Aircraft practical training method and system
Through the combination of virtual and real methods in the aircraft training system, rich training resources and scenarios are provided, which solves the problems of insufficient resources and low interaction in existing aircraft training, and improves the efficiency and effectiveness of training.
Patent Information
- Application Number
- CN202510094301.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-21
- Publication Date
- 2025-03-07
AI Technical Summary
In the existing aircraft training, insufficient resources, few scenarios and low interaction levels make it difficult for students to deeply understand the principles and maintenance processes of the aircraft system, and the practical training results are poor.
Using a combination of virtual and real methods, a rich training resources and scenarios are provided to improve the interaction level through the simulated engine, operating table subsystem and teacher terminal system in the aircraft training system.
Through virtualization, the internal structure and working principles of the aircraft are demonstrated, hardware limitations are reduced, training content and scenarios are enriched, and training efficiency and effectiveness are improved.
Smart Images
Figure CN119580559A_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the field of aircraft training technology, and more specifically, to an aircraft training method and system. Background Art
[0002] For aircraft, any failure may bring serious consequences, or even cause irreparable losses. Therefore, for personnel engaged in aircraft maintenance, they not only need to master solid theoretical knowledge, but also must have a high degree of situational awareness and proficient maintenance skills.
[0003] However, existing aircraft operation and maintenance training is often based on observation and maintenance training on old aircraft and actual maintenance operations. There are insufficient training resources, few training scenarios, and a low level of interaction. It is difficult for trainees to deeply understand the principles, structures, and maintenance processes of aircraft systems, resulting in poor training results. Summary of the invention
[0004] In view of this, the purpose of this application is to provide an aircraft training method and system, which can provide rich training resources and training scenarios based on a combination of virtual and real methods, and have a high degree of interaction, thereby improving the effect of aircraft training.
[0005] An aircraft training method provided in an embodiment of the present application is applied to an aircraft training system, wherein the aircraft training system comprises: a control system and a simulated engine; the control system comprises an operation console subsystem and an instructor terminal subsystem; the simulated engine comprises a hardware model and a data acquisition mechanism constructed based on a real engine; the data acquisition mechanism comprises a plurality of data acquisition components, and the data acquisition components are installed inside or outside the hardware model; the operation console subsystem displays a first human-machine interaction interface, and the first human-machine interaction interface displays a virtual operation console of an aircraft cockpit; the instructor terminal subsystem displays a second human-machine interaction interface, and the second human-machine interaction interface displays a virtual engine model of the real engine and operation principle diagrams of a plurality of aircraft submodules; the training method comprises:
[0006] A first training operation is performed based on the hardware model of the simulation engine, and a data acquisition mechanism of the simulation engine acquires target state data corresponding to the hardware model and the first training operation, and sends the target state data to the operation console subsystem and / or the instructor terminal system;
[0007] In response to receiving the target state data, the operation console subsystem updates the state of the virtual operation console based on the target state data so that the state of the virtual operation console matches the first practical training operation;
[0008] In response to receiving the target state data, the instructor subsystem updates the display result of the second human-computer interaction interface so that the display result of the second human-computer interaction interface matches the first training operation.
[0009] In some embodiments, in the aircraft training method, the hardware model of the simulated engine includes a plurality of target parts for disassembly and assembly training, and the data acquisition mechanism includes a first acquisition element for acquiring in-situ state data of the target parts, and a second acquisition element for acquiring operating state data of the hardware model of the simulated engine;
[0010] The data collection mechanism of the simulation engine collects target state data corresponding to the first training operation, including:
[0011] The data acquisition mechanism of the simulated engine acquires the target part in-place status data corresponding to the first training operation and / or the operation status data of the hardware model of the simulated engine.
[0012] In some embodiments, the aircraft training method further includes:
[0013] In response to receiving a second practical training operation for the virtual operating console, the operating console subsystem updates the state of the virtual operating console so that the state of the virtual operating console matches the second practical training operation;
[0014] The operation platform subsystem generates training instruction information based on the second training operation, and sends the training instruction information to the instructor subsystem;
[0015] In response to receiving the practical training instruction information, the instructor terminal system updates the display result of the second human-computer interaction interface so that the display result of the second human-computer interaction interface matches the second practical training operation.
[0016] In some embodiments, in the aircraft training method, the virtual operating console includes an operating panel model, a switch model, and an indicator light model of the aircraft cockpit;
[0017] In response to receiving a second training operation for the virtual operating console, the operating console subsystem updates the state of the virtual operating console to make the state of the virtual operating console match the second training operation, including:
[0018] In response to receiving the second training operation for the virtual operating console, the operating console subsystem simulates and displays the screen of each display device in the operating panel model;
[0019] Determine the real-time position of the switch in the switch model and update the state of the switch model;
[0020] Based on the real-time position of the ignition switch, a virtual instrument and display information in the screen of the display device are determined.
[0021] In some embodiments, in the aircraft training method, updating the display result of the second human-computer interaction interface includes:
[0022] updating the second human-computer interaction interface to display the state of the virtual engine model of the real engine;
[0023] and / or,
[0024] The state of the operation schematic diagram of the aircraft submodule displayed on the second human-machine interaction interface is updated.
[0025] In some embodiments, the aircraft training method further comprises:
[0026] In response to the interface switching operation on the instructor terminal system, the second human-computer interaction interface is controlled to switch and display the virtual engine model and the operating principle diagram.
[0027] In some embodiments, the aircraft training method further includes: the second graphical user interface of the instructor terminal system also displays a fault setting interface;
[0028] The instructor subsystem generates a fault setting instruction in response to a fault setting operation on the fault setting interface;
[0029] The instructor terminal system responds to the fault setting instruction by controlling the second human-computer interaction interface to display a first fault state matching the virtual engine model and the fault setting instruction, and / or controls the display of a second fault state matching the dynamic schematic diagram and the fault setting instruction.
[0030] In some embodiments, the aircraft training method further includes:
[0031] The instructor subsystem sends the fault setting instruction to the console subsystem, so that the first graphical user interface of the console subsystem displays the third fault state that matches the virtual console and the fault setting instruction;
[0032] Based on the third fault state of the virtual operating console, a second practical training operation on the virtual operating console is performed.
[0033] In some embodiments, in the aircraft training method, the aircraft training system further includes a scoring subsystem;
[0034] The scoring subsystem acquires the target state data corresponding to the first training operation, the training instruction information corresponding to the second training operation, and the manual scoring information collected by the data collection mechanism;
[0035] A training scoring result is determined based on the target state data corresponding to the first training operation, the training instruction information corresponding to the second training operation, and the manual scoring information.
[0036] In some embodiments, an aircraft training system is further provided, the aircraft training system comprising: a control system and a simulated engine; the control system comprises an operating console subsystem and an instructor terminal subsystem; the simulated engine comprises a hardware model and a data acquisition mechanism built based on a real engine; the data acquisition mechanism comprises a plurality of data acquisition elements, and the data acquisition elements are installed inside or outside the hardware model; the operating console subsystem displays a first human-computer interaction interface, and the first human-computer interaction interface displays a virtual operating console of an aircraft cockpit; the instructor terminal subsystem displays a second human-computer interaction interface, and the second human-computer interaction interface displays a virtual engine model of the real engine and an operation schematic diagram of a plurality of aircraft submodules; the training method comprises:
[0037] Based on the simulation engine, a first practical training operation is performed through a hardware model, and a data acquisition mechanism of the simulation engine acquires target state data corresponding to the hardware model and the first practical training operation, and sends the target state data to an operation console subsystem and / or an instructor terminal system;
[0038] The operating platform subsystem is used for updating the state of the virtual operating platform based on the target state data in response to receiving the target state data so that the state of the virtual operating platform matches the first practical training operation;
[0039] The instructor terminal system is used to update the display result of the second human-computer interaction interface in response to receiving the target state data, so that the display result of the second human-computer interaction interface matches the first training operation.
[0040] In an embodiment of the present application, an aircraft training method and system are provided, which are applied to an aircraft training system, wherein the aircraft training system comprises: a control system and a simulated engine; the control system comprises an operating console subsystem and an instructor terminal subsystem; the simulated engine comprises a hardware model and a data acquisition mechanism constructed based on a real engine; the data acquisition mechanism comprises a plurality of data acquisition components, and the data acquisition components are installed inside or outside the hardware model; the operating console subsystem displays a first human-computer interaction interface, and the first human-computer interaction interface displays a virtual operating console of an aircraft cockpit; the instructor terminal subsystem displays a second human-computer interaction interface, and the second human-computer interaction interface displays a virtual engine of the real engine. The training method performs a first training operation based on the hardware model of the simulation engine, and the data acquisition mechanism of the simulation engine acquires the hardware model and target state data corresponding to the first training operation, and sends the target state data to the console subsystem and / or the instructor terminal subsystem; the console subsystem responds to receiving the target state data and updates the state of the virtual console based on the target state data so that the state of the virtual console matches the first training operation; the instructor terminal subsystem responds to receiving the target state data and updates the display result of the second human-computer interaction interface so that the display result of the second human-computer interaction interface matches the first training operation. The simulation engine is built based on the real engine, and its hardware model and data acquisition mechanism can accurately reflect the actual working status of the engine during training. The operating table subsystem displays the virtual operating table of the aircraft cockpit, so that trainees can perform training operations under conditions close to the real environment. The instructor terminal system provides a more intuitive display of the principles and structures of connecting the aircraft during the training process for trainees by displaying the virtual engine model and the operating principle diagrams of multiple aircraft submodules, thereby enhancing the authenticity and interactivity of the training. Based on the interaction between the operating table subsystem, the instructor terminal system and the simulation engine, trainees learn the impact of practical training operations on the status of the operating table in the cockpit in real time through the operating table subsystem, thereby And deepen the understanding of the aircraft operating system; through the instructor terminal system, the corresponding engine model status and operating principle diagram during the training process of hardware model disassembly and assembly are synchronously displayed, helping students understand the working principle and internal structure of the engine, so that the training is no longer limited to a single disassembly and assembly operation, but covers all-round training and intuitive dynamic display from the operating table to the internal structure of the engine, thereby enriching the training content and scenarios; through virtualization, the changes, principles and structures that the hardware model cannot directly display are displayed, and through the combination of simulated engines, virtual operating tables and virtual engine models, the hardware limitations during training are reduced, thereby effectively making up for the problem of insufficient resources in traditional training; based on this, the efficiency and effectiveness of training can be improved. BRIEF DESCRIPTION OF THE DRAWINGS
[0041] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings required for use in the embodiments will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without paying creative work.
[0042] Figure 1 A schematic diagram of the structure of the simulation engine described in the embodiment of the present application is shown;
[0043] Figure 2 A schematic diagram of the first human-computer interaction interface of an embodiment of the present application is shown;
[0044] Figure 3 A schematic diagram of the second human-computer interaction interface of an embodiment of the present application is shown;
[0045] Figure 4 Another schematic diagram of the second human-computer interaction interface of the embodiment of the present application is shown;
[0046] Figure 5 A flow chart of the aircraft training method according to an embodiment of the present application is shown;
[0047] Figure 6 A flow chart of another aircraft training method according to an embodiment of the present application is shown;
[0048] Figure 7 A flow chart of another aircraft training method described in an embodiment of the present application is shown. DETAILED DESCRIPTION
[0049] To make the purpose, technical scheme and advantages of the embodiments of the present application clearer, the technical scheme in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. It should be understood that the drawings in the present application only serve the purpose of explanation and description and are not used to limit the scope of protection of the present application. In addition, it should be understood that the schematic drawings are not drawn in real proportion. The flowchart used in this application shows the operations implemented according to some embodiments of the present application. It should be understood that the operations of the flowchart can be implemented out of sequence, and the steps without logical context can be reversed in order or implemented simultaneously. In addition, those skilled in the art can add one or more other operations to the flowchart under the guidance of the content of the present application, or remove one or more operations from the flowchart.
[0050] In addition, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. The components of the embodiments of the present application described and shown in the drawings here can be arranged and designed in various configurations. Therefore, the following detailed description of the embodiments of the present application provided in the drawings is not intended to limit the scope of the application claimed for protection, but merely represents the selected embodiments of the present application. Based on the embodiments of the present application, all other embodiments obtained by those skilled in the art without making creative work belong to the scope of protection of the present application.
[0051] It should be noted that the term "comprising" will be used in the embodiments of the present application to indicate the existence of the features declared thereafter, but does not exclude the addition of other features.
[0052] For aircraft, any failure may bring serious consequences, or even cause irreparable losses. Therefore, for personnel engaged in aircraft maintenance, they not only need to master solid theoretical knowledge, but also must have a high degree of situational awareness and proficient maintenance skills.
[0053] However, in the existing aircraft operation and maintenance training, there is a lack of training resources and a low level of interaction, making it difficult for trainees to deeply understand the principles, structures, and maintenance processes of aircraft systems, resulting in poor training results.
[0054] Based on this, an aircraft training method and system are provided in an embodiment of the present application, which are applied to an aircraft training system, wherein the aircraft training system includes: a control system and a simulated engine; the control system includes an operating console subsystem and an instructor terminal system; the simulated engine includes a hardware model and a data acquisition mechanism built based on a real engine; the data acquisition mechanism includes a plurality of data acquisition elements, and the data acquisition elements are installed inside or outside the hardware model; the operating console subsystem displays a first human-computer interaction interface, and the first human-computer interaction interface displays a virtual operating console of the aircraft cockpit; the instructor terminal system displays a second human-computer interaction interface, and the second human-computer interaction interface displays a virtual An engine model, and operating principle diagrams of multiple aircraft sub-modules; the training method performs a first training operation based on the hardware model of the simulated engine, and the data acquisition mechanism of the simulated engine acquires the hardware model and target state data corresponding to the first training operation, and sends the target state data to the operating console subsystem and / or the instructor terminal subsystem; the operating console subsystem responds to receiving the target state data and updates the state of the virtual operating console based on the target state data so that the state of the virtual operating console matches the first training operation; the instructor terminal subsystem responds to receiving the target state data and updates the display result of the second human-computer interaction interface so that the display result of the second human-computer interaction interface matches the first training operation. First, the practical training operation is matched; the simulation engine is built based on the real engine, and its hardware model and data acquisition mechanism can accurately reflect the actual working state of the engine during the practical training; the operating console subsystem displays the virtual operating console of the aircraft cockpit, so that trainees can perform practical training operations under conditions close to the real environment; the instructor terminal system provides a more intuitive display of the principles and structures of connecting the aircraft during the practical training of trainees by displaying the virtual engine model and the operating principle diagrams of multiple aircraft sub-modules, thereby enhancing the authenticity and interactivity of the practical training; based on the interaction between the operating console subsystem, the instructor terminal system and the simulation engine, trainees learn the impact of practical training operations on the status of the operating console in the cockpit in real time through the operating console subsystem, Thereby deepening the understanding of the aircraft operating system; synchronously displaying the corresponding engine model status and operating schematic diagram during the practical training process such as hardware model disassembly and assembly through the instructor terminal system, helping trainees understand the working principle and internal structure of the engine, so that the training is no longer limited to a single disassembly and assembly operation, but covers all-round training and intuitive dynamic display from the operating console to the internal structure of the engine, thereby enriching the training content and scenarios; displaying the changes, principles and structures that the hardware model cannot directly display in a virtual way, and reducing the hardware limitations during training through the combination of simulated engines, virtual operating consoles and virtual engine models, thereby effectively making up for the problem of insufficient resources in traditional training; based on this, the efficiency and effectiveness of training can be improved.
[0055] The present application embodiment provides an aircraft training method, which is applied to an aircraft training system, wherein the aircraft training system includes: a control system and a simulated engine; the control system includes an operating console subsystem and an instructor terminal subsystem; please refer to Figure 1 , Figure 1 The structure diagram of the simulation engine described in the embodiment of the present application is shown; the simulation engine includes a hardware model and a data acquisition mechanism built based on a real engine; the data acquisition mechanism includes a plurality of data acquisition elements, and the data acquisition elements are installed inside or outside the hardware model; please refer to Figure 2 , Figure 2 The schematic diagram of the first human-machine interaction interface of the embodiment of the present application is shown; the console subsystem displays the first human-machine interaction interface, and the first human-machine interaction interface displays the virtual console of the aircraft cockpit; please refer to Figure 3 , Figure 3 A schematic diagram of the second human-computer interaction interface of the embodiment of the present application is shown; please refer to Figure 4 , Figure 4 Another schematic diagram of the second human-machine interaction interface of the embodiment of the present application is shown; the instructor terminal system displays the second human-machine interaction interface, and the second human-machine interaction interface displays the virtual engine model of the real engine and the operating principle diagram of multiple aircraft submodules; please refer to Figure 5 The training method includes the following steps S501-S503:
[0056] S501, performing a first training operation based on the hardware model of the simulation engine, wherein the data acquisition mechanism of the simulation engine acquires the hardware model and target state data corresponding to the first training operation, and sends the target state data to the operation console subsystem and / or the instructor terminal system;
[0057] S502: In response to receiving the target state data, the operation console subsystem updates the state of the virtual operation console based on the target state data so that the state of the virtual operation console matches the first practical training operation;
[0058] S503: In response to receiving the target state data, the instructor terminal system updates the display result of the second human-computer interaction interface so that the display result of the second human-computer interaction interface matches the first training operation.
[0059] The safety and stability of aircraft engines, as the "heart" of an aircraft, are directly related to flight safety. Therefore, for personnel engaged in aircraft maintenance, practical training on aircraft engines is a top priority. They not only need to master solid theoretical knowledge, but also must have a high degree of situational operational awareness and proficient maintenance skills.
[0060] Based on this, in an embodiment of the present application, a simulation engine is specially constructed based on the aircraft training system to conduct training for trainees based on the simulation engine.
[0061] In step S101, a first training operation is performed based on the hardware model of the simulation engine. The data acquisition mechanism of the simulation engine acquires the hardware model and target state data corresponding to the first training operation, and sends the target state data to the operating console subsystem and / or the instructor terminal system.
[0062] The simulated engine includes a hardware model built based on a real engine. A simulation design is carried out for the target model engine to ensure that the simulation quality is closely matched with the practical training function. In terms of meeting the disassembly and assembly needs, the key components are highly simulated and their structural characteristics are finely restored to meet the strict requirements of disassembly and assembly strength, ensuring that trainees can truly experience and master the disassembly and assembly skills during the training process.
[0063] For details, please refer to Figure 1 In this embodiment, the simulated engine 2 for aircraft training is also connected to a simulated wing 1. The simulated wing 1 and the simulated engine 2 are integrated into one body through a support 3 to facilitate teaching and training.
[0064] In this embodiment, if Figure 1 As shown, in order to make this training equipment closer to the actual wing and engine, the simulated wing 1 is detachably arranged on the top of the support 3, and the simulated engine 2 is suspended at the bottom of the simulated wing 1 through the support 3. Furthermore, the simulated wing 1 and the simulated engine 2 are both detachably connected to the support 3, so as to facilitate the repair and replacement of the simulated wing 1 and the simulated engine 2. In addition, it should be noted that the specifications, materials and specific structures of the simulated wing 1 and the simulated engine 2 in this embodiment are not fixed, and should be determined comprehensively according to actual conditions such as training content, as long as they can meet the teaching and training needs.
[0065] The data acquisition elements in the data acquisition mechanism of the simulated engine include sensors, collectors, etc. The sensors include displacement sensors and / or proximity sensors. In this way, on the basis of restoring the hardware structure of the target model engine, the engine is also innovatively modified, and signal devices such as sensors and collectors are added. These devices can collect and transmit information to the control system in real time, and realize linkage with the operating platform subsystem and the instructor terminal system.
[0066] Based on this, the hardware model of the simulated engine includes a plurality of target parts for disassembly and assembly training, and the data acquisition mechanism includes a first acquisition element for acquiring in-situ state data of the target parts, and a second acquisition element for acquiring operating state data of the hardware model of the simulated engine;
[0067] The data collection mechanism of the simulation engine collects target state data corresponding to the first training operation, including:
[0068] The data acquisition mechanism of the simulated engine acquires the target part in-place status data corresponding to the first training operation and / or the operation status data of the hardware model of the simulated engine.
[0069] That is to say, the target state data is the in-place state data of the target parts corresponding to the first training operation and / or the running state data of the hardware model of the simulated engine.
[0070] The target part in-place status data is used to determine whether the target part is successfully disassembled or assembled.
[0071] The operating state data of the hardware model of the simulated engine represents the operating state of the hardware model of the simulated engine, such as speed data, temperature and pressure data, etc.
[0072] The target status data is sent to the operating console subsystem and / or the instructor subsystem. That is, for each target status data, the target status data can be sent to the operating console subsystem individually, to the instructor subsystem individually, or to the operating console subsystem and / or the instructor subsystem simultaneously.
[0073] In the step S102 , in response to receiving the target state data, the operating console subsystem updates the state of the virtual operating console based on the target state data so that the state of the virtual operating console matches the first training operation.
[0074] The virtual operating console in the operating console subsystem includes an operating panel model, a switch model and an indicator light model of the aircraft cockpit.
[0075] The operation panel model provides an interface for interacting with various aircraft systems, allowing precise control and adjustment of various functions of the aircraft; illustratively, the operation panel model includes multiple parts such as flight control, navigation, communication, engine control, etc., each part has specific operation buttons and switches, and students can achieve comprehensive control of the aircraft or engine through these operation panels.
[0076] The switch is the key component that controls the switches of various aircraft systems. It can start or shut down various functions of the aircraft, such as landing gear, flaps, lights, etc.
[0077] Indicator lights are an important source of information in the cockpit of an aircraft. They can display various status information of the aircraft in real time, such as engine status, fuel level, vibration value, etc. By observing the status of the indicator lights, you can timely understand the operation of the aircraft and make corresponding operations and adjustments. In addition, when a fault or abnormal situation occurs, the indicator light will light up to remind the pilot to take timely measures to deal with it and ensure the safety of the flight.
[0078] The console subsystem can realize the operation of cockpit panels and switches, enrich the practical training content and training scenarios, and interact with the simulated engine hardware. Trainees can learn the relationship between the engine and the status of the console in the cockpit in real time, thereby deepening their understanding of the aircraft operating system.
[0079] In response to receiving the target status data, the operating console subsystem updates the status of the virtual operating console based on the target status data so that the status of the virtual operating console matches the first training operation. Specifically, the information displayed in the virtual operating console can be updated, such as updating the speed data, or updating the indicator light status of the indicator light module, such as the engine fault indicator light is on, thereby intuitively demonstrating the linkage relationship between the training operations such as engine maintenance and disassembly and assembly and the virtual operating console.
[0080] Please refer to Figure 6 In some embodiments, in the aircraft training method, the training method further includes the following steps S601-S603:
[0081] S601: In response to receiving a second training operation for a virtual operating console, the operating console subsystem updates the state of the virtual operating console so that the state of the virtual operating console matches the second training operation;
[0082] S602, the operating platform subsystem generates training instruction information based on the second training operation, and sends the training instruction information to the instructor subsystem;
[0083] S603: In response to receiving the practical training instruction information, the instructor terminal system updates the display result of the second human-computer interaction interface so that the display result of the second human-computer interaction interface matches the second practical training operation.
[0084] The second training operation is used to simulate the working status logic of various aircraft systems for the aircraft cockpit panels and switches. The various aircraft systems mainly include: air conditioning, automatic flight, communication, power supply, fire alarm, flight control, fuel, hydraulics, anti-icing, indication and recording, lighting, oxygen, bleed air, APU, power unit and other systems.
[0085] In response to receiving a second training operation for the virtual operating console, the operating console subsystem updates the state of the virtual operating console to make the state of the virtual operating console match the second training operation, including:
[0086] In response to receiving the second training operation for the virtual operating console, the operating console subsystem simulates and displays the screen of each display device in the operating panel model;
[0087] Determine the real-time position of the switch in the switch model and update the state of the switch model;
[0088] Based on the real-time position of the ignition switch, a virtual instrument and display information in the screen of the display device are determined.
[0089] That is to say, the console subsystem can simulate the screens of display devices such as PFD, ND, CDU, etc., and control the changes of virtual instruments and information in each screen in real time according to the different positions of each switch.
[0090] The operating console subsystem interacts with the instructor terminal subsystem to achieve linkage between the operating console subsystem and the instructor terminal subsystem. When the state of the virtual operating console is updated based on the second practical training operation control for the virtual operating console, the virtual engine model and / or operating schematic diagram displayed by the instructor terminal subsystem is synchronously updated. This dynamic display enhances the realism and immersion of the practical training, enabling trainees to better understand the working principles and internal structures of various aircraft systems.
[0091] In the step S103, the instructor subsystem updates the display result of the second human-computer interaction interface in response to receiving the target state data, so that the display result of the second human-computer interaction interface matches the first training operation.
[0092] Specifically, updating the display result of the second human-computer interaction interface includes:
[0093] updating the second human-computer interaction interface to display the state of the virtual engine model of the real engine;
[0094] and / or,
[0095] The state of the operation schematic diagram of the aircraft submodule displayed on the second human-machine interaction interface is updated.
[0096] In response to the interface switching operation on the instructor terminal system, the second human-computer interaction interface is controlled to switch and display the virtual engine model and the operating principle diagram.
[0097] That is to say, for the virtual engine model and the operating principle diagram, both the target state data corresponding to the first training operation can be updated, and the training instruction information corresponding to the second training operation can be updated.
[0098] The dynamic schematic diagram can dynamically display the flow direction of the fuel line, as well as changes in fuel temperature and oil color; when operating the virtual operating console (cockpit switches and switches), the dynamic schematic diagram can make corresponding changes.
[0099] The virtual engine model is synchronized with the first training operation of the hardware model. Compared with the disassembly, assembly, and maintenance training based on the hardware model, the virtual engine model can be enlarged, flipped, split, and has the advantages of operational flexibility and visualization: at the same time, it is safer, has lower risks, and has high training efficiency and repeatability.
[0100] In addition, the virtual engine model records the first training operation and the second training operation during the training process, which is convenient for trainees to analyze their own shortcomings afterwards, thereby improving the training effect.
[0101] In some embodiments, trainees can perform simulated disassembly and assembly based on the virtual engine model, alleviating the problem of insufficient practical training resources.
[0102] Please refer to Figure 7 In some embodiments, the second graphical user interface of the instructor terminal system further displays a fault setting interface; the training method further includes the following steps S701-S702:
[0103] S701, the instructor subsystem generates a fault setting instruction in response to a fault setting operation on the fault setting interface;
[0104] S702. In response to the fault setting instruction, the instructor terminal system controls the second human-computer interaction interface to display a first fault state in which the virtual engine model matches the fault setting instruction, and / or controls the display of a second fault state in which the dynamic schematic diagram matches the fault setting instruction.
[0105] In some embodiments, the instructor terminal system sets a certain component failure, a certain component in the dynamic schematic diagram can display the failure state, and the fuel line flow direction displays a phenomenon consistent with the failure.
[0106] In some embodiments, the aircraft training method further comprises:
[0107] The instructor subsystem sends the fault setting instruction to the console subsystem, so that the first graphical user interface of the console subsystem displays the third fault state that matches the virtual console and the fault setting instruction;
[0108] Based on the third fault state of the virtual operating console, a second practical training operation on the virtual operating console is performed.
[0109] Exemplarily, for example, if a transmission failure is set, the engine failure indicator light of the virtual operating console will light up.
[0110] In some embodiments, the aircraft training system further includes a scoring subsystem;
[0111] The scoring subsystem acquires the target state data corresponding to the first training operation, the training instruction information corresponding to the second training operation, and the manual scoring information collected by the data collection mechanism;
[0112] A training scoring result is determined based on the target state data corresponding to the first training operation, the training instruction information corresponding to the second training operation, and the manual scoring information.
[0113] In some embodiments, the grading subsystem is configured in the instructor subsystem.
[0114] In some embodiments, the scoring subsystem is configured in a cloud service or a backend.
[0115] The scoring subsystem can receive detection signals sent by sensors, collectors and other devices of the simulation hardware, receive the training instruction information corresponding to the second training operation, extract key information through precise data analysis and processing, and provide strong data support for computer scoring and judgment. At the same time, the system can also automatically generate scores for computer automatic scoring, which greatly reduces the burden of scoring work; in addition, teachers or experts can perform real-time scoring while students complete training tasks according to specific task scoring tables; finally, the system will combine the results of computer automatic scoring and manual scoring to generate a detailed final score and scoring report, and send it to the instructor's desk to provide strong support for teaching management and decision-making.
[0116] The scoring subsystem is a comprehensive platform that integrates functions such as signal reception and analysis, intelligent judgment, and multi-person evaluation and scoring. It combines computer automatic scoring with manual scoring, thereby achieving complementary advantages between the two. Computer scoring is based on its objectivity and efficiency to ensure that the scoring process is rapid and accurate. Manual scoring can capture complex factors that are difficult for computers to quantify, such as the standardization and correctness of operations, thus making up for the shortcomings of computer scoring. This combination not only greatly improves the accuracy and fairness of scoring, but also makes the entire scoring process more comprehensive and reliable.
[0117] The teacher terminal system has a complete teaching resource management capability; it can uniformly store, classify and retrieve various teaching resources, such as teaching videos, teaching courseware, teaching materials, etc.; teachers can quickly call these resources according to teaching needs to provide students with rich and diverse learning materials; the teacher terminal system can easily set and issue training tasks; teachers can formulate personalized training plans based on the students' learning progress and ability level, and issue these tasks to students through the teacher's desk; students can receive tasks on their own terminals and complete them as required.
[0118] Fault setting is an important function in the instructor terminal system. It is used to simulate various possible fault conditions of the engine. The instructor can set different fault types through the instructor terminal to test the students' troubleshooting ability.
[0119] In addition, it also has a student management function, which can record the basic information, learning progress, training results, etc. of the students; the instructor can check the learning situation of the students at any time through the instructor's desk, understand the strengths and weaknesses of the students, so as to provide targeted guidance and help; the instructor's desk can automatically record the training results of the students, and conduct statistics and analysis; the instructor can evaluate the learning effect of the students based on the performance data, so as to adjust the teaching plan and teaching methods in time; at the same time, the performance management function can also provide students with a fair and transparent competition environment to stimulate their learning enthusiasm. The instructor subsystem provides different scoring tables for each practical training task to facilitate experts or instructors to score the operation process, and receives the final results sent by the scoring subsystem for summary and analysis.
[0120] Based on the same inventive concept, an aircraft training system corresponding to the aircraft training method is also provided in the embodiment of the present application. Since the principle of solving the problem by the system in the embodiment of the present application is similar to the above-mentioned method in the embodiment of the present application, the implementation of the system can refer to the implementation of the method, and the repeated parts will not be repeated.
[0121] In some embodiments, an aircraft training system is provided, the aircraft training system comprising: a control system and a simulated engine; the control system comprises an operation console subsystem and an instructor terminal subsystem; the simulated engine comprises a hardware model and a data acquisition mechanism built based on a real engine; the data acquisition mechanism comprises a plurality of data acquisition elements, the data acquisition elements being installed inside or outside the hardware model; the operation console subsystem displays a first human-machine interaction interface, the first human-machine interaction interface displays a virtual operation console of an aircraft cockpit; the instructor terminal subsystem displays a second human-machine interaction interface, the second human-machine interaction interface displays a virtual engine model of the real engine, and operation schematic diagrams of a plurality of aircraft submodules; the training method comprises:
[0122] Based on the simulation engine, a first practical training operation is performed through a hardware model, and a data acquisition mechanism of the simulation engine acquires target state data corresponding to the hardware model and the first practical training operation, and sends the target state data to an operation console subsystem and / or an instructor terminal system;
[0123] The operating platform subsystem is used for updating the state of the virtual operating platform based on the target state data in response to receiving the target state data so that the state of the virtual operating platform matches the first practical training operation;
[0124] The instructor terminal system is used to update the display result of the second human-computer interaction interface in response to receiving the target state data, so that the display result of the second human-computer interaction interface matches the first training operation.
[0125] In some embodiments, in the aircraft training system, the hardware model of the simulated engine includes a plurality of target parts for disassembly and assembly training, and the data acquisition mechanism includes a first acquisition element for acquiring in-situ state data of the target parts, and a second acquisition element for acquiring operating state data of the hardware model of the simulated engine;
[0126] The simulation engine, when collecting target state data corresponding to the first training operation through the data collection mechanism, is specifically used to:
[0127] The data acquisition mechanism of the simulated engine acquires the target part in-place status data corresponding to the first training operation and / or the operation status data of the hardware model of the simulated engine.
[0128] In some embodiments, in the aircraft training system, the operating console subsystem is further used for:
[0129] In response to receiving a second practical training operation for the virtual operating platform, updating the state of the virtual operating platform to make the state of the virtual operating platform match the second practical training operation;
[0130] The operation platform subsystem generates training instruction information based on the second training operation, and sends the training instruction information to the instructor subsystem;
[0131] The instructor terminal system is further configured to update the display result of the second human-computer interaction interface in response to receiving the practical training instruction information, so that the display result of the second human-computer interaction interface matches the second practical training operation.
[0132] In some embodiments, in the aircraft training system, the virtual operating console includes an operating panel model, a switch model, and an indicator light model of the aircraft cockpit;
[0133] The operating platform subsystem, in response to receiving a second training operation for the virtual operating platform, updates the state of the virtual operating platform so that the state of the virtual operating platform matches the second training operation, specifically for:
[0134] In response to receiving the second training operation for the virtual operating console, the operating console subsystem simulates and displays the screen of each display device in the operating panel model;
[0135] Determine the real-time position of the switch in the switch model and update the state of the switch model;
[0136] Based on the real-time position of the ignition switch, a virtual instrument and display information in the screen of the display device are determined.
[0137] In some embodiments, in the aircraft training system, the instructor terminal system, when updating the display result of the second human-computer interaction interface, is specifically used to:
[0138] updating the second human-computer interaction interface to display the state of the virtual engine model of the real engine;
[0139] and / or,
[0140] The state of the operation schematic diagram of the aircraft submodule displayed on the second human-machine interaction interface is updated.
[0141] In some embodiments, in the aircraft training system, the instructor terminal system is also used to control the second human-computer interaction interface to switch and display the virtual engine model and the operating principle diagram in response to an interface switching operation on the instructor terminal system.
[0142] In some embodiments, in the aircraft training system, the second graphical user interface of the instructor terminal system further displays a fault setting interface; the instructor terminal system is further used to:
[0143] In response to a fault setting operation on the fault setting interface, generating a fault setting instruction;
[0144] The instructor terminal system responds to the fault setting instruction by controlling the second human-computer interaction interface to display a first fault state matching the virtual engine model and the fault setting instruction, and / or controls the display of a second fault state matching the dynamic schematic diagram and the fault setting instruction.
[0145] In some embodiments, in the aircraft training system, the instructor terminal system is further used for:
[0146] Sending the fault setting instruction to the operation console subsystem so that the first graphical user interface of the operation console subsystem displays a third fault state that matches the virtual operation console and the fault setting instruction;
[0147] Based on the third fault state of the virtual operating console, a second practical training operation on the virtual operating console is performed.
[0148] In some embodiments, the aircraft training system further includes a scoring subsystem;
[0149] The scoring subsystem is further used to obtain the target state data corresponding to the first training operation, the training instruction information corresponding to the second training operation, and the manual scoring information collected by the data collection mechanism;
[0150] A training scoring result is determined based on the target state data corresponding to the first training operation, the training instruction information corresponding to the second training operation, and the manual scoring information.
[0151] Those skilled in the art can clearly understand that, for the convenience and simplicity of description, the specific working process of the system and device described above can refer to the corresponding process in the method embodiment, and will not be repeated in this application. In the several embodiments provided in this application, it should be understood that the disclosed system, device and method can be implemented in other ways. The device embodiments described above are merely schematic. For example, the division of the modules is only a logical function division. There may be other division methods in actual implementation. For example, multiple modules or components can be combined or integrated into another system, or some features can be ignored or not executed. Another point is that the mutual coupling or direct coupling or communication connection shown or discussed can be through some communication interfaces, indirect coupling or communication connection of devices or modules, which can be electrical, mechanical or other forms.
[0152] The modules described as separate components may or may not be physically separated, and the components shown as modules may or may not be physical units, that is, they may be located in one place or distributed on multiple network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of this embodiment.
[0153] In addition, each functional unit in each embodiment of the present application may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit.
[0154] If the functions are implemented in the form of software functional units and sold or used as independent products, they can be stored in a non-volatile computer-readable storage medium that is executable by a processor. Based on this understanding, the technical solution of the present application, or the part that contributes to the prior art or the part of the technical solution, can be embodied in the form of a software product, which is stored in a storage medium and includes several instructions for a computer device (which can be a personal computer, a platform server, or a network device, etc.) to perform all or part of the steps of the method described in each embodiment of the present application. The aforementioned storage medium includes: various media that can store program codes, such as USB flash drives, mobile hard drives, ROM, RAM, magnetic disks, or optical disks.
[0155] The above are only specific implementations of the present application, but the protection scope of the present application is not limited thereto. Any technician familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present application, which should be included in the protection scope of the present application. Therefore, the protection scope of the present application should be based on the protection scope of the claims.
Claims
1. An aircraft training method, characterized in that: Applied to an aircraft training system, the aircraft training system comprises: a control system and a simulated engine; the control system comprises an operation console subsystem and an instructor terminal subsystem; the simulated engine comprises a hardware model and a data acquisition mechanism built based on a real engine; the data acquisition mechanism comprises a plurality of data acquisition elements, and the data acquisition elements are installed inside or outside the hardware model; the operation console subsystem displays a first human-machine interaction interface, and the first human-machine interaction interface displays a virtual operation console of an aircraft cockpit; the instructor terminal subsystem displays a second human-machine interaction interface, and the second human-machine interaction interface displays a virtual engine model of the real engine and operation principle diagrams of a plurality of aircraft submodules; the training method comprises: A first training operation is performed based on the hardware model of the simulation engine, and a data acquisition mechanism of the simulation engine acquires target state data corresponding to the hardware model and the first training operation, and sends the target state data to the operation console subsystem and / or the instructor terminal system; In response to receiving the target state data, the operation console subsystem updates the state of the virtual operation console based on the target state data so that the state of the virtual operation console matches the first practical training operation; In response to receiving the target state data, the instructor subsystem updates the display result of the second human-computer interaction interface so that the display result of the second human-computer interaction interface matches the first training operation.
2. The aircraft training method according to claim 1, characterized in that: The hardware model of the simulated engine includes a plurality of target parts for disassembly and assembly training, and the data acquisition mechanism includes a first acquisition element for acquiring in-situ state data of the target parts, and a second acquisition element for acquiring operating state data of the hardware model of the simulated engine; The data collection mechanism of the simulation engine collects target state data corresponding to the first training operation, including: The data acquisition mechanism of the simulated engine acquires the target part in-place status data corresponding to the first training operation and / or the operation status data of the hardware model of the simulated engine.
3. The aircraft training method according to claim 1, characterized in that: The training method also includes: In response to receiving a second practical training operation for the virtual operating console, the operating console subsystem updates the state of the virtual operating console so that the state of the virtual operating console matches the second practical training operation; The operation platform subsystem generates training instruction information based on the second training operation, and sends the training instruction information to the instructor subsystem; In response to receiving the practical training instruction information, the instructor terminal system updates the display result of the second human-computer interaction interface so that the display result of the second human-computer interaction interface matches the second practical training operation.
4. The aircraft training method according to claim 3, characterized in that: The virtual operation console includes an operation panel model, a switch model and an indicator light model of the aircraft cockpit; In response to receiving a second training operation for the virtual operating console, the operating console subsystem updates the state of the virtual operating console to make the state of the virtual operating console match the second training operation, including: In response to receiving the second training operation for the virtual operating console, the operating console subsystem simulates and displays the screen of each display device in the operating panel model; Determine the real-time position of the switch in the switch model and update the state of the switch model; Based on the real-time position of the ignition switch, a virtual instrument and display information in the screen of the display device are determined.
5. The aircraft training method according to claim 1 or 3, characterized in that: The updating of the display result of the second human-computer interaction interface includes: updating the second human-computer interaction interface to display the state of the virtual engine model of the real engine; and / or, The state of the operation schematic diagram of the aircraft submodule displayed on the second human-machine interaction interface is updated.
6. The aircraft training method according to claim 5, characterized in that: The training method also includes: In response to the interface switching operation on the instructor terminal system, the second human-computer interaction interface is controlled to switch and display the virtual engine model and the operating principle diagram.
7. The aircraft training method according to claim 1, characterized in that: The second graphical user interface of the instructor terminal system also displays a fault setting interface; the training method also includes: The instructor subsystem generates a fault setting instruction in response to a fault setting operation on the fault setting interface; The instructor terminal system responds to the fault setting instruction by controlling the second human-computer interaction interface to display a first fault state matching the virtual engine model and the fault setting instruction, and / or controls the display of a second fault state matching the dynamic schematic diagram and the fault setting instruction.
8. The aircraft training method according to claim 7, characterized in that: The training method further includes: the instructor subsystem sending the fault setting instruction to the console subsystem, so that the first graphical user interface of the console subsystem displays the third fault state that matches the virtual console and the fault setting instruction; Based on the third fault state of the virtual operating console, a second practical training operation on the virtual operating console is performed.
9. The aircraft training method according to claim 3, characterized in that: The aircraft training system also includes a scoring subsystem; The scoring subsystem acquires the target state data corresponding to the first training operation, the training instruction information corresponding to the second training operation, and the manual scoring information collected by the data collection mechanism; A training scoring result is determined based on the target state data corresponding to the first training operation, the training instruction information corresponding to the second training operation, and the manual scoring information.
10. An aircraft training system, characterized in that: The aircraft training system comprises: a control system and a simulated engine; the control system comprises an operation console subsystem and an instructor terminal subsystem; the simulated engine comprises a hardware model and a data acquisition mechanism built based on a real engine; the data acquisition mechanism comprises a plurality of data acquisition elements, and the data acquisition elements are installed inside or outside the hardware model; the operation console subsystem displays a first human-machine interaction interface, and the first human-machine interaction interface displays a virtual operation console of an aircraft cockpit; the instructor terminal subsystem displays a second human-machine interaction interface, and the second human-machine interaction interface displays a virtual engine model of the real engine and operation schematic diagrams of a plurality of aircraft submodules; the training method comprises: Based on the simulation engine, a first practical training operation is performed through a hardware model, and a data acquisition mechanism of the simulation engine acquires target state data corresponding to the hardware model and the first practical training operation, and sends the target state data to an operation console subsystem and / or an instructor terminal system; The operating platform subsystem is used for updating the state of the virtual operating platform based on the target state data in response to receiving the target state data so that the state of the virtual operating platform matches the first practical training operation; The instructor terminal system is used to update the display result of the second human-computer interaction interface in response to receiving the target state data, so that the display result of the second human-computer interaction interface matches the first training operation.