top rod passes through the inner hole of the valve and extends into the inner cavity of the valve body seat, the outer side shoulder of the top rod abuts against the outer side end face of the valve, the self-locking nut is installed on the top rod through threads and abuts against the end face of the valve, the spring is sleeved on the outside of the top rod, and the two ends of the spring abut against the valve and the wheel assembly respectively, the valve is pushed by the spring to make the valve tightly fit the valve body seat, and the end face sealing ring is arranged at the matching position of the valve and the valve body seat.

[0005] Further, the valve body seat is installed on the wheel assembly through threads.

[0006] Further, the wheel assembly and the valve body seat are both provided with a fuse hole, and a fuse can be used to prevent loosening to stably install the valve body seat on the wheel assembly.

[0007] Further, the matching position of the valve and the valve body seat is a conical surface.

[0008] Advantages: compared with the prior art, the wheel structure with air tightness and one-way conduction capability of the present application sets a valve body seat on the aircraft wheel, sets a valve and a top rod and other components in the valve body seat to realize air tightness and one-way conduction capability, sets an interface on the valve body seat for connecting performance parts on the wheel, and is convenient and fast to install and has good maintainability. BRIEF DESCRIPTION OF DRAWINGS

[0009] Figure 1The machine wheel structure with air tightness and one-way conduction ability of the application is shown in the figure. In the figure: 1-machine wheel assembly, 2-valve body sealing ring, 3-valve body seat, 4-end face sealing ring, 5-top rod, 6-shutter, 7-self-locking nut, 8-spring. DETAILED DESCRIPTION

[0010] As Figure 1 shown, a machine wheel structure with air tightness and one-way conduction ability includes machine wheel assembly 1, valve body sealing ring 2, valve body seat 3, end face sealing ring 4, top rod 5, shutter 6, self-locking nut 7 and spring 8. The valve body seat 3 is installed on the machine wheel assembly 1 and is screwed on the machine wheel assembly 1. Both the machine wheel assembly 1 and the valve body seat 3 are provided with fuse holes, and a fuse can be used to prevent loosening to ensure that the valve body seat 3 is stably installed on the machine wheel assembly 1. The machine wheel assembly 1 is provided with an air hole to communicate the inner cavity of the valve body seat 3 with one side of the tire installed on the machine wheel. The outer side of the valve body seat 3 is provided with an interface for connecting other performance components on the machine wheel, such as temperature and pressure sensors, tire pressure sensors, etc. The machine wheel assembly 1 and the valve body seat 3 are provided with the valve body sealing ring 2 to effectively ensure air tightness. The inner cavity of the valve body seat 3 is provided with the top rod 5, the shutter 6 and the spring 8. The inner side of the top rod 5 extends into the inner cavity of the valve body seat 3 through the inner hole of the shutter 6. The outer side shaft shoulder of the top rod 5 abuts against the outer side end face of the shutter 6. The self-locking nut 7 is screwed on the top rod 5 and abuts against the end face of the shutter 6. The spring 8 is sleeved on the outer side of the top rod 5, and the two ends of the spring 8 abut against the shutter 6 and the machine wheel assembly 1 respectively. The shutter 6 is pushed by the spring 8 to tightly abut against the valve body seat 3. The shutter 6 and the valve body seat 3 are cooperated at a tapered surface. The cooperation part of the shutter 6 and the valve body seat 3 is provided with the end face sealing ring 4 to ensure air tightness. The outer side end face of the top rod 5 is located in the interface on the outer side of the valve body. When the components are installed at the interface, pressure is applied to the top rod 5.

[0011] Working principle: The valve body seat 3 is provided with an installation interface for installing other performance components on the machine wheel. The interface on the valve body seat 3 can be adjusted according to the interface requirements of the performance components to improve the installation capacity of the machine wheel. When the temperature and pressure sensors, tire pressure sensors and other components are installed on the valve body seat 3, pressure is applied to the top rod 5. After the top rod 5 is stressed, the shutter 6, the self-locking nut 7 and the end face sealing ring 4 are moved to the inside of the valve body seat 3 to compress the spring 8, so that the shutter 6 is separated from the valve body seat 3, and a gap is generated between them. The air pressure in the machine wheel is communicated with the tire pressure sensor through the gap to realize real-time monitoring of the tire pressure of the aviation machine wheel. When the tire pressure sensor is disassembled, the spring 8 is reset to push the shutter 6, the self-locking nut 7, the end face sealing ring 4 and the top rod 5 to move outward, so that the shutter 6 abuts against the valve body seat 3 to restore the air tightness and realize the air tightness and one-way conduction ability of the aviation machine wheel.

[0012] The above merely describes preferred specific embodiments of the present application, but the protection scope of the present application is not limited thereto, and any person skilled in the art, according to the technical solution and inventive concept of the present application, makes equivalent replacement or change within the technical range disclosed by the present application, which should be covered within the protection scope of the present application.

Claims

1. A wheel structure with airtight unidirectional conduction capability, characterized in that: The utility model provides a valve seat and machine wheel assembly, including machine wheel assembly (1), valve body sealing ring (2), valve body seat (3), end face sealing ring (4), top rod (5), valve (6), self locking nut (7) and spring (8), valve body seat (3) is installed on machine wheel assembly (1), and machine wheel assembly (1) is equipped with air hole and is communicated with the inside chamber of valve body seat (3) and the one side of machine wheel installation tire, and the outside of valve body seat (3) is equipped with interface, and machine wheel assembly (1) is equipped with valve body sealing ring (2) between valve body seat (3), and the inside chamber of valve body seat (3) is equipped with top rod (5), valve (6) and spring (8), and the inside of top rod (5) passes through the hole of valve (6) and extends into the inside chamber of valve body seat (3), and the outside shaft shoulder of top rod (5) is in abutment with the outside end face of valve (6), and self locking nut (7) is installed on top rod (5) through thread and is in abututment with the end face of valve (6), and spring (8) is sleeved on the outside of top rod (5), and the both ends of spring (8) are in abutment with valve (6) and machine wheel assembly (1) respectively, and the valve (6) is pushed by spring (8) to make valve (6) and valve body seat (3) tightly adhere, and end face sealing ring (4) is arranged at the cooperation place of valve (6) and valve body seat (3).

2. The wheel structure with air-tight one-way conducting capability according to claim 1, characterized in that: The valve body seat (3) is installed on the machine wheel assembly (1) through thread.

3. The wheel structure with air-tight one-way conducting capability according to claim 1, characterized in that: The machine wheel assembly (1) and the valve body seat (3) are both equipped with fuse hole, and fuse can be used to prevent loosening to make the valve body seat (3) stably installed on the machine wheel assembly (1).

4. The wheel structure with air-tight one-way conducting capability according to claim 1, characterized in that: The cooperation place of the valve (6) and the valve body seat (3) is conical surface.