CN215911051U - Airborne automatic flight display control virtual training equipment - Google Patents
Airborne automatic flight display control virtual training equipment Download PDFInfo
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- CN215911051U CN215911051U CN202120219103.2U CN202120219103U CN215911051U CN 215911051 U CN215911051 U CN 215911051U CN 202120219103 U CN202120219103 U CN 202120219103U CN 215911051 U CN215911051 U CN 215911051U
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- 238000004088 simulation Methods 0.000 claims abstract description 104
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 25
- 238000012549 training Methods 0.000 claims abstract description 21
- 230000000694 effects Effects 0.000 claims description 49
- 230000005284 excitation Effects 0.000 claims description 12
- 238000012544 monitoring process Methods 0.000 claims description 3
- 238000007726 management method Methods 0.000 description 11
- 238000000034 method Methods 0.000 description 8
- 230000006870 function Effects 0.000 description 7
- 238000012360 testing method Methods 0.000 description 6
- 238000012423 maintenance Methods 0.000 description 4
- 238000011161 development Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 206010034719 Personality change Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000019771 cognition Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 238000013024 troubleshooting Methods 0.000 description 1
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Abstract
The utility model discloses an airborne automatic flight display control virtual training device, which is used for flight training and relates to the technical field of flight simulation; the teaching aid comprises a teacher control seat and a student control seat, wherein the student control seat comprises a simulation flight mode control panel, a simulation multifunctional display component, a simulation flight control computer, a simulation flight management computer, a simulation steering wheel, a simulation pedal, a simulation throttle lever, a simulation airplane comprehensive electronic instrument system, a simulation automatic flight state notice board and a simulation warning lamp which are electrically connected.
Description
Technical Field
The utility model discloses airborne automatic flight display control virtual training equipment, which is used for flight training and relates to the technical field of flight simulation.
Background
With the rapid development of the aviation technology and the continuous increase of the complexity of an aircraft system, the most obvious characteristic of the development of the aviation technology is that the automation degree of an aircraft is higher and higher, and for flight, a pilot is still at the core position of a control system, so that more trainers are needed to meet the requirement of space flight, the training of the trainers is divided into two parts, namely theoretical education and actual operation, the theoretical education mainly comprises the theoretical knowledge of learning aerodynamics, air pilotage, aerometeorology, working principles of aerotechnical equipment and the like, and the actual operation is to exercise the physical quality of the trainers, so that the trainers can adapt to the high-altitude flight environment as soon as possible.
When training personnel, if a real aircraft is adopted, the cost is high, and certain danger is caused; the existing flight experience equipment is simple in structural design and difficult to enable trainees to obtain a real experience effect, so that the problem of how to enable the trainees to obtain real flight simulation training at low cost is continuously solved.
SUMMERY OF THE UTILITY MODEL
The utility model aims to: the airborne automatic flight display control virtual training equipment is provided, combines the media expression forms of three-dimensional figures, animations and the like, visually displays the working principle of the automatic flight system and main component equipment thereof and the effect generated by practice training operation, and improves the training effect.
The technical scheme adopted by the utility model is as follows: the machine-mounted virtual training equipment for automatic flight display control comprises a teacher control seat and a student control seat, wherein the student control seat comprises a simulation flight mode control panel, a simulation multifunctional display component, a simulation flight control computer, a simulation flight management computer, a simulation steering wheel, a simulation pedal, a simulation throttle lever, a simulation airplane comprehensive electronic instrument system, a simulation automatic flight state notice board and a simulation warning lamp which are electrically connected.
The simulated flight mode control panel is arranged on an instrument panel of the cockpit and is communicated with student control seat software through an RS232 interface.
The simulation multifunctional display component is a simulation multifunctional control display and is communicated with student control seat software through an RS232 interface.
The simulation flight control computer receives and resolves the guidance signal from the simulation flight management computer, receives the instruction signal excitation effect corresponding to the given state of the student control seat, and sends the output effect and the actuation effect corresponding to the given state and the signal excitation to the student control seat software through the output port.
The simulation flight management computer generates simulation guidance signals, the simulation guidance signals are transmitted to the simulation flight control computer through the student control seat software to realize the resolving of the signals, instruction signal excitation effects corresponding to fixed states are generated, and output effects and actuating effects corresponding to the given states and the signal excitation are sent to the student control seat software through the output port.
The simulated airplane comprehensive electronic instrument system comprises a simulated EFIS display and a simulated EICAS display, wherein the simulated EFIS display provides a working state monitoring function consistent with a B737NG airplane EFIS display (PFD) and a corresponding indication effect; the simulated EICAS display provides the operating function and mode consistent with that of a specific model EICAS display, generates simulated operating effects and display states consistent with the actual flight state of the aircraft, and sends parameter signals involved in automatic flight operations to student control seats and the simulated EICAS display.
The simulation automatic flight state notice board receives simulation instruction signals from the simulation flight control computer, and generates an indication effect corresponding to the given state of the simulation automatic flight state notice board, and the effect is consistent with the real flight state.
The simulation warning lamp receives a simulation instruction signal from the simulation flight control computer, generates an indication state corresponding to a given state of the simulation warning lamp, and keeps the effect consistent with the real flight state.
In summary, due to the adoption of the technical scheme, the utility model has the beneficial effects that:
the utility model combines the media expression forms of three-dimensional figures, animations and the like to visually display the working principle of the automatic flight system and the main components thereof and the effect generated by practice training operation, such as the display of flight simulation state and flight parameters of the airplane; the comprehensive training platform for supporting course contents of the professional automatic flight system related to aircraft maintenance is provided, and knowledge and capability training of different levels such as system cognition, composition, principle, operation, test, disassembly and assembly, troubleshooting and the like is realized from shallow to deep, classroom teaching is assisted, and the capability of students for comprehensively applying professional course knowledge to solve practical engineering application problems is developed.
Drawings
The utility model will now be described, by way of example, with reference to the accompanying drawings, in which:
FIG. 1 is a block diagram of the structural distribution of the present invention;
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, not all, embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example 1
As shown in fig. 1, an airborne automatic flight display control virtual training device comprises a teacher control seat and a student control seat, wherein the student control seat comprises an electrically connected simulated flight mode control panel, a simulated multifunctional display component, a simulated flight control computer, a simulated flight management computer, a simulated steering wheel, a simulated pedal, a simulated throttle lever, a simulated airplane comprehensive electronic instrument system, a simulated automatic flight state annunciator and a simulated warning lamp, and is combined with media representation forms such as three-dimensional graphs and animations to visually display the working principle of the automatic flight system and the main components thereof and the effect generated by practice training operation, such as the display of the simulated flight state and flight parameters of the airplane; providing relevant teaching resources (such as animation, video, text, PPT) and the like of an automatic flight system of the airplane, and further comprising an automatic pilot, a flight director, an automatic throttle system, a yaw damping system and a stabilizer balancing system, so as to meet the teaching requirements of links such as theory, practical training and the like; the student control seats receive input signals from the simulation flight control components, receive instruction signals output by a flight control computer and a flight management computer (including hardware simulation and software simulation), and provide display effects corresponding to the software and hardware simulation display components, actuation effects of software simulation control surfaces and airplane attitude change and parameter display; and confirming the completion of the training task and sending training task completion information to a teacher control seat, wherein the airborne automatic flight display control system is consistent with the current B737NG airplane.
The simulated flight mode control panel is arranged on an instrument panel of the cockpit and is communicated with student control seat software through an RS232 interface; providing an operation function and an operation mode which are consistent with a main stream type flight mode control board, generating an operation effect (electric effect) which is consistent with the operation function and the operation mode, sending simulation signals corresponding to specific operations to a student control seat, a simulation flight control computer and the like, and supporting the resolving of the student control seat and the simulation flight control computer to a flight path error signal; receiving and managing the operation information in the student training process, and providing the operation information for the student control seats to realize the synchronization of hardware simulation and software simulation.
The simulation multifunctional display component is a simulation multifunctional control display and is communicated with student control seat software through an RS232 interface; providing an operation function and an operation mode which are consistent with the airborne multifunctional control display with a specific model, generating a simulation operation effect corresponding to the aviation signal generator with the specific model, sending a parameter signal corresponding to the automatic flight operation to the student control seat and the simulated airborne multifunctional control display, and supporting the receiving, processing and resolving of the student control seat, the simulated computer and the flight parameters; receiving and managing operation information in the student training process, and providing the operation information to the student control seats to generate an effect consistent with that in the actual operation process; receiving and managing the operation information in the student training process, and providing the operation information for the student control seats to realize the synchronization of hardware simulation and software simulation.
The simulation flight control computer receives and resolves the guidance signal from the simulation flight management computer, receives the instruction signal excitation effect corresponding to the given state of the student control seat, and sends the output effect and the actuation effect corresponding to the given state and the signal excitation to the student control seat software through the output port; the working state of the simulated flight control computer is given by adopting a mode that a guiding teacher directly sets the simulated flight control computer, so that the working state of the simulated flight control computer is given; receiving information of operation, test, replacement and the like in the student training process, and providing corresponding flight control computer operation and test effects; the simulation signal of the simulation flight control computer is required to be sent to a simulation display component, a warning lamp (including hardware and software simulation) and an airplane model of student control seat software, and display and actuation effects consistent with the real flight condition are generated.
The simulation flight management computer generates a simulation guidance signal, the simulation guidance signal is transmitted to the simulation flight control computer through the student control seat software to realize the resolving of the signal, an instruction signal excitation effect corresponding to a fixed state is generated, and an output effect and an actuation effect corresponding to the given state and the signal excitation are sent to the student control seat software through an output port; the working state of the simulation flight management computer is given in a mode that a guidance teacher directly sets the simulation flight management computer, so that the working state of the simulation flight management computer is given; receiving information of operation, test, replacement and the like in the training process of students, and providing corresponding operation and test effects of the flight management computer.
The simulated airplane comprehensive electronic instrument system comprises a simulated EFIS display and a simulated EICAS display, wherein the simulated EFIS display provides a working state monitoring function consistent with a B737NG airplane EFIS display (PFD) and a corresponding indication effect; the simulation EICAS display provides an operation function and an operation mode which are consistent with the EICAS display of a specific model, generates a simulation operation effect and a display state which are consistent with the real flight state of the airplane, and sends parameter signals related to automatic flight operation to the student control seats and the simulation EICAS display; the receiving, processing and resolving of student control seats, simulation computers and flight parameters are supported; according to the inspection and test requirements of an airplane maintenance manual and a component maintenance manual, the simulated EICAS display is checked and tested according to the actual maintenance process; receiving and managing the operation information in the training process of the students and providing the operation information to the student control seats.
The simulation automatic flight state notice board receives a simulation instruction signal from the simulation flight control computer, generates an indication effect corresponding to the given state of the simulation automatic flight state notice board, keeps the effect consistent with the real flight state, and provides a power-on effect consistent with the main stream type automatic flight state notice board.
The simulation warning lamp receives a simulation instruction signal from the simulation flight control computer, generates an indication state corresponding to a given state of the simulation warning lamp, keeps the effect consistent with the real flight state, and provides a power-on effect consistent with the main machine type warning lamp.
The above description is only a preferred embodiment of the present invention, and not intended to limit the present invention, the scope of the present invention is defined by the appended claims, and all structural changes that can be made by using the contents of the description and the drawings of the present invention are intended to be embraced therein.
Claims (1)
1. The onboard virtual practical training equipment for automatic flight display control comprises a teacher control seat and a student control seat, and is characterized in that the student control seat comprises a simulation flight mode control panel, a simulation multifunctional display component, a simulation flight control computer, a simulation flight management computer, a simulation steering wheel, a simulation pedal, a simulation throttle lever, a simulation airplane comprehensive electronic instrument system, a simulation automatic flight state notice board and a simulation warning lamp which are electrically connected; the simulated flight mode control panel is arranged on an instrument panel of the cockpit and is communicated with student control seat software through an RS232 interface; the simulation multifunctional display component is a simulation multifunctional control display and is communicated with student control seat software through an RS232 interface; the simulation flight control computer receives and resolves the guidance signal from the simulation flight management computer, receives the instruction signal excitation effect corresponding to the given state of the student control seat, and sends the output effect and the actuation effect corresponding to the given state and the signal excitation to the student control seat software through the output port; the simulation flight management computer generates a simulation guidance signal, the simulation guidance signal is transmitted to the simulation flight control computer through the student control seat software to realize the resolving of the signal, an instruction signal excitation effect corresponding to a fixed state is generated, and an output effect and an actuation effect corresponding to the given state and the signal excitation are sent to the student control seat software through an output port; the simulated airplane comprehensive electronic instrument system comprises a simulated EFIS display and a simulated EICAS display, wherein the simulated EFIS display provides a working state monitoring function consistent with that of the B737NG airplane EFIS display and a corresponding indication effect; the simulation EICAS display provides an operation function and an operation mode which are consistent with those of the EICAS display, generates a simulation operation effect and a display state which are consistent with the real flight state of the airplane, and sends parameter signals related to automatic flight operation to the student control seats and the simulation EICAS display; the simulation automatic flight state notice board receives a simulation instruction signal from the simulation flight control computer, and generates an indication effect corresponding to the given state of the simulation automatic flight state notice board, and the effect is consistent with the real flight state; the simulation warning lamp receives a simulation instruction signal from the simulation flight control computer, generates an indication state corresponding to a given state of the simulation warning lamp, and keeps the effect consistent with the real flight state.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120219103.2U CN215911051U (en) | 2021-01-27 | 2021-01-27 | Airborne automatic flight display control virtual training equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120219103.2U CN215911051U (en) | 2021-01-27 | 2021-01-27 | Airborne automatic flight display control virtual training equipment |
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| Publication Number | Publication Date |
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| CN215911051U true CN215911051U (en) | 2022-02-25 |
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| CN202120219103.2U Expired - Fee Related CN215911051U (en) | 2021-01-27 | 2021-01-27 | Airborne automatic flight display control virtual training equipment |
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| CN (1) | CN215911051U (en) |
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2021
- 2021-01-27 CN CN202120219103.2U patent/CN215911051U/en not_active Expired - Fee Related
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