Wheel brake monitoring system and method

Abstract

The invention discloses a wheel brake monitoring system and method, wherein the monitoring system includes a basic platform, an operation management layer, a business layer, and a presentation layer; the basic platform is provided with a wheel brake database; the operation management layer includes a number of information processing modules, each of which obtains the wheel brake information corresponding to its module from the wheel brake database, and displays it visually on the wheel brake information summary page of the business layer after aggregation; the business layer is used to query or add wheel brake information, and update the added information to the wheel brake database; the presentation layer is divided into a PC terminal and a mobile terminal, both of which are accessible to users. The monitoring system of the invention can digitally record and monitor wheel damage, tire pressure, and remaining brake life, identify airports with high puncture rates, formulate corresponding control measures, monitor tire leakage rates, identify abnormally short brake life, and prevent unsafe incidents of tire blowouts caused by wheel brake system failures.

Description

Technical Field

[0001] The present invention relates to the technical field of aircraft wheel maintenance, and in particular to an aircraft wheel brake monitoring system and method. Background Art

[0002] As an important component of the aircraft landing gear, aircraft wheels support and reduce shock when the aircraft is parked, taxied, taking off or landing. For damage that does not exceed the standard, if there is no effective monitoring, it is easy for the damage to worsen or even exceed the standard but not be discovered in time. Repeated confirmation of damage during route operation is likely to cause flight delays and economic losses. If the wheel has excessive damage, it is very easy to cause tire blowouts, air leaks, etc. If these situations occur when the aircraft is taxiing at high speed, it will seriously affect flight safety, and at best, it will run off the runway, and at worst, the aircraft will be destroyed and people will die. At present, most airlines use oil-based markers to directly mark the tire side corresponding to the damaged part of the tire when monitoring aircraft wheel damage.

[0003] Regarding tire pressure, many airlines do not have the option of installing tire pressure sensors, and the tire pressure values ​​obtained during tire pressure measurement are recorded on paper work cards.

[0004] Regarding the remaining life of the brakes, there are only brake indicator pins on the aircraft, but no sensors. The remaining length of the brake indicator pins measured during the inspection (indicating the remaining life) is also only recorded on the paper work card.

[0005] Disadvantages of existing technology:

[0006] 1. Use an oil-based marker pen to mark the wheel directly. As the wheel wears more or the side wears, the mark will be lost easily.

[0007] 2. Only by seeing the actual wheel can we determine whether there is any damage record for the wheel.

[0008] 3. Due to the lack of relevant information such as the time and location of the injury, the specific injury size, and the injury standard, it is impossible to further analyze the injury data.

[0009] 4. Regarding tire pressure, many airlines do not have the option of installing tire pressure sensors, and the tire pressure values ​​measured are recorded on paper work cards, which make it impossible to quickly query and perform data analysis to monitor whether the tire has potential failures such as excessive leakage rates.

[0010] 5. Regarding the remaining life of brakes, there are only brake indicator pins on the aircraft, but no sensors. Information such as which brakes currently installed in the fleet are about to reach the replacement threshold, that is, the remaining life is close to zero, cannot be obtained, so it is impossible to extract brake life information for flight adjustments, and replacement may be required during operation, resulting in flight delays.

[0011] In view of this, the inventor has designed a system and method that can digitally record and monitor wheel damage, tire pressure, and remaining brake life. Summary of the invention

[0012] The purpose of the present invention is to provide a wheel brake monitoring system and method. By establishing this system, wheel damage, tire pressure, and remaining brake life can be digitally recorded and monitored, data can be analyzed, and airports with high puncture rates can be identified, so that corresponding management and control measures can be formulated. The leakage rate of tires within a certain period can be monitored, and defective tires can be replaced in advance. The situation of abnormally short brake life can also be identified, thereby identifying potential system failures, preventive troubleshooting to eliminate unsafe incidents such as tire blowouts caused by system failures, and flight adjustments can be made in advance, and brake components with a life close to zero can be replaced in an orderly manner, reducing temporary replacements during operation and avoiding flight delays.

[0013] To achieve the above object, the technical solution adopted by the present invention is:

[0014] Wheel brake monitoring system, including:

[0015] A basic platform, which is provided with a wheel brake database, which stores the wheel brake information recorded on the most recent inspection work card, the wheel brake information including the machine number, model, wheel part number / serial number, current number of use cycles, tire pressure value, brake pin remaining length and wheel damage record; the wheel brake database is associated with an external accessory management system, the machine number, model, wheel part number / serial number, current number of use cycles are captured from the accessory management system, the wheel damage record includes the damage type, damage occurrence time, location, specific damage size, damage mark and verification worker information;

[0016] The operation management layer includes several information processing modules. Each information processing module obtains the wheel brake information corresponding to the module from the wheel brake database, and summarizes and visualizes the information on the wheel brake information summary page of the business layer.

[0017] The business layer is used to query or add tire pressure values, brake pin remaining length and wheel damage records in the wheel brake information, and update the newly added information to the wheel brake database;

[0018] The presentation layer is divided into a PC terminal and a mobile terminal, both of which are accessible to users. The PC terminal is used for users to log in to the system and perform full-authority operations on the business layer and operation management layer, and the mobile terminal is used for users to log in to the system and perform business layer content operations.

[0019] Furthermore, the information processing module includes a wheel damage monitoring module, a tire pressure monitoring module, a brake life monitoring module, a wheel damage statistics module, a tire pressure statistics module, and a brake life statistics module; the wheel damage monitoring module is used to obtain wheel damage records from the wheel brake database in real time and summarize the wheel damage records to obtain the damage number and visualize it on the wheel information summary page of the business layer, and the wheel damage statistics module is used to summarize the wheel damage records and visualize it on the PC page to determine whether the wheel damage exceeds the aircraft route operation limit; the tire pressure monitoring module and the brake life monitoring module are respectively used to obtain the tire pressure value and the brake indicator pin remaining length value from the wheel brake database, and visualize them on the wheel brake information summary page of the business layer, and the tire pressure statistics module and the brake life statistics module are respectively used to summarize the tire pressure and brake indicator pin remaining length data, and visualize them on the PC to determine whether there is a leakage rate exceeding the standard and abnormal brake wear;

[0020] The business layer includes a wheel damage record module, a tire pressure record module, a brake life record module, a wheel damage query module, a tire pressure query module, and a brake life query module; the wheel damage query module is used to retrieve the wheel information summary page to query whether there is a wheel damage record, and the damage record module is used to add or modify a wheel damage record; the tire pressure query module and the brake life query module are respectively used to retrieve the wheel information summary page to query the tire pressure record and the brake life record, and the tire pressure record module and the brake life record module are respectively used to add or modify the tire pressure record and the brake life record, and the newly added or modified wheel damage record, tire pressure record and brake life record are saved to the wheel brake database to update the corresponding data.

[0021] Furthermore, the wheel damage recording module includes a CAD-assisted positioning module, which is used to establish a two-dimensional coordinate model according to different wheels of different models. The model takes the aircraft tire valve core axis as the origin and is marked 360° clockwise at intervals of 10°, and based on the CAD two-dimensional graphics, a tire contour map and a tread expansion map with the aforementioned marking degrees are obtained. The damage mark can be marked once or twice on the tire contour map and the tread expansion map, respectively, to locate the circumferential position and axial position of the damage, respectively. The tire contour map and the tread expansion map with the aforementioned damage mark are linked to the wheel information summary page.

[0022] Furthermore, the mobile terminal includes an AR auxiliary positioning module, which is used to call the camera of the mobile terminal to capture a real-time wheel image and align it with a tire contour map with a circular scale to achieve circumferential auxiliary positioning of wheel damage.

[0023] Furthermore, the wheel damage recording module includes a damage auxiliary judgment module, in which the damage standards corresponding to the tire manufacturer and tire model are pre-recorded in the wheel damage monitoring module. When the damage size is entered in the wheel damage wheel module, the damage auxiliary judgment module compares the entered damage size with the pre-recorded damage standard to determine whether it exceeds the damage standard.

[0024] Furthermore, the PC terminal uses a WEB browser to log in to the system to perform full-authority operations on the business layer and operation management layer content, and the mobile terminal includes an APP that supports the Android or IOS operating system, which is used for users to log in to the system to perform business layer content operations.

[0025] The monitoring method of the above-mentioned wheel brake monitoring system comprises the following steps:

[0026] A1. The user logs in to the system through the PC or mobile terminal, enters the business layer, and checks the number of wheel damage records, current tire pressure, and current brake indicator pin length on the wheel brake information summary page. If the detailed information of the wheel damage record is to be queried, proceed to step A2. If the tire pressure record needs to be changed, proceed to step A5. If the brake indicator pin length needs to be changed, proceed to step A6.

[0027] A2. Click the damage number on the wheel brake information summary page to enter the wheel damage query module. If there is a damage record on the wheel damage query page, go to step A3. If there is no such damage record on the wheel summary page and there is wheel damage in this inspection, go to step A4.

[0028] A3. Enter the corresponding wheel damage record interface to verify whether the damage record is a recorded damage. If it is recorded, the process ends; if it is not recorded, proceed to step A4;

[0029] A4. Enter the wheel damage record module, select and check the corresponding machine number, wheel part number / serial number, tire manufacturer information, damage type, input the time and location of the damage, specific damage size, damage mark information, and complete the wheel damage record;

[0030] A5. Click on the tire pressure on the wheel and brake information summary page to enter the tire pressure query module. If there is no corresponding record or the current tire pressure value is inconsistent with the record, enter the latest tire pressure value;

[0031] A6. Click the brake indicator pin remaining length on the wheel brake information summary page to enter the brake life query module. If there is no corresponding record or the current brake indicator pin remaining length is inconsistent with the record, enter the latest brake indicator pin length value.

[0032] Furthermore, the above monitoring method further comprises the following steps:

[0033] B1. The user logs in to the system through the mobile terminal, enters the business layer, clicks the damage number on the wheel brake information summary page, and enters the wheel damage query module;

[0034] B2. If there is a record of wheel damage, enter the AR auxiliary positioning module, start the camera, and retrieve the tire contour map. By aligning the tire contour map with a circular scale displayed in the camera, rotating the camera, adjusting the lens distance, and aligning the valve core positioning line with the valve core on the wheel entity as the origin, 360° rapid positioning of the damage circumference on the wheel entity can be achieved.

[0035] Furthermore, the step A4 specifically includes:

[0036] A41. Select and check the corresponding machine number, wheel part number / serial number, tire manufacturer information, and damage type;

[0037] A42, enter the CAD auxiliary positioning module, and retrieve the tire contour diagram and tread development diagram of the corresponding aircraft model and wheel;

[0038] A43. If it is sidewall damage, the time, location, specific damage form and damage size information of the damage shall be marked on the side of the tire. If it is tread damage, the time, location, specific damage form and damage size information of the damage shall be marked on the tread expansion diagram. After the aforementioned marked information is verified and confirmed by the verification worker with verification authority, the verification worker information shall be recorded to complete the wheel damage record.

[0039] After adopting the above scheme, the present invention has the following beneficial effects:

[0040] 1. The present invention establishes a wheel brake monitoring system to digitally record and monitor wheel damage. With the establishment of digital records, the data can be analyzed to identify airports with high incidence rates of puncture injuries, thereby formulating corresponding control measures.

[0041] 2. By recording the tire pressure numerically, the system can monitor the tire leakage rate within a certain period of time and replace defective tires in advance.

[0042] 3. By establishing this system, the remaining life of the brakes can be effectively monitored. On the one hand, it can identify situations where the brake life is abnormally short, thereby identifying potential system failures and preventive troubleshooting to eliminate unsafe incidents such as tire blowouts caused by system failures. On the other hand, with the digital monitoring of the remaining life of the brakes, flight adjustments can be made in advance, and brake components with a lifespan close to zero can be replaced in an orderly manner, reducing temporary replacements during operation and avoiding flight delays.

[0043] 4. By establishing a wheel information summary page and accessing the wheel brake database, the tire pressure value and the remaining length of the brake indicator pin and the current condition of the wheel damage on the most recent inspection work card are displayed on the wheel information summary page, which is convenient for line maintenance personnel and crew members to quickly understand the current status of the corresponding wheels of the aircraft. BRIEF DESCRIPTION OF THE DRAWINGS

[0044] Figure 1 It is a structural block diagram of the wheel brake monitoring system of the present invention;

[0045] Figure 2 It is a schematic diagram of the wheel information summary page of the present invention;

[0046] Figure 3 and Figure 4 They are tire profile diagram and tread development diagram based on two-dimensional model respectively;

[0047] Figure 5 This is a schematic diagram of the 360° rapid positioning of damage based on AR;

[0048] Figure 6 The present invention is a flowchart for querying and recording wheel damage. DETAILED DESCRIPTION

[0049] like Figure 1-4 As shown, the present invention discloses a wheel brake monitoring system, including a basic platform, an operation management layer, a business layer, and a presentation layer.

[0050] The above-mentioned basic platform is provided with a wheel brake database, which stores the wheel brake information recorded on the most recent inspection work card. The wheel brake information includes the machine number, model, wheel part number / serial number, current number of cycles, tire pressure value, brake pin remaining length and wheel damage record; the wheel brake database is associated with an external accessory management system, and the machine number, model, wheel part number / serial number, and current number of cycles are captured from the accessory management system. The wheel damage record includes the type of damage, the time and location of the damage, the specific damage size, the damage mark and the information of the checker. The above-mentioned accessory management system is an existing system for recording information such as machine number, model, wheel part number / serial number, etc. and for managing the information of aircraft in-place components. Through the association of the wheel brake database, the system can capture important information such as machine number, model, wheel part number / serial number, etc., thereby providing the basic platform with initial wheel data. The "capturing machine number, model, wheel part number / serial number, and current number of cycles" technology adopted by the present invention is to automatically obtain the above information from the accessory management system through a data interface.

[0051] The above-mentioned operation management layer includes several information processing modules, each of which obtains the wheel brake information corresponding to its module from the wheel brake database, and summarizes and displays it visually on the wheel brake information summary page of the business layer; specifically, the information processing module includes a wheel damage monitoring module, a tire pressure monitoring module, a brake life monitoring module, a wheel damage statistics module, a tire pressure statistics module, and a brake life statistics module; the wheel damage monitoring module is used to obtain wheel damage records from the wheel brake database in real time, summarize the wheel damage records to obtain the damage number, and display it visually on the wheel information summary page of the business layer. The wheel damage statistics module is used to summarize the wheel damage records and visualize them on the PC page to determine whether the wheel damage exceeds the aircraft route operation limit; the tire pressure monitoring module and the brake life monitoring module are used to obtain the tire pressure value and the brake indicator pin remaining length value from the wheel brake database respectively, and visualize them on the wheel brake information summary page of the business layer; the tire pressure statistics module and the brake life statistics module are used to summarize the tire pressure and brake indicator pin remaining length data respectively, and visualize them on the PC to determine whether there is an excessive leakage rate or abnormal brake wear.

[0052] The above-mentioned business layer is used to query or add tire pressure values, remaining length of brake pins and wheel damage records in wheel brake information, and update the newly added information to the wheel brake database, that is, the tire pressure values, remaining length of brake pins and wheel damage records are queried and entered by the wheel maintenance operator in the business layer; specifically, the business layer includes a wheel damage record module, a tire pressure record module, a brake life record module, a wheel damage query module, a tire pressure query module, and a brake life query module; the wheel damage query module is used to retrieve the wheel information summary page to query whether there is a wheel damage record, and the damage record module is used to add or modify the wheel damage record; the tire pressure query module and the brake life query module are respectively used to retrieve the wheel information summary page to query the tire pressure record and the brake life record, and the tire pressure record module and the brake life record module are respectively used to add or modify the tire pressure record and the brake life record, and the newly added or modified wheel damage record, tire pressure record and brake life record are saved to the wheel brake database to update the corresponding data.

[0053] The above presentation layer is divided into a PC terminal and a mobile terminal, both of which are accessible to users. The PC terminal is used for users to log in to the system and perform full-authority operations on the business layer and operation management layer, and the mobile terminal is used for users to log in to the system and perform business layer content operations.

[0054] Furthermore, the above-mentioned wheel damage recording module includes a CAD-assisted positioning module, which is used to establish a two-dimensional coordinate model according to different wheels of different models. The model takes the aircraft tire valve core axis as the origin and is marked 360° clockwise at intervals of 10°, and based on the CAD two-dimensional graphics, a tire contour map and a tread expansion map with the aforementioned marking degrees are obtained. The damage mark can be marked once or twice on the tire contour map and the tread expansion map, respectively, to locate the circumferential position and axial position of the damage, respectively. The tire contour map and the tread expansion map with the aforementioned damage mark are linked to the wheel information summary page. When querying, the damage number on the wheel information summary page can be linked to the tire contour map and the tread expansion map with the aforementioned damage mark.

[0055] Furthermore, the mobile terminal includes an AR auxiliary positioning module, which is used to call the mobile terminal's camera to capture a real-time wheel image and align it with a tire contour map with a circular scale to achieve circumferential auxiliary positioning of wheel damage.

[0056] Furthermore, the above-mentioned wheel damage recording module includes a damage auxiliary judgment module, in which the damage standards corresponding to the tire manufacturer and tire model are pre-recorded in the wheel damage monitoring module. When the damage size is entered in the wheel damage wheel module, the damage auxiliary judgment module compares the entered damage size with the pre-recorded damage standard to determine whether it exceeds the damage standard. If it exceeds the damage standard, it will immediately prompt that the wheel needs to be replaced.

[0057] Furthermore, the PC terminal uses a WEB browser to log in to the system to perform full-authority operations on the business layer and operation management layer content, and the mobile terminal includes an APP that supports the Android or IOS operating system, which is used for users to log in to the system to perform business layer content operations.

[0058] The monitoring system of the present invention has the following advantages:

[0059] 1. The present invention establishes a wheel brake monitoring system to digitally record and monitor wheel damage. With the establishment of digital records, the data can be analyzed to identify airports with high incidence rates of puncture injuries, thereby formulating corresponding control measures.

[0060] 2. By numerically recording the tire pressure, the tire leakage rate within a certain period can be monitored and defective tires can be replaced in advance.

[0061] 3. By establishing this system, the remaining life of the brakes can be effectively monitored. On the one hand, it can identify situations where the brake life is abnormally short, thereby identifying potential system failures and preventive troubleshooting to eliminate unsafe incidents such as tire blowouts caused by system failures. On the other hand, with the digital monitoring of the remaining life of the brakes, flight adjustments can be made in advance, and brake components with a lifespan close to zero can be replaced in an orderly manner, reducing temporary replacements during operation and avoiding flight delays.

[0062] 4. By establishing a wheel information summary page and accessing the wheel brake database, the tire pressure and remaining length of the brake indicator pin on the most recent inspection work card and the current status of the wheel damage are displayed on the wheel information summary page, making it easier for line maintenance personnel and crew members to quickly understand the current status of the corresponding wheels of the aircraft.

[0063] 5. When replacing a wheel, the existing wheel damage defects can be automatically cleared through the wheel brake database, thus achieving closed-loop management of wheel damage disposal.

[0064] like Figure 6 As shown, the present invention also discloses a method for monitoring a wheel brake system, comprising the following steps:

[0065] A1. The user logs in to the system through the PC or mobile terminal, enters the business layer, and checks the number of wheel damage records, current tire pressure, and current brake indicator pin length on the wheel brake information summary page. If the detailed information of the wheel damage record is to be queried, proceed to step A2. If the tire pressure record needs to be changed, proceed to step A5. If the brake indicator pin length needs to be changed, proceed to step A6.

[0066] A2. Click the damage number on the wheel brake information summary page to enter the wheel damage query module. If there is a damage record on the wheel damage query page, go to step A3. If there is no such damage record on the wheel summary page and there is wheel damage in this inspection, go to step A4.

[0067] A3. Enter the corresponding wheel damage record interface to verify whether the damage record is a recorded damage. If it is recorded, the process ends; if it is not recorded, proceed to step A4;

[0068] A4. Enter the wheel damage record module, select and check the corresponding machine number, wheel part number / serial number, tire manufacturer information, damage type, input the time and location of the damage, specific damage size, damage mark information, and complete the wheel damage record;

[0069] A5. Click on the tire pressure on the wheel and brake information summary page to enter the tire pressure query module. If there is no corresponding record or the current tire pressure value is inconsistent with the record, enter the latest tire pressure value;

[0070] A6. Click the brake indicator pin remaining length on the wheel brake information summary page to enter the brake life query module. If there is no corresponding record or the current brake indicator pin remaining length is inconsistent with the record, enter the latest brake indicator pin length value.

[0071] Furthermore, the above monitoring method further comprises the following steps:

[0072] B1. The user logs in to the system through the mobile terminal, enters the business layer, clicks the damage number on the wheel brake information summary page, and enters the wheel damage query module;

[0073] B2. If there is a record of wheel damage, enter the AR auxiliary positioning module, start the camera, and retrieve the tire contour map. By aligning the tire contour map with a circular scale displayed in the camera, rotating the camera, adjusting the lens distance, and aligning the valve core positioning line with the valve core on the wheel entity as the origin, 360° rapid positioning of the damage circumference on the wheel entity can be achieved.

[0074] Furthermore, the above step A4 specifically includes:

[0075] A41. Select and check the corresponding machine number, wheel part number / serial number, tire manufacturer information, and damage type;

[0076] A42, enter the CAD auxiliary positioning module, and retrieve the tire contour diagram and tread development diagram of the corresponding aircraft model and wheel;

[0077] A43. If it is sidewall damage, the time, location, specific damage form and damage size information of the damage shall be marked on the side of the tire. If it is tread damage, the time, location, specific damage form and damage size information of the damage shall be marked on the tread expansion diagram. After the aforementioned marked information is verified and confirmed by the verification worker with verification authority, the verification worker information shall be recorded to complete the wheel damage record.

[0078] The above description is only an implementation example of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions and improvements within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. Wheel brake monitoring system, characterized by include: A basic platform, which is provided with a wheel brake database, which stores the wheel brake information recorded on the most recent inspection work card, the wheel brake information including the machine number, model, wheel part number / serial number, current number of use cycles, tire pressure value, brake pin remaining length and wheel damage record; the wheel brake database is associated with an external accessory management system, the machine number, model, wheel part number / serial number, current number of use cycles are captured from the accessory management system, the wheel damage record includes the damage type, damage occurrence time, location, specific damage size, damage mark and verification worker information; The operation management layer includes several information processing modules. Each information processing module obtains the wheel brake information corresponding to the module from the wheel brake database, and summarizes and visualizes the information on the wheel brake information summary page of the business layer. The business layer is used to query or add tire pressure values, brake pin remaining length and wheel damage records in the wheel brake information, and update the newly added information to the wheel brake database; The presentation layer is divided into a PC terminal and a mobile terminal, both of which are accessible to users. The PC terminal is used for users to log in to the system and perform full-authority operations on the business layer and operation management layer, and the mobile terminal is used for users to log in to the system and perform business layer content operations.

2. The wheel brake monitoring system according to claim 1, characterized in that: The information processing module includes a wheel damage monitoring module, a tire pressure monitoring module, a brake life monitoring module, a wheel damage statistics module, a tire pressure statistics module, and a brake life statistics module; the wheel damage monitoring module is used to obtain wheel damage records from the wheel brake database in real time and summarize the wheel damage records to obtain the damage number and visualize it on the wheel information summary page of the business layer; the wheel damage statistics module is used to summarize the wheel damage records and visualize it on the PC page to determine whether the wheel damage exceeds the aircraft route operation limit; the tire pressure monitoring module and the brake life monitoring module are respectively used to obtain the tire pressure value and the brake indicator pin remaining length value from the wheel brake database, and visualize them on the wheel brake information summary page of the business layer; the tire pressure statistics module and the brake life statistics module are respectively used to summarize the tire pressure and brake indicator pin remaining length data, and visualize them on the PC to determine whether there is a leakage rate exceeding the standard or abnormal brake wear; The business layer includes a wheel damage record module, a tire pressure record module, a brake life record module, a wheel damage query module, a tire pressure query module, and a brake life query module; the wheel damage query module is used to retrieve the wheel information summary page to query whether there is a wheel damage record, and the damage record module is used to add or modify a wheel damage record; the tire pressure query module and the brake life query module are respectively used to retrieve the wheel information summary page to query the tire pressure record and the brake life record, and the tire pressure record module and the brake life record module are respectively used to add or modify the tire pressure record and the brake life record, and the newly added or modified wheel damage record, tire pressure record and brake life record are saved to the wheel brake database to update the corresponding data.

3. The wheel brake monitoring system according to claim 2, characterized in that: The wheel damage recording module includes a CAD-assisted positioning module, which is used to establish a two-dimensional coordinate model according to different wheels of different models. The model takes the aircraft tire valve core axis as the origin and is marked 360° clockwise at intervals of 10°. Based on the CAD two-dimensional graphics, a tire contour map and a tread expansion map with the aforementioned marking degrees are obtained. The damage mark can be marked once or twice on the tire contour map and the tread expansion map, respectively, to locate the circumferential position and axial position of the damage, respectively. The tire contour map and the tread expansion map with the aforementioned damage mark are linked to the wheel information summary page.

4. The wheel brake monitoring system according to claim 1, characterized in that: The mobile terminal includes an AR auxiliary positioning module, which is used to call the camera of the mobile terminal to capture a real-time wheel image and align it with a tire contour map with a circular scale to achieve circumferential auxiliary positioning of wheel damage.

5. The wheel brake monitoring system according to claim 2, characterized in that: The wheel damage recording module includes a damage auxiliary judgment module. The damage standards corresponding to the tire manufacturer and tire model are pre-recorded in the wheel damage monitoring module. When the damage size is entered in the wheel damage wheel module, the damage auxiliary judgment module compares the entered damage size with the pre-recorded damage standard to determine whether it exceeds the damage standard.

6. The wheel brake monitoring system according to claim 1, characterized in that: The PC terminal uses a WEB browser to log in to the system to perform full-authority operations on the business layer and operation management layer content. The mobile terminal includes an APP that supports the Android or IOS operating system, which is used for users to log in to the system to perform business layer content operations.

7. A monitoring method for a wheel brake monitoring system, characterized in that The following steps are involved: A1. The user logs in to the system through the PC or mobile terminal, enters the business layer, and checks the number of wheel damage records, current tire pressure, and current brake indicator pin length on the wheel brake information summary page. If the detailed information of the wheel damage record is to be queried, proceed to step A2. If the tire pressure record needs to be changed, proceed to step A5. If the brake indicator pin length needs to be changed, proceed to step A6. A2. Click the damage number on the wheel brake information summary page to enter the wheel damage query module. If there is a damage record on the wheel damage query page, go to step A3. If there is no such damage record on the wheel summary page and there is wheel damage in this inspection, go to step A4. A3. Enter the corresponding wheel damage record interface to verify whether the damage record is a recorded damage. If it is recorded, the process ends; if it is not recorded, proceed to step A4; A4. Enter the wheel damage record module, select and check the corresponding machine number, wheel part number / serial number, tire manufacturer information, damage type, input the time and location of the damage, specific damage size, damage mark information, and complete the wheel damage record; A5. Click on the tire pressure on the wheel and brake information summary page to enter the tire pressure query module. If there is no corresponding record or the current tire pressure value is inconsistent with the record, enter the latest tire pressure value; A6. Click the brake indicator pin remaining length on the wheel brake information summary page to enter the brake life query module. If there is no corresponding record or the current brake indicator pin remaining length is inconsistent with the record, enter the latest brake indicator pin length value.

8. The monitoring method of the wheel brake monitoring system according to claim 7, characterized in that The monitoring method further comprises the following steps: B1. The user logs in to the system through the mobile terminal, enters the business layer, clicks the damage number on the wheel brake information summary page, and enters the wheel damage query module; B2. If there is a record of wheel damage, enter the AR auxiliary positioning module, start the camera, and retrieve the tire contour map. By aligning the tire contour map with a circular scale displayed in the camera, rotating the camera, adjusting the lens distance, and aligning the valve core positioning line with the valve core on the wheel entity as the origin, 360° rapid positioning of the damage circumference on the wheel entity can be achieved.

9. The monitoring method of the wheel brake monitoring system according to claim 7, characterized in that: The step A4 specifically includes: A41. Select and check the corresponding machine number, wheel part number / serial number, tire manufacturer information, and damage type; A42, enter the CAD auxiliary positioning module, and retrieve the tire contour diagram and tread development diagram of the corresponding aircraft model and wheel; A43. If it is sidewall damage, the time, location, specific damage form and damage size information of the damage shall be marked on the side of the tire. If it is tread damage, the time, location, specific damage form and damage size information of the damage shall be marked on the tread expansion diagram. After the aforementioned marked information is verified and confirmed by the verification worker with verification authority, the verification worker information shall be recorded to complete the wheel damage record.

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