A kind of aviation tire cable test equipment and method

Abstract

The present invention relates to the technical field of aviation test equipment, and in particular to an aviation tire cable-passing test equipment and method. It comprises: a tire rolling simulation device, including an aviation tire and a pavement simulation component, which is used to drive the aviation tire to roll and provide a simulation scene of the aviation tire rolling on the pavement; it also comprises a sensor test device, a control device, and a cable-passing device, including a variable-section steel cable and a traction component. During the cable-passing test, the traction component pulls the variable-section steel cable from an initial position to a terminal position, and contacts and rolls with the aviation tire to complete the tire cable-passing test. The present invention obtains accurate tire test data by comprehensively analyzing tire performance, which helps to improve the quality of the tire and its cable-passing performance, obtains first-hand effective data for studying tire characteristics, and provides a reliable basis for improving tire production quality and optimizing tire design.

Description

Technical Field

[0001] The present invention relates to the technical field of aviation test equipment, and in particular to an aviation tire cable-passing test device and method. Background Art

[0002] Aircraft wheel cable passing is one of the important dynamic tests that must be conducted to verify the quality, performance and life of aircraft tires. It is an important guarantee for ensuring the safety of carrier-based aircraft cable passing and taxiing. At present, there is no special tire dynamic cable passing test equipment in China. The existing method is to use a simple test by pressing the tire on a steel pipe (or steel bar) for static loading.

[0003] Whether it is a carrier-based aircraft or a land-based aircraft, the tires are subjected to a transient impact load when passing through the cable under high-speed rolling conditions. If the static loading test method is used, first of all, there is a difference between the tire pressing on the steel cable and pressing on the surface of the steel tube, and secondly, the difference between static load and dynamic load. At the same time, the influence of the tire rolling speed and inertia force is not considered, and it does not have the ability to simulate the tire roll and yaw. Obviously, the static test method is not comprehensive enough and cannot correctly evaluate the tire quality, performance and service life. Summary of the invention

[0004] The present invention provides an aviation tire cable test device and method to solve the problem that the current wheel test method is not comprehensive enough and cannot correctly evaluate the tire quality, performance and service life.

[0005] In order to solve the above technical problems, the technical solution of the present invention is as follows:

[0006] An aviation tire cable test device, comprising:

[0007] A tire rolling simulation device, including an aircraft tire and a pavement simulation component, is used to drive the aircraft tire to roll and provide a simulation scene of the aircraft tire rolling on the pavement;

[0008] A sensor test device, including a sensor device, the sensor device is connected to the aircraft tire and is used to obtain various test data of the aircraft tire during the cable passing process;

[0009] A control device for controlling the aircraft tire cable test process and collecting test data; and

[0010] The cable passing device includes a variable-section steel cable and a traction assembly. During the cable passing test, the traction assembly pulls the variable-section steel cable from an initial position to an end position, and contacts and rolls with the aviation tire to complete the tire cable passing test.

[0011] Furthermore, the cable passing device also includes a steel cable guide tube and a limit clamp; the steel cable guide tube and the limit clamp are arranged on the traction assembly, the retracted end of the variable-section steel cable is limitedly passed through the steel cable guide tube, the steel cable guide tube is arranged on both sides of the limit clamp, and the limit clamp is used to limit the variable-section steel cable after traction and retraction to the end position.

[0012] Furthermore, the cable passing device also includes a follower bracket and a bracket guide ring; the bracket guide ring is arranged on both sides of the limit clamp; the bracket ring of the follower bracket is sleeved on the variable-section steel cable, and the rod sliding limit is arranged on the bracket guide ring, and is transmitted and retracted as the variable-section steel cable is pulled and retracted; the other end of the follower bracket is provided with a reset handle for adjusting the position of the steel cable.

[0013] Furthermore, the traction assembly includes a mounting base, a driving cylinder and a steel cable guide wheel. The driving cylinder is mounted on the mounting base and is connected to the variable-section steel cable traction drive through the steel cable guide wheel.

[0014] Furthermore, the driving cylinder is rotatably arranged at an angle adjustable on the mounting base, and the driving cylinder is adjusted at a relative angle on the mounting base according to the angle of the variable-section steel cable.

[0015] Furthermore, the tire rolling simulation device also includes a main load-bearing outer frame of the test bench and a tire attitude control frame. The tire attitude control frame is installed on the main load-bearing outer frame of the test bench and is connected to the tire attitude control frame for adjusting the position and attitude of the aircraft tire. The sensor equipment is arranged on the tire attitude control frame.

[0016] Furthermore, the sensor device includes a three-axis force measuring platform.

[0017] Furthermore, the pavement simulation component includes a simulation base and a pavement simulation flywheel, the pavement simulation flywheel is driven and installed on the simulation base, and the inner hub surface of the pavement simulation flywheel is provided with a pavement for abutting against an aviation tire to simulate a road surface.

[0018] Furthermore, the tire rolling simulation device also includes a loading cylinder, which is directly or indirectly installed on the main load-bearing outer frame of the test bench.

[0019] The present invention also provides an aircraft tire cable test method, characterized in that the above-mentioned aircraft tire cable test equipment is used, and the method comprises:

[0020] S1. Before the test, adjust the tire posture according to the test requirements, and use the reset handle to push the variable-section steel cable to the initial position and keep it in a suspended state;

[0021] S2, controlling the driving surface simulation flywheel to simulate the aircraft speed through the control device, and simulating the ground load of the aircraft tire through the loading cylinder;

[0022] S3. When the rotation speed of the pavement simulation flywheel reaches a predetermined test speed, the aircraft tire under test is pressed onto the inner hub surface of the pavement simulation flywheel for rolling, and finally the vertical loading cylinder presses the aircraft tire onto the inner hub surface of the rotating pavement simulation flywheel;

[0023] S4. The traction assembly on the cable passing device tightens the variable-section steel cable and pulls the variable-section steel cable along the steel cable guide wheel to be rolled over by the tire 23. During the test process, a special sensor is used to measure and collect various relevant parameters and upload them. Under the action of the tension of the variable-section steel cable and the rolling of the aviation tire, the variable-section steel cable is driven, thrown out and pulled to the end position, completing a tire cable passing test.

[0024] Furthermore, the tire posture includes at least a normal posture, a yaw posture and a roll posture.

[0025] The present invention takes the tire usage conditions into consideration and uses a real special steel cable for cable passing, which not only simulates the rolling speed and impact overload of the tire, but also can measure the impact overload size of the tire under the premise of ensuring safety. In addition, the device has tire yaw and roll test functions, and then obtains tire performance through comprehensive analysis, obtains accurate tire test data, helps to improve the quality of the tire and its cable passing performance, obtains first-hand effective data for studying tire characteristics, and provides a reliable basis for improving tire production quality and optimizing tire design. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] Figure 1 It is a three-dimensional structural diagram of the aviation tire cable-passing test equipment in an embodiment of the present invention.

[0027] Figure 2 It is a partial enlarged view of the aviation tire cable testing equipment in an embodiment of the present invention.

[0028] Figure 3 Schematic diagram of the structure of the cable passing device in an embodiment of the present invention.

[0029] Figure 4 It is a schematic diagram of the structure of the cable passing device in an embodiment of the present invention without a partial outer frame.

[0030] in:

[0031] The tire rolling simulation device is 10, the aviation tire is 11, the road surface simulation component is 12, the main load-bearing outer frame of the test bench is 13, the tire attitude control frame is 14, the loading cylinder is 15, the simulation base is 121, and the road surface simulation flywheel is 122;

[0032] The cable passing device is 20, the variable-section steel cable is 21, the traction assembly is 22, the steel cable guide tube is 23, the limit clamp is 24, the follower bracket is 25, the bracket guide ring is 26, the mounting base is 221, the driving cylinder is 222, and the steel cable guide wheel is 223. DETAILED DESCRIPTION

[0033] In order to make the purpose, technical solution and advantages of the implementation mode of the present application clearer, the technical solution in the implementation mode of the present application will be clearly and completely described below in conjunction with the drawings in the implementation mode of the present application. The described implementation mode is a part of the implementation mode of the present application, not all the implementation modes.

[0034] Therefore, the following detailed description of the embodiments of the present application provided in the accompanying drawings is not intended to limit the scope of the present application for protection, but merely represents the selected embodiments of the present application. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in the field without creative work are within the scope of protection of the present application.

[0035] Embodiment 1

[0036] Figure 1 It shows a three-dimensional structural diagram of the cable-passing test equipment of the aviation tire 11 in this embodiment; Figure 2 A partial enlarged view of the cable-passing test equipment for the aircraft tire 11 in this embodiment is shown; Figure 3 The structure diagram of the cable passing device 20 in this embodiment is shown;

[0037] Figure 4 A schematic structural diagram of the cable passing device 20 in an embodiment of the present invention is shown with a partial outer frame removed.

[0038] It is worth noting that Figure 1-4 , the variable cross-section steel cable 21 is in the initial position and the final position, wherein the variable cross-section steel cable 21 is in the initial position when it is not in contact with the aircraft tire 11, that is, the variable cross-section steel cable 21 is in the initial position when it is in the extended state. The variable cross-section steel cable 21 is in the final position when it is in contact with the limit clamp 24 after being rolled by the tire, that is, the variable cross-section steel cable 21 is in the final position when it is in the stored state.

[0039] like Figure 1-4As shown, this embodiment provides an aviation tire 11 cable-passing test equipment, which is mainly used for cable-passing tests on the wheels of carrier-based aircraft, namely, the aviation tire 11 in the text. Specifically, in the aviation field, wheel cable-passing is one of the important dynamic tests that must be conducted to verify the quality, performance and life of the aviation tire 11, and it is also an important guarantee for ensuring the safety of cable-passing and taxiing of carrier-based aircraft. At present, there is no special tire dynamic cable-passing test equipment in China. The common method is to press the tire on a steel pipe for static loading, so as to obtain simple test results and data, but it is impossible to fully and correctly evaluate the quality and life of the tire.

[0040] The cable-passing test equipment for the aircraft tire 11 in this embodiment arranges multiple test components, conducts tests under conditions that truly simulate the use conditions, and collects test data during the test, and finally completes the wheel cable-passing test. Specifically, the cable-passing test equipment for the aircraft tire 11 in this embodiment specifically includes a tire rolling simulation device 10, a sensor test device, a control device, and a cable-passing device 20.

[0041] The tire rolling simulation device 10 includes an aircraft tire 11 and a pavement simulation component 12. The aircraft tire 11 is a wheel for an aircraft. In this embodiment, the aircraft tire 11 is simulated by the pavement simulation component 12 to perform wheel sliding simulation, and finally simulates the rolling speed and inertia force of the wheel during normal use. The pavement simulation component 12 drives and controls the pavement simulation flywheel 122 through a control device. Through the rolling of the flywheel, a runway surface is formed on the inner side surface. After contacting the aircraft tire 11, it drives the aircraft tire 11 to roll, simulating a real scene of an aircraft landing. The tire rolling simulation device 10 obtains a real simulation environment through the pavement simulation component 12, and is used as a simulation device in the test equipment to drive the aircraft tire 11 to roll and provide a simulated scene of the aircraft tire 11 rolling on the pavement.

[0042] The sensor test device includes a sensor device, which includes a variety of dedicated sensors for measuring various relevant parameters of the aircraft tire 11 during the test and uploading the parameter records, wherein the sensor device is connected to the aircraft tire 11 for sensing and collecting various test data of the aircraft tire 11 during the cable passing process. On the other hand, the control device in this embodiment is mainly used to control the test process, collect test data, and complete the information exchange between the test equipment and the test personnel.

[0043] The key point is that after simulating the real scene of the tire, the test equipment of this embodiment performs the tire cable passing test through the cable passing device 20. Specifically, the cable passing device includes a variable-section steel cable 21 and a traction assembly 22. The variable-section steel cable 21 is used to contact the aircraft tire 11 to achieve cable passing, and the traction assembly 22 is used to pull the variable-section steel cable 21. During the cable passing test, the traction assembly 22 pulls the variable-section steel cable 21 from the initial position to the terminal position, and contacts and rolls with the aircraft tire 11 to complete the tire cable passing test.

[0044] In order to provide a better operating experience, a specific test process of the cable passing device is provided. Before the test, the tire posture is adjusted according to the test requirements, and the variable-section steel cable 21 is set at the preset initial position. The pavement simulation component 12 is controlled by the control device to simulate the aircraft speed and control the ground load between the aircraft tire 11 and the pavement. After reaching the predetermined test speed, the test aircraft tire 11 is pressed at the corresponding position for rolling, and then the variable-section steel cable 21 is pulled by the cable passing device 20 to pass through the aircraft tire 11 and roll to the terminal position to complete the test. During the test, a dedicated sensor is used to measure various related parameters. In multiple tests, the above process is repeated according to different tire state parameters to complete the cable passing test, and the overload, acceleration and surface damage of the tire during the cable passing process are obtained. The impact of the tire cable passing characteristics is evaluated through data analysis, and a test basis is provided for various improvements and optimization designs for improving tire quality and its characteristic parameters.

[0045] The advantage of this embodiment is that, from the perspective of tire usage conditions, a real special steel cable is used for cable passing, which not only simulates the rolling speed and impact overload of the tire, but also can measure the impact overload size of the tire under the premise of ensuring safety. In addition, the device has tire yaw and roll test functions, and then the tire performance is obtained through comprehensive analysis, and accurate tire test data is obtained, which helps to improve the quality of the tire and its cable passing performance, obtains first-hand effective data for studying tire characteristics, and provides a reliable basis for improving tire production quality and optimizing tire design.

[0046] Embodiment 2

[0047] The present embodiment provides a cable-passing test device for an aviation tire 11, comprising a tire rolling simulation device 10, comprising an aviation tire 11 and a pavement simulation component 12, for driving the aviation tire 11 to roll and providing a simulation scene of the aviation tire 11 rolling on the pavement; a sensing test device, comprising a sensor device, the sensor device is connected to the aviation tire 11, and is used to obtain various test data of the aviation tire 11 during the cable-passing process; a control device, for controlling the cable-passing test process of the aviation tire 11 and collecting the test data; and a cable-passing device 20, comprising a variable-section steel cable 21 and a traction component 22, during the cable-passing test process, the traction component 22 tractions the variable-section steel cable 21 from an initial position to an end position, and contacts and rolls with the aviation tire 11 to complete the tire cable-passing test.

[0048] The difference between this embodiment and the first embodiment is that this embodiment also provides the following specific implementation methods. Please refer to the following contents together Figure 1-4 .

[0049] In terms of the cable passing device 20, as a preferred embodiment of the present invention, the cable passing device 20 further includes a steel cable guide tube 23, a limit clamp 24, a follower bracket 25 and a bracket guide ring 26. In addition, the traction assembly 22 includes a mounting base 221, a driving cylinder 222 and a steel cable guide wheel 223. The functions of each component are introduced as follows: the steel cable guide tube 23 is mainly used to guide the variable-section steel cable 21. It is fixedly mounted on the mounting base 221. When the traction assembly 22 pulls the variable-section steel cable 21 back to the end position, it guides the variable-section steel cable 21. The limit clamp 24 is used to determine the end position of the variable-section steel cable 21. At the same time, the function of the follower bracket 25 is to facilitate the operator to adjust the position of the variable-section steel cable 21. One end of the follower bracket 25 is sleeved on the steel cable, and the other end is provided with a reset handle. The operator adjusts the position of the variable-section steel cable 21 through the reset handle, for example, resetting the variable-section steel cable 21 to the starting position after completing a test. The bracket guide ring 26 is used to guide the follower bracket 25. Since the follower bracket 25 will move with the variable-section steel cable 21 when the variable-section steel cable 21 is pulled back, the bracket guide ring 26 is used to effectively guide it.

[0050] In the traction assembly 22, the mounting base 221 provides a mounting platform, such as Figure 3-4 As shown, it includes a base and a protective outer frame above the base, and other components of the cable passing device 20 are directly or indirectly mounted on the mounting base 221. Among them, the driving cylinder 222 is controlled by the control device and is used to pull the variable-section steel cable 21. The steel cable guide wheel 223 also plays a guiding role. One end of the variable-section steel cable 21 is used to test contact with the aircraft tire 11, and the other end is connected to the driving cylinder 222 through the steel cable guide wheel 223.

[0051] In terms of connection, the traction cable guide tube 23 and the limit clamp 24 are both arranged on the traction assembly 22, specifically, on the outer frame above the mounting base 221. The retracted end of the variable-section steel cable 21 is limitedly inserted into the cable guide tube 23. The cable guide tube 23 is arranged on both sides of the limit clamp 24. The limit clamp 24 is used to limit the variable-section steel cable 21 after traction and retraction at the end position. More specifically, the bracket guide ring 26 in the cable passing device 20 is arranged on both sides of the limit clamp 24. The bracket ring sleeve of the follower bracket 25 is arranged on the variable-section steel cable 21. The rod sliding limit is arranged on the bracket guide ring 26, and is driven and retracted with the traction and retraction of the variable-section steel cable 21; the other end of the follower bracket 25 is provided with a reset handle for adjusting the position of the steel cable. In terms of the traction assembly 22, the driving cylinder 222 is installed on the mounting base 221, and is connected to the traction drive of the variable-section steel cable 21 through the cable guide wheel 223. As a preferred embodiment, the driving cylinder 222 is rotatably arranged at an angle adjustable on the mounting base 221 , and the driving cylinder 222 is adjusted at a relative angle on the mounting base 221 according to the angle of the variable-section steel cable 21 .

[0052] See also Figure 1-2 In terms of the tire rolling simulation device 10, the tire rolling simulation device 10 in this embodiment also includes a main load-bearing outer frame 13 of the test bench and a tire attitude control frame 14, wherein the main load-bearing outer frame 13 of the test bench is the main load-bearing platform of the entire test equipment, and each device is directly or indirectly connected to the main load-bearing outer frame 13 of the test bench, so as to be stably fixed on the ground or workbench in the working area. The tire attitude control frame 14 is installed on the main load-bearing outer frame 13 of the test bench, which is mainly used to connect with the attitude control of the aircraft tire 11, and is used to adjust the position and attitude of the aircraft tire 11 to meet the test requirements, wherein the tire attitude at least includes normal attitude, yaw attitude and roll attitude. In some embodiments, the sensor equipment can be set on the attitude control frame of the aircraft tire 11, and data of the aircraft tire 11 is collected. In some embodiments, the sensor equipment includes a three-axis force measuring platform.

[0053] See also Figure 1-2 In terms of the road simulation component, as a preferred embodiment of the present invention, the pavement simulation component 12 includes a simulation base 121 and a pavement simulation flywheel 122. The pavement simulation flywheel 122 is driven and mounted on the simulation base 121, and the inner hub surface of the pavement simulation flywheel 122 is provided with a pavement surface for contacting with the aircraft tire 11 to simulate the road surface. The tire rolling simulation device 10 also includes a loading cylinder 15, which is directly or indirectly mounted on the main load-bearing outer frame 13 of the test bench. The loading cylinder 15 is mainly used to adjust the contact force between the aircraft tire 11 and the inner hub surface of the pavement simulation flywheel 122, thereby simulating the landing impact force of the aircraft.

[0054] Embodiment 3

[0055] This embodiment provides an aircraft tire cable test method. The test method uses the aircraft tire cable test equipment in the first or second embodiment to perform an aircraft tire cable test. The specific test method includes the following steps:

[0056] S1. Before the test, adjust the tire posture according to the test requirements, and use the reset handle to push the variable-section steel cable to the initial position and keep it in a suspended state;

[0057] S2, controlling the driving surface simulation flywheel to simulate the aircraft speed through the control device, and simulating the ground load of the aircraft tire through the loading cylinder;

[0058] S3. When the rotation speed of the pavement simulation flywheel reaches a predetermined test speed, the aircraft tire under test is pressed onto the inner hub surface of the pavement simulation flywheel for rolling, and finally the vertical loading cylinder presses the aircraft tire onto the inner hub surface of the rotating pavement simulation flywheel;

[0059] S4. The traction component on the cable passing device tightens the variable-section steel cable and pulls the variable-section steel cable along the steel cable guide wheel to pass through the tire rolling. During the test, a special sensor is used to measure and collect various relevant parameters and upload them. Under the action of the tension of the variable-section steel cable and the rolling of the aviation tire, the variable-section steel cable is driven, thrown out and pulled to the end position, completing a tire cable passing test.

[0060] Preferably, the tire posture includes at least a normal posture, a yaw posture and a roll posture.

[0061] The test method of this embodiment fully takes the tire usage conditions into consideration, can simulate the rolling speed and impact overload of the tire, can accurately measure the impact overload size of the tire, and the device has tire yaw and roll test functions, and then obtains tire performance through comprehensive analysis, obtains accurate tire test data, helps to improve the quality of the tire and its cable passing performance, obtains first-hand effective data for studying tire characteristics, and provides a reliable basis for improving tire production quality and optimizing tire design.

[0062] In the description of the present application, it should be understood that the terms indicating orientation or positional relationship are based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present application.

[0063] In this application, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", "fixed" and the like should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0064] In the description of the present application, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. indicate positions or positional relationships based on the positions or positional relationships shown in the accompanying drawings, or the positions or positional relationships in which the product of the application is usually placed when in use. They are only for the convenience of describing the present application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific position, be constructed and operated in a specific position, and therefore cannot be understood as a limitation on the present application. In addition, the terms "first", "second", "third", etc. are only used to distinguish the description, and cannot be understood as indicating or implying relative importance.

[0065] In addition, the terms "horizontal", "vertical", "overhanging" and the like do not mean that the components are required to be absolutely horizontal or overhanging, but can be slightly tilted. For example, "horizontal" only means that its direction is more horizontal than "vertical", and does not mean that the structure must be completely horizontal, but can be slightly tilted.

[0066] In the present application, unless otherwise clearly specified and limited, a first feature being above or below a second feature may include the first and second features being in direct contact, or may include the first and second features not being in direct contact but being in contact through another feature between them. Moreover, a first feature being above, above, and above a second feature includes the first feature being directly above and obliquely above the second feature, or simply means that the first feature is higher in level than the second feature. A first feature being below, below, and below a second feature includes the first feature being directly below and obliquely below the second feature, or simply means that the first feature is lower in level than the second feature.

[0067] Although the description of the present application is carried out in conjunction with the above specific embodiments, it is obvious that those skilled in the art can make many substitutions, modifications and changes according to the above content. Therefore, all such substitutions, improvements and changes are included in the spirit and scope of the appended claims.

Claims

1. An aviation tire cable test equipment, characterized in that: include: A tire rolling simulation device, including an aircraft tire and a pavement simulation component, is used to drive the aircraft tire to roll and provide a simulation scene of the aircraft tire rolling on the pavement; A sensor test device, including a sensor device, wherein the sensor device is connected to the aircraft tire for sensing and is used to obtain various test data of the aircraft tire during the cable passing process; A control device, used to control the aircraft tire cable test process and collect test data; as well as The cable passing device includes a variable-section steel cable and a traction assembly. During the cable passing test, the traction assembly pulls the variable-section steel cable from an initial position to an end position, and contacts and rolls with the aviation tire to complete the tire cable passing test.

2. The aircraft tire cable test equipment according to claim 1, characterized in that: The cable passing device also includes a steel cable guide tube and a limit clamp; the steel cable guide tube and the limit clamp are arranged on the traction assembly, the gathered end of the variable-section steel cable is limitedly passed through the steel cable guide tube, the steel cable guide tube is arranged on both sides of the limit clamp, and the limit clamp is used to limit the variable-section steel cable after traction and gathering at the end position.

3. The aircraft tire cable test equipment according to claim 2, characterized in that: The cable passing device also includes a follower bracket and a bracket guide ring; the bracket guide ring is arranged on both sides of the limit clamp; the bracket ring of the follower bracket is sleeved on the variable-section steel cable, and the rod sliding limit is arranged on the bracket guide ring, and is transmitted and retracted as the variable-section steel cable is pulled and retracted; the other end of the follower bracket is provided with a reset handle for adjusting the position of the steel cable.

4. The aircraft tire cable test equipment according to claim 1, characterized in that: The traction assembly comprises a mounting base, a driving oil cylinder and a steel cable guide wheel. The driving oil cylinder is mounted on the mounting base and is connected to the variable-section steel cable traction drive through the steel cable guide wheel.

5. The aircraft tire cable test equipment according to claim 4, characterized in that: The driving cylinder is rotatably arranged at an angle adjustable on the mounting base, and the driving cylinder is adjusted at a relative angle on the mounting base according to the angle of the variable-section steel cable.

6. The aircraft tire cable test equipment according to claim 1, characterized in that: The tire rolling simulation device also includes a main load-bearing outer frame of the test bench and a tire attitude control frame. The tire attitude control frame is installed on the main load-bearing outer frame of the test bench and is connected to the tire attitude control frame for adjusting the position and attitude of the aircraft tire. The sensor device is arranged on the tire attitude control frame.

7. The aircraft tire cable test equipment according to claim 6, characterized in that: The sensor device includes a three-axis force measuring platform.

8. The aircraft tire cable test equipment according to any one of claims 1 to 7, characterized in that: The road surface simulation component includes a simulation base and a road surface simulation flywheel. The road surface simulation flywheel is driven and installed on the simulation base, and the inner hub surface of the road surface simulation flywheel is provided with a road surface for abutting against an aviation tire to simulate a road surface.

9. The aircraft tire cable test equipment according to claim 6, characterized in that: The tire rolling simulation device also includes a loading cylinder, which is directly or indirectly installed on the main load-bearing outer frame of the test bench.

10. A method for testing the cable passing of an aviation tire, characterized in that: Using the aviation tire cable test equipment according to any one of claims 1 to 9, the method comprises: S1. Before the test, adjust the tire posture according to the test requirements, and use the reset handle to push the variable-section steel cable to the initial position and keep it in a suspended state; S2, controlling the driving surface simulation flywheel to simulate the aircraft speed through the control device, and simulating the ground load of the aircraft tire through the loading cylinder; S3. When the rotation speed of the pavement simulation flywheel reaches a predetermined test speed, the aircraft tire under test is pressed onto the inner hub surface of the pavement simulation flywheel for rolling, and finally the vertical loading cylinder presses the aircraft tire onto the inner hub surface of the rotating pavement simulation flywheel; S4. The traction assembly on the cable passing device tightens the variable-section steel cable and pulls the variable-section steel cable along the steel cable guide wheel to pass through the tire rolling. During the test, a special sensor is used to measure and collect various relevant parameters and upload them. The variable-section steel cable is driven by the aviation tire rolling, thrown out and pulled to the end position, completing a tire cable passing test.

11. The aircraft tire cable test method according to claim 10, characterized in that: The tire posture includes at least a normal posture, a yaw posture and a roll posture.

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