Fault visualization system based on maintenance three-dimensional technology and analysis method thereof
By adopting a fault visualization system based on three-dimensional maintenance process in the field of aircraft maintenance, and using lightweight digital-analog explicitization to display the fault location and distribution rules, the problem of low efficiency in fault information transmission in the existing technology is solved, and the rapid accuracy of fault analysis and traceable fault data management throughout the process is achieved.
Patent Information
- Application Number
- CN202411989147.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-31
- Publication Date
- 2025-06-03
AI Technical Summary
In the field of aircraft maintenance, it is difficult for the existing technology to effectively demonstrate the fault location and distribution rules, resulting in low efficiency in transmission of fault information, and it is difficult for technicians to quickly and accurately analyze the causes of the fault and modify the process plan.
The fault visualization system based on maintenance three-dimensional process is adopted, and the design digital-analog is imported through the data reception module, the process management module manages the three-dimensional process information, and the three-dimensional process editing module edits the three-dimensional process. The fault registration module completes the fault registration, generates lightweight digital-analog and locates the fault points on the digital-analog, summarizes and manages the fault data and triggers the fault analysis process, and provides a fault solution.
By lightweight digital-analog, it demonstrates the fault location and distribution rules, improves the communication efficiency of the fault information transmission process, helps technicians quickly and accurately analyze the causes of the fault and realizes traceable fault data management throughout the process.
Smart Images

Figure CN120087938A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the field of aircraft maintenance technology, and particularly to a fault visualization system based on maintenance three-dimensional technology and an analysis method thereof. Background Art
[0002] In the field of aircraft maintenance, during the fault inspection process, it is necessary to register fault data on the work card and transfer it to the maintenance process for implementation. When a certain number of faults accumulate, technicians need to analyze and summarize the common fault causes to improve the process plan. Since the method of text description cannot visually display the fault location, the communication efficiency in the information transfer process is not high; the fault distribution law cannot be visually displayed, resulting in technicians being unable to quickly and accurately analyze the reasons and modify the process plan. With the popularization of three-dimensional technology in the field of aircraft maintenance, fault data is registered based on three-dimensional technology on mobile terminals, and the statistical display of fault data on the digital model is realized on the computer side, realizing the full-process traceable management of aircraft fault data initiation, analysis, approval, and closed-loop.
[0003] Chinese invention patent CN104517011A (publication date: April 15, 2015) discloses a method for visualizing faults of product components based on a 3D digital model, which has four major steps, including product three-dimensional model conversion, unit-level fault information visualization design, component-level fault information visualization design, and fault monitoring process based on the visualization model. The disadvantage is that this method does not have a method for generating fault solutions.
[0004] Chinese invention patent CN108462323A (publication date: August 28, 2018) discloses a fault visualization motor and a fault visualization method thereof. Through this method, maintenance personnel can determine the fault location according to the displayed operating parameter values when the motor fails. It does not involve the field of aircraft maintenance and is only applicable to motor products. Summary of the Invention
[0005] In order to solve the above problems, the present invention proposes a fault visualization system based on maintenance three-dimensional technology and an analysis method thereof.
[0006] A fault visualization system based on maintenance three-dimensional technology includes:
[0007] A data receiving module for importing the digital model designed by the design;
[0008] A process management module for managing three-dimensional process information, triggering the fault analysis process through fault analysis, and providing fault solutions;
[0009] A three-dimensional process editing module for editing three-dimensional processes;
[0010] A fault registration module for completing fault registration;
[0011] Other expansion modules to complete the extended application of lightweight digital models.
[0012] The data receiving module includes functions such as digital model lightweighting and design information extraction.
[0013] The data receiving module generates a lightweight digital model by calling a lightweight converter, extracts the design information in the digital model at the same time, and stores the above content in the process management module.
[0014] The process management module includes functions such as three-dimensional lightweight digital model management, three-dimensional process management, three-dimensional fault data management, three-dimensional process resource management, and three-dimensional lightweight digital model reader.
[0015] The process management module browses the stored three-dimensional lightweight digital model and three-dimensional processes by calling a three-dimensional lightweight digital model reader.
[0016] The three-dimensional process editing module triggers a three-dimensional process editor through the process management module, sends the lightweight digital model and three-dimensional process resources in the process management module to the three-dimensional process editor. After completion of editing, a three-dimensional process animation model is generated and returned to the process management module for storage and management.
[0017] The fault registration module calls a three-dimensional lightweight model reader to view the three-dimensional process animation model through an interactive electronic manual.
[0018] If fault registration is required, call the three-dimensional process editor, mark the fault at the same position with reference to the digital model, return the three-dimensional model with fault markings to the three-dimensional process management module, and view the fault summary display on the digital model through a three-dimensional lightweight model reader.
[0019] An analysis method for a fault visualization system based on maintenance three-dimensional processes is as follows:
[0020] S1. Initiate fault entry: When the fault inspection personnel perform the fault inspection process, initiate the fault entry process through a mobile terminal;
[0021] S2. Obtain fault information: The flight number, process, and basic part information are automatically obtained and imported into the fault entry process by the interactive electronic manual, and the detailed information such as fault mode and fault description is registered by the fault inspection personnel;
[0022] S3. Locate the fault point on the model: Through means such as rotation and sectioning, accurately locate the fault point on the digital model and mark the geometric position;
[0023] S4. Fault data management: Transmit the mobile terminal data to the computer terminal, accumulate the single-aircraft fault data on the aircraft type digital model for summary management, and trigger the fault analysis process at the same time;
[0024] S5. Generate a fault solution: Observe whether to initiate a fault analysis process;
[0025] S6. Use of the fault solution: Enter the single - machine fault solution into the fault knowledge base for subsequent fault solution recommendation, and at the same time send the solution to the production department for scheduling construction.
[0026] In step S5 described above, when initiating a fault analysis process, the fault is sent to the name of the technician, and the technician analyzes the fault and formulates a single - machine fault solution; if the fault analysis process is not initiated, the fault information is matched with the fault knowledge base. If the match is successful, the model - type fault solution is used as the solution to this fault. If the match is unsuccessful, the technician completes the formulation of the single - machine fault solution.
[0027] The beneficial effects of the present invention are as follows: By using lightweight digital models to solve the problem that text descriptions cannot explicitly display the fault location, it is used in the aircraft maintenance fault inspection link, effectively improving the communication efficiency in the process of fault information transmission. By summarizing faults through digital models and explicitly displaying the fault distribution law, it is beneficial for technicians to analyze the fault law based on historical faults, realizing the fully traceable management of the entire process of aircraft fault data initiation, analysis, approval, and closed - loop. Brief Description of the Drawings
[0028] The present invention will be further described below in conjunction with the drawings and embodiments.
[0029] Figure 1 is the system structure schematic diagram of the present invention;
[0030] Figure 2 is the process schematic diagram of the present invention. Detailed Embodiments
[0031] In order to make the technical means, creative features, achieved purposes, and effects of the present invention easy to understand, the present invention will be further elaborated below.
[0032] As Figures 1 to 2 shown, a fault visualization system based on maintenance three - dimensional processes includes:
[0033] A data receiving module for importing the digital models designed by the design department;
[0034] A process management module for managing three - dimensional process information, triggering and completing a fault analysis process through fault analysis, and providing a fault solution;
[0035] A three - dimensional process editing module for editing three - dimensional processes;
[0036] A fault registration module for completing fault registration;
[0037] Other extended modules to complete the extended application of lightweight digital models.
[0038] The data receiving module includes functions such as digital model lightweighting and design information extraction.
[0039] The data receiving module generates a lightweight digital model by calling a lightweight converter, extracts the design information in the digital model at the same time, and stores the above content in the process management module.
[0040] The process management module includes functions such as three-dimensional lightweight digital model management, three-dimensional process management, three-dimensional fault data management, three-dimensional process resource management, and three-dimensional lightweight digital model reader. It solves the problem that the fault location cannot be explicitly shown by text description through the lightweight digital model, and is used in the aircraft maintenance fault inspection link to effectively improve the communication efficiency in the process of fault information transmission. By summarizing faults through digital models and explicitly displaying the fault distribution law, it is beneficial for technicians to analyze fault laws based on historical faults, and realize the full-process traceable management of the initiation, analysis, approval, and closed-loop of aircraft fault data.
[0041] The process management module browses the stored three-dimensional lightweight digital model and three-dimensional processes by calling a three-dimensional lightweight digital model reader, and connects the integrated process from digital model reception, process editing to fault registration; realizes the full-process traceable management of the initiation, analysis, approval, and closed-loop of aircraft fault data.
[0042] The three-dimensional process editing module triggers a three-dimensional process editor through the process management module, sends the lightweight digital model and three-dimensional process resources in the process management module to the three-dimensional process editor, generates a three-dimensional process animation model after completion of editing, and returns it to the process management module for storage and management, realizing the fine-grained association of new fault information with the three-dimensional model, facilitating data statistical analysis; realizing the establishment of a matching model between new faults and historical faults, quickly recommending historical solutions, and providing a process for improving the fault knowledge base.
[0043] The fault registration module calls a three-dimensional lightweight model reader through an interactive electronic manual to view the three-dimensional process animation model.
[0044] If fault registration is required, call the three-dimensional process editor, mark the fault at the same position with reference to the digital model, return the three-dimensional model with fault marks to the three-dimensional process management module, and view the fault summary display on the digital model through a three-dimensional lightweight model reader. Data transmission between the classified network and the industrial control network is carried out through data ferry.
[0045] The other extended modules complete the application by calling the three-dimensional lightweight digital model to other systems, such as digital twin applications, production progress display applications, etc.
[0046] An analysis method of a fault visualization system based on a maintenance three-dimensional process, the specific steps of which are as follows:
[0047] S1. Initiate fault entry: When the fault inspection personnel are performing the fault inspection process, they initiate the fault entry process through the mobile terminal;
[0048] S2. Fault information acquisition: The basic information of the rack number, process, and parts is automatically acquired from the interactive electronic manual and imported into the fault entry process. The detailed information of the fault mode and fault description is registered by the fault inspection personnel;
[0049] S3. Locate the fault point on the model: accurately locate the fault point on the digital model by means of rotation and sectioning, and mark the geometric position;
[0050] S4, fault data management: transfer the mobile terminal data to the computer, and accumulate the single machine fault data to the machine model digital model for summary management, and trigger the fault analysis process at the same time;
[0051] S5. Generate fault solution: observe whether to initiate the fault analysis process;
[0052] S6. Use of fault solutions: Enter the single-machine fault solution into the fault knowledge base for subsequent fault solution recommendations, and send the solution to the production department for production scheduling and construction.
[0053] In the step S5, when the fault analysis process is initiated, the fault is sent to the technician, who analyzes the fault and develops a single-machine fault solution. If the fault analysis process is not initiated, the fault information is matched with the fault knowledge base. If the match is successful, the model fault solution is used as the solution to the fault. If the match is unsuccessful, the technician will complete the development of a single-machine fault solution.
[0054] The above shows and describes the basic principles, main features and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited to the above embodiments. The above embodiments and descriptions only describe the principles of the present invention. Without departing from the spirit and scope of the present invention, the present invention may have various changes and improvements, which fall within the scope of the present invention. The scope of protection of the present invention is defined by the attached claims and their equivalents.
Claims
1. A fault visualization system based on maintenance three-dimensional technology, characterized by: include: Data receiving module, used to import the designed digital model; The process management module is used to manage the 3D process information, complete the fault analysis process through fault analysis triggers, and provide fault solutions; Three-dimensional process editing module, to edit the three-dimensional process; Fault registration module, completes fault registration; Other extension modules complete the extended application of lightweight digital models.
2. A fault visualization system based on maintenance three-dimensional technology according to claim 1, characterized in that: The data receiving module includes functions such as digital model lightweighting and design information extraction.
3. The fault visualization system based on maintenance three-dimensional process according to claim 1, characterized in that: The data receiving module generates a lightweight digital-analog signal by calling a lightweight converter.
4. The fault visualization system based on maintenance three-dimensional process according to claim 1, characterized in that: The process management module includes functions such as three-dimensional lightweight digital model management, three-dimensional process management, three-dimensional fault data management, three-dimensional process resource management, and three-dimensional lightweight digital model reader.
5. A fault visualization system based on maintenance three-dimensional technology according to claim 4, characterized in that: The process management module browses the stored three-dimensional lightweight digital models and three-dimensional processes by calling the three-dimensional lightweight digital model reader.
6. The fault visualization system based on maintenance three-dimensional process according to claim 1, characterized in that: The three-dimensional process editing module triggers the three-dimensional process editor through the process management module.
7. The fault visualization system based on maintenance three-dimensional process according to claim 4, characterized in that: The fault registration module calls the three-dimensional lightweight model reader through the interactive electronic manual to consult the three-dimensional process animation model.
8. An analysis method for a fault visualization system based on a three-dimensional maintenance process according to any one of claims 1 to 7, characterized in that: The specific steps are as follows: S1. Initiate fault entry: When the fault inspection personnel are performing the fault inspection process, they initiate the fault entry process through the mobile terminal; S2. Fault information acquisition: The basic information of the rack number, process, and parts is automatically acquired from the interactive electronic manual and imported into the fault entry process. The detailed information of the fault mode and fault description is registered by the fault inspection personnel; S3. Locate the fault point on the model: accurately locate the fault point on the digital model by means of rotation and sectioning, and mark the geometric position; S4, fault data management: transfer the mobile terminal data to the computer, and accumulate the single machine fault data to the machine model digital model for summary management, and trigger the fault analysis process at the same time; S5. Generate fault solution: observe whether to initiate the fault analysis process; S6. Use of fault solutions: Enter the single-machine fault solution into the fault knowledge base for subsequent fault solution recommendations, and send the solution to the production department for production scheduling and construction.
9. The analysis method of a fault visualization system based on a three-dimensional maintenance process according to claim 8, characterized in that: In the step S5, when the fault analysis process is initiated, the fault is sent to the technician, who analyzes the fault and develops a single-machine fault solution. If the fault analysis process is not initiated, the fault information is matched with the fault knowledge base. If the match is successful, the model fault solution is used as the solution to the fault. If the match is unsuccessful, the technician will complete the development of a single-machine fault solution.
Citation Information
Patent Citations
Product component fault visualization method based on 3D digital model
CN104517011A
Fault visualization television and fault visualization method thereof
CN108462323A