A simulated training command communication device for an aircraft flight simulator

Abstract

The utility model discloses a kind of simulation training command communication devices suitable for flight simulator, including shell, the power supply component is set on the shell, the voice signal amplifier component is set on the shell, the PLC control component is set on the shell, the transceiving communication component is set on the shell, the power supply component, the voice signal amplifier component, the PLC control component and the transceiving communication component are connected by cable electricity between, interconnection and intercommunication between flight simulator and real-time interconnection with real aeronautical tower control system are realized jointly, multiple models flight simulator can be adapted, support multi-unit cooperative training, improve communication simulation fidelity and equipment stability, suitable for military and civilian aviation flight simulation communication training scene.

Description

Technical Field

[0001] This utility model belongs to the field of aviation simulation training communication technology, specifically relating to a simulation training command and communication device adapted to flight simulators. Background Technology

[0002] Flight simulators are core equipment for improving the piloting skills and emergency response capabilities of military and civilian aviation systems. They are widely used in training systems. After technological iterations, existing flight simulators have relatively complete functions such as visual simulation, weather simulation, and special situation simulation. However, they still have the following shortcomings in hardware adaptation and system linkage related to command and communication: 1. It lacks the hardware structure adapted to aviation radio functions, and cannot simulate the functions required in real flight scenarios such as AM modulation, channel switching, half-duplex communication, and shared channel occupation through physical components; 2. The lack of standardized interconnection communication channel settings makes it difficult to form a stable network with the communication hardware equipment of the actual ground control system (tower, approach, area control), and it is difficult to achieve system linkage between multiple units; 3. The lack of modulation function hardware required for multi-simulator collaborative training makes it impossible to achieve orderly control of multi-channel communication, resulting in a disconnect between simulation training and actual flight hardware operation scenarios, which restricts the training effect. Therefore, we propose a simulation training command and communication device adapted to flight simulators. Utility Model Content

[0003] The purpose of this invention is to provide a simulation training command and communication device adapted to flight simulators, so as to solve the problems mentioned in the background art.

[0004] To achieve the above objectives, this utility model provides the following technical solution: a simulation training command and communication device adapted to a flight simulator, comprising: case; A power supply assembly, which is disposed on the housing; A voice signal amplifier assembly, wherein the voice signal amplifier assembly is disposed on the housing; PLC control component, wherein the PLC control component is mounted on the housing; A transceiver communication component, wherein the transceiver communication component is disposed on the housing; The power supply component, the voice signal amplifier component, the PLC control component, and the transceiver communication component are electrically connected by cables to jointly realize the interconnection between flight simulators and real-time interconnection with the real air traffic control tower system.

[0005] Preferably, the power supply assembly includes an AC power supply unit and a DC power supply unit, used to provide AC and DC dual-mode power supply for the simulation training command and communication device.

[0006] Preferably, the AC power supply unit includes an AC220V power connector and an AC power module; The AC220V power connector is located on the rear side of the housing, and the AC power module is located inside the housing. The AC220V power connector and the AC power module are connected, and the AC power module is connected to the voice signal amplifier assembly and the transceiver communication assembly via cables.

[0007] Preferably, the DC power supply unit includes a DC27V power interface; The DC27V power interface is located on the rear side of the housing, and the DC27V power interface is connected to the power input ports of the voice signal amplifier assembly and the transceiver communication assembly via cables. A power switch and a digital voltmeter are provided on the front side of the housing; The power switch is connected to the AC power module and the DC27V power interface, and the power switch is also connected to the digital voltmeter.

[0008] Preferably, the voice signal amplifier assembly includes a voice signal amplifier and a pilot communication lead wiring hole; Both the voice signal amplifier and the pilot communication lead wiring hole are provided with several, and the number is the same. Several of the aforementioned voice signal amplifiers are disposed within the housing, and several of the aforementioned pilot communication lead wiring holes are disposed on the rear side of the housing. The input terminals of the voice signal amplifiers are connected to the transceiver communication component, and the output terminals of the voice signal amplifiers are connected to the pilot communication lead wiring holes.

[0009] Preferably, the PLC control component includes a PLC controller and a serial test interface; The PLC controller is housed within the housing, and the serial test interface is located on the rear side of the housing. The PLC controller is electrically connected to the serial test interface, which is used to connect to an external programming device.

[0010] Preferably, the PLC controller is a Mitsubishi FX-3U series relay output type PLC controller; The PLC controller is equipped with several input ports and several output ports; Several input ports are connected to the transceiver communication component; Several output ports are connected to several of the pilot communication lead wires and the transceiver communication components.

[0011] Preferably, the transceiver communication component includes a transceiver, a communication control box, and a communication switch assembly; The transceiver is disposed inside the housing, the communication control box is nested on the housing, and the front panel of the communication control box extends out of the front side of the housing, and the communication switch assembly is disposed on the front side of the housing; The transceiver communication component further includes an antenna, which is disposed on the rear side of the housing. The transceiver is connected to the antenna and to the communication control box. The output port on the PLC controller is connected to the PTT port of the transceiver.

[0012] Preferably, the communication switch assembly includes a communication transmission power switch, a power indicator light, and a communication transmission indicator light; The communication transmission power switch, the power indicator light, and the communication transmission indicator light are all located on the front side of the housing; The power supply component is connected to the communication transmission power switch. The power indicator light and the communication transmission indicator light are both electrically connected to the power supply component through the communication transmission power switch, and the communication transmission indicator light is connected to the output port of the PLC controller.

[0013] Preferably, the outer sides of the housing are provided with symmetrically distributed heat dissipation windows, the rear side of the housing is provided with a heat dissipation fan vent, and the interior of the housing is provided with a heat dissipation fan at the position corresponding to the heat dissipation fan vent. The heat dissipation fan is connected to the power supply component.

[0014] Compared with the prior art, the beneficial effects of this utility model are: 1. Strong adaptability to multiple scenarios, reducing training site limitations: The power supply component has a dual power supply structure of AC220V mains power and DC27V DC power, which can be adapted to different environments such as indoor training halls (mains power) and temporary outdoor training sites (DC backup power), without the need to build additional power supply lines. 2. Multi-aircraft formation collaborative training support to improve the level of training systemization: The four independent channels of the voice signal amplifier component and the half-duplex hardware logic of the PLC control component can simultaneously connect to four flight simulators, supporting advanced training courses such as multi-aircraft formation collaboration and handling of special situations in the aircraft group. Furthermore, by expanding the number of built-in hardware modules, it is possible to support the linkage of multiple flight simulators, effectively reducing the investment cost of training equipment. 3. Seamless interconnection with real control towers, narrowing the gap between simulation and actual operation: The transceiver components adopt real aviation transceivers (supporting AM modulation and 118-137MHz civil aviation frequency band), and are equipped with a ¼ wavelength low-power whip omnidirectional antenna, which can directly access the control frequencies of military (civilian) control towers. This allows pilots to achieve the same communication control process (such as frequency switching and call response) as in actual training during simulation training, solving the problem of "virtualized communication scenarios and disconnect from actual operation" in existing flight simulators, and improving the realism of training. 4. Stable and reliable hardware control, reducing the risk of training failure: The PLC control component adopts relay output type hardware, which can effectively avoid communication interruption caused by program crashes compared with software control schemes. In addition, the heat dissipation window, heat dissipation fan vent and heat dissipation fan work together to effectively control the temperature inside the housing, preventing the transceiver and power module from crashing due to high temperature, thus improving the stability and reliability of the device operation. 5. Standardized interfaces and convenient maintenance reduce operation and maintenance costs: Standardized AC220V power connectors, DC27V interfaces, communication lead wiring holes, and serial test interfaces are used. Operators can identify the connections without training, avoiding component damage caused by incorrect connections. The serial test interface supports calibration with external programming equipment, allowing for troubleshooting of PLC logic problems without disassembling the housing, facilitating maintenance. Each component is modular and can be replaced independently. Failure of a single component does not require replacement of the entire device, reducing operation and maintenance costs. Attached Figure Description

[0015] Figure 1 This is a three-dimensional structural diagram of the device of this utility model; Figure 2 This is a three-dimensional structural diagram of the device of this utility model; Figure 3 This is a three-dimensional structural diagram of the device of this utility model; Figure 4 This is a cross-sectional perspective view of the device of this utility model. Figure 5 This is a circuit connection schematic diagram of the present invention.

[0016] In the diagram: 1. Housing; 2. Power supply assembly; 201. AC220V power connector; 202. AC power module; 203. DC27V power interface; 204. Power switch; 205. Digital voltmeter; 3. Voice signal amplifier assembly; 301. Voice signal amplifier; 302. Pilot communication lead wire connection hole; 4. PLC control assembly; 401. PLC controller; 402. Serial test interface; 5. Transceiver communication assembly; 501. Transceiver; 502. Communication control box; 503. Communication switch assembly; 5031. Communication transmission power switch; 5032. Power indicator light; 5033. Communication transmission indicator light; 504. Antenna; 6. Heat dissipation window; 7. Heat dissipation fan vent; 8. Heat dissipation fan. Detailed Implementation

[0017] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0018] Please see Figures 1-5 The simulation training command and communication device adapted to flight simulators provided by this utility model includes: The housing 1 has symmetrically distributed heat dissipation windows 6 on both outer sides, a heat dissipation fan vent 7 on the rear side of the housing 1, and a heat dissipation fan 8 inside the housing 1 at the position corresponding to the heat dissipation fan vent 7. The heat dissipation fan 8 is connected to the power supply component 2. The heat dissipation window 6, the heat dissipation fan vent 7 and the heat dissipation fan 8 work together to form an air circulation heat dissipation system, which dissipates the heat generated by the components inside the housing, and avoids the performance degradation or failure of electrical components such as power supply and transceiver due to high temperature. The heat dissipation fan 8 is connected to the power supply component 2 via a cable to ensure that the fan and the device start and stop synchronously, without the need for additional power supply. Power supply component 2 is mounted on housing 1. Power supply component 2 includes an AC power supply unit and a DC power supply unit, which are used to provide AC and DC dual-mode power supply for the simulation training command and communication device. The AC power supply unit includes an AC220V power connector 201 and an AC power module 202. An AC220V power connector 201 is located on the rear side of housing 1. An AC power module 202 is located inside housing 1. The AC220V power connector 201 and the AC power module 202 are connected. The AC power module 202 is connected to the voice signal amplifier assembly 3 and the transceiver communication assembly 5 via cables. The DC power supply unit includes a DC27V power interface 203. The DC27V power interface 203 is located on the rear side of housing 1. The DC27V power interface 203 is connected to the power input ports of the voice signal amplifier assembly 3 and the transceiver communication assembly 5 via cables. A power switch 204 and a digital voltmeter 205 are located on the front side of housing 1. The power switch 204 is connected to the AC power module 202 and the DC27V power interface 203, and the power switch 204 is also connected to the digital voltmeter 205. AC220V power connector 201 is compatible with AC mains power. AC power module 202 converts AC mains power to DC27V (for transceiver 501) and DC12V (for voice signal amplifier 301) to meet the voltage requirements of different components. DC27V power interface 203 is compatible with external DC power supply (such as backup DC power supply for training site) to achieve AC mains power + DC dual power supply redundancy and avoid training interruption due to single power supply failure. The power switch 204 is a centralized control device for power on / off, which is convenient to operate. The digital voltmeter 205 displays the power supply voltage in real time, which makes it easy for operators to quickly determine whether the power supply is within the normal working range and to promptly troubleshoot power supply abnormalities. The voice signal amplifier assembly 3 is mounted on the housing 1. The voice signal amplifier assembly 3 includes a voice signal amplifier 301 and a pilot communication lead wire connection hole 302. The voice signal amplifier 301 is model TPA3118. There are four voice signal amplifiers 301 and four pilot communication lead wire connection holes 302. The four voice signal amplifiers 301 are located inside the housing 1, and the four pilot communication lead wire connection holes 302 are located on the rear side of the housing 1. The input terminal of the voice signal amplifier 301 is connected to the transceiver communication assembly 5, and the output terminal of the voice signal amplifier 301 is connected to the pilot communication lead wire connection hole 302. The voice signal amplifier 301 receives the weak audio signal output by the transceiver 501 and amplifies the signal to a volume suitable for the pilot's headset through a Class D audio power amplifier circuit. At the same time, four independent pilot communication lead wire connection holes 302 can connect the pilot headsets and microphones of four flight simulators simultaneously, supporting multi-team collaborative training. The connection holes use standardized audio interfaces, eliminating the need to replace adapter plugs and reducing operational complexity. PLC control component 4 is mounted on housing 1. PLC control component 4 includes PLC controller 401 and serial test interface 402. PLC controller 401 is mounted inside housing 1, and serial test interface 402 is mounted on the rear side of housing 1. PLC controller 401 is electrically connected to serial test interface 402. Serial test interface 402 is used to connect to external programming devices. PLC controller 401 is a Mitsubishi FX-3U series relay output type PLC controller; PLC controller 401 is equipped with multiple sets of input ports and output ports; four input ports are connected to transceiver communication component 5; five output ports are connected to four pilot communication lead wire wiring holes 302 and transceiver communication component 5. The PLC controller program runs in a cyclic scanning mode, and its logical judgment process is as follows: Input sampling stage: Read the status of input terminals X0-X3 (i.e., the signals of transmit buttons 1#-4#); Program execution phase: Based on the ladder diagram program, determine which button was pressed and handle interlocking and other logical relationships (e.g., ensure that only one microphone is activated at a time). Output refresh phase: Based on the logic operation results, update the state of output terminals Y0-Y4 and activate the corresponding microphone channels (Y1-Y4); at the same time, control Y0 to output a low level, so that the transceiver enters the transmit (PTT) state; The transceiver communication component 5 is mounted on the housing 1. The transceiver communication component 5 includes a transceiver 501, a communication control box 502, and a communication switch assembly 503. The transceiver 501 is a TKR-123 transceiver, and the communication control box 502 is a TKR123-K6E transceiver. The transceiver 501 is housed within the housing 1, and the communication control box 502 is nested within the housing 1, with its front panel extending beyond the front side of the housing 1. The communication switch assembly 503 is located on the front side of the housing 1. The transceiver communication component 5 also includes an antenna 504, which is a ¼-wavelength low-power whip omnidirectional antenna located on the rear side of the housing 1. The transceiver 501 is connected to the antenna 504 and the communication control box 502. The output port of the PLC controller 401 is connected to the PTT port of the transceiver 501. The communication switch assembly 503 includes a communication transmission power switch 5031, a power indicator light 5032, and a communication transmission indicator light 5033; the communication transmission power switch 5031, the power indicator light 5032, and the communication transmission indicator light 5033 are all located on the front side of the housing 1; the power supply assembly 2 is connected to the communication transmission power switch 5031, and the power indicator light 5032 and the communication transmission indicator light 5033 are both electrically connected to the power supply assembly 2 through the communication transmission power switch 5031, and the communication transmission indicator light 5033 is correspondingly connected to the output port of the PLC controller 401; The PLC controller 401 receives trigger signals from the flight simulator or the communication transmitter power switch 5031 through input ports (X0-X3). Hardware relay logic enables half-duplex control, allowing only one channel to be active at a time, avoiding signal superposition and distortion caused by simultaneous transmission from multiple channels. Output ports (Y1-Y4) connect to four pilot microphones. Port Y0 connects to the PTT control terminal of the transceiver 501, ensuring synchronization between the trigger signal and the transceiver's transmission action. The serial test interface 402 connects to an external programming device, allowing calibration of the PLC hardware logic (such as adjusting channel response delays). Maintenance can be performed without disassembling the device, improving repair efficiency. After receiving the PTT signal from the PLC controller 401, the transceiver 501 modulates the audio signal from the pilot's microphone into a high-frequency signal, which is then radiated through the antenna 504. Simultaneously, it receives high-frequency signals from other simulators or real control towers, demodulates them into audio signals, and sends them to the voice signal amplifier 301. The communication control box 502 realizes frequency switching (such as the 118-137MHz civil aviation frequency band), channel preset, and adapts to the communication protocols of different training courses. The communication transmission power switch 5031 is the power switch for the communication switch assembly. Its function is to supply power to the communication switch assembly. The corresponding switch can be turned on according to the number and sequence of simulators used to control the operation of the communication switch assembly. The power indicator 5032 (green) indicates whether the channel is powered on, and the communication transmission indicator 5033 (red) indicates whether the channel is in the transmission state. Operators can quickly judge the working status of each channel through the indicator lights and troubleshoot in a timely manner. The power supply component 2, the voice signal amplifier component 3, the PLC control component 4 and the transceiver communication component 5 are electrically connected by cables to jointly realize the interconnection and interoperability between flight simulators and the real-time interconnection with the real air traffic control system. like Figure 5 The diagram shown is a schematic diagram of the circuit connection between the power supply component 2, the voice signal amplifier component 3, the PLC control component 4, and the transceiver communication component 5 in this utility model. This is well known to those skilled in the art and will not be described in detail here.

[0019] The beneficial effects of this utility model are as follows: 1. Strong adaptability to multiple scenarios, reducing training site limitations: The dual power supply structure of power component 2, with AC220V mains power and DC27V DC power, can be adapted to different environments such as indoor training halls (mains power) and temporary outdoor training sites (DC backup power), without the need to build additional power supply lines. 2. Multi-aircraft team collaborative training support, improving the level of training systemization: The four independent channels of the voice signal amplifier component 3 and the half-duplex hardware logic of the PLC control component 4 can be connected to four flight simulators at the same time, supporting advanced training subjects such as multi-aircraft formation collaboration and handling special situations of aircraft groups. Moreover, by expanding the number of built-in hardware modules, it is possible to support the linkage of multiple flight simulators, effectively reducing the investment cost of training equipment. 3. Seamless interconnection with real control towers, narrowing the gap between simulation and actual operation: The transceiver communication component 5 adopts a real aviation transceiver (supporting AM modulation and 118-137MHz civil aviation frequency band), and is equipped with a ¼ wavelength low-power whip omnidirectional antenna. It can directly access the control frequencies of military (civilian) aviation control towers, enabling pilots to achieve the same communication control process (such as frequency switching and call response) as in actual operation during simulation training. This solves the problem of "virtualized communication scenarios and disconnection from actual operation" in existing flight simulators, and improves the realism of training. 4. Stable and reliable hardware control reduces the risk of training failures: The PLC control component 4 adopts relay output type hardware, which can effectively avoid communication interruption caused by program crashes compared with software control schemes. In addition, the heat dissipation window 6, heat dissipation fan vent 7 and heat dissipation fan 8 work together to effectively control the temperature inside the housing, preventing the transceiver and power module from crashing due to high temperature, and improving the stability and reliability of the device operation. 5. Standardized interfaces and convenient maintenance reduce operation and maintenance costs: Standardized AC220V power connectors, DC27V interfaces, communication lead wiring holes, and serial test interfaces are used. Operators can identify the connections without training, avoiding component damage caused by incorrect connections. The 402 serial test interface supports calibration with external programming equipment, allowing for troubleshooting of PLC logic problems without disassembling the housing, facilitating maintenance. Each component is modular and can be replaced independently. Failure of a single component does not require replacement of the entire device, reducing operation and maintenance costs.

[0020] In summary, the usage method of the simulation training command and communication device adapted to flight simulators provided in this embodiment is as follows: 1. Device Connection: First, the operator connects the communication leads of the pilot's headset and microphone to the communication lead wiring hole 302 on the rear side of housing 1, and connects the omnidirectional antenna to the antenna mounting bracket on the rear side of housing 1; then, the power supply line is connected to the AC220V power connector 201 or DC27V power interface 203 on the rear side of housing. 2. Power on: The operator stands in front of the housing 1, presses the power switch 204, and observes the display value of the front digital voltmeter 205: if it displays "DC27V±0.5V", it means that the power supply is normal; at the same time, observe whether the rear cooling fan 8 is rotating. If it is not rotating, the power should be disconnected immediately and the fan cable connection should be checked. 3. Training parameter settings: The operator sets the communication parameters according to the training requirements through the communication control box 502 on the front side of housing 1: Frequency setting: Rotate the "Frequency Adjustment" knob on the communication control box to adjust the communication frequency to the specified training value (such as 125.8MHz for civil aviation approach frequency and 225MHz for military aviation training frequency). The frequency value is displayed in real time on the display screen of the communication control box. Channel preset: Press the "Channel Storage" button on the communication control box to store the current frequency to the specified channel (corresponding to the frequency commonly used in training). It can be quickly recalled later through the "Channel Switching" button without having to repeatedly adjust the frequency. 4. Communication simulation training: Single-channel communication operation: The operator instructs the pilot of simulator #1 to press the simulator's communication button (or directly press the communication transmission power switch 5031 on the front of the device #1), and observe the communication transmission indicator light 5033 on channel #1 on the front of the device: if the red light is on, it means that channel #1 has entered the transmission state; The pilot in simulator #1 issues a training call command through the microphone, and the pilots in channels #2-#4 listen with headphones. If they can clearly hear the command from pilot #1 without noise or delay (delay ≤0.5s), it indicates that the single-channel communication is normal. Test channels 2 through 4 in sequence to ensure that the "transmit-receive" function of each channel is normal before proceeding to formal training; Multi-channel coordination and conflict resolution: Multi-channel coordination: The pilots of simulators #1 and #2 press the communication button in turn. Channel #1 launches first, and channel #2 waits for channel #1 to finish launching before triggering. The hardware logic of PLC control component 4 realizes "alternating launch" to simulate multi-aircraft formation coordinated communication. Conflict handling verification: Intentionally instruct the pilots of simulators #1 and #3 to press the communication button simultaneously and observe the indicator light status: Only the red light of the channel that is triggered first (such as #1) is on, while the red light of the channel that is triggered later (#3) is not on. This indicates that the half-duplex interlock logic of the PLC control module is effective, avoiding communication interruption caused by signal superposition. If the red lights of two channels are on at the same time, the input response delay of the PLC needs to be calibrated through the serial test interface 402.

[0021] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A simulation training command and communication device adapted to a flight simulator, characterized in that, include: Shell (1); Power supply assembly (2), the power supply assembly (2) being disposed on the housing (1); A voice signal amplifier assembly (3) is disposed on the housing (1); PLC control component (4), the PLC control component (4) is disposed on the housing (1); A transceiver communication component (5) is disposed on the housing (1); The power supply component (2), the voice signal amplifier component (3), the PLC control component (4) and the transceiver communication component (5) are electrically connected by cables to jointly realize the interconnection between flight simulators and the real-time interconnection with the real aviation tower control system.

2. The simulation training command and communication device adapted to a flight simulator according to claim 1, characterized in that: The power supply component (2) includes an AC power supply unit and a DC power supply unit, which are used to provide AC and DC dual-mode power supply for the simulation training command and communication device.

3. The simulation training command and communication device adapted to a flight simulator according to claim 2, characterized in that: The AC power supply unit includes an AC220V power connector (201) and an AC power module (202). The AC220V power connector (201) is located on the rear side of the housing (1), and the AC power module (202) is located inside the housing (1). The AC220V power connector (201) and the AC power module (202) are connected together, and the AC power module (202) is connected to the voice signal amplifier assembly (3) and the transceiver communication assembly (5) via cables.

4. The simulation training command and communication device adapted to a flight simulator according to claim 3, characterized in that: The DC power supply unit includes a DC27V power interface (203). The DC27V power interface (203) is located on the rear side of the housing (1), and the DC27V power interface (203) is connected to the power input ports of the voice signal amplifier assembly (3) and the transceiver communication assembly (5) via cables. A power switch (204) and a digital voltmeter (205) are provided on the front side of the housing (1). The power switch (204) is connected to the AC power module (202) and the DC27V power interface (203), and the power switch (204) is connected to the digital voltmeter (205).

5. The simulation training command and communication device adapted to a flight simulator according to claim 1, characterized in that: The voice signal amplifier assembly (3) includes a voice signal amplifier (301) and a pilot communication lead wire connection hole (302). The voice signal amplifier (301) and the pilot communication lead wire connection hole (302) are each provided with several, and the number is the same; A plurality of the aforementioned voice signal amplifiers (301) are disposed inside the housing (1), and a plurality of the aforementioned pilot communication lead wire connection holes (302) are disposed on the rear side of the housing (1). The input end of the voice signal amplifier (301) is connected to the transceiver communication component (5), and the output end of the voice signal amplifier (301) is connected to the pilot communication lead wire connection hole (302).

6. The simulation training command and communication device adapted to a flight simulator according to claim 5, characterized in that: The PLC control component (4) includes a PLC controller (401) and a serial test interface (402). The PLC controller (401) is located inside the housing (1), and the serial test interface (402) is located on the rear side of the housing (1). The PLC controller (401) is electrically connected to the serial test interface (402), and the serial test interface (402) is used to connect to an external programming device.

7. A simulation training command and communication device adapted to a flight simulator according to claim 6, characterized in that: The PLC controller (401) is a Mitsubishi FX-3U series relay output type PLC controller; The PLC controller (401) is equipped with several input ports and several output ports; Several input ports are connected to the transceiver communication component (5); Several output ports are connected to several of the pilot communication lead wires (302) and the transceiver communication component (5).

8. The simulation training command and communication device adapted to a flight simulator according to claim 7, characterized in that: The transceiver communication component (5) includes a transceiver (501), a communication control box (502), and a communication switch component (503). The transceiver (501) is disposed inside the housing (1), the communication control box (502) is nested on the housing (1), and the front panel of the communication control box (502) extends out of the front side of the housing (1), and the communication switch assembly (503) is disposed on the front side of the housing (1); The transceiver communication component (5) further includes an antenna (504), which is disposed on the rear side of the housing (1). The transceiver (501) is connected to the antenna (504) and the transceiver (501) is connected to the communication control box (502). The output port on the PLC controller (401) is connected to the PTT port of the transceiver (501).

9. A simulation training command and communication device adapted to a flight simulator according to claim 8, characterized in that: The communication switch assembly (503) includes a communication transmission power switch (5031), a power indicator (5032), and a communication transmission indicator (5033). The communication transmission power switch (5031), the power indicator (5032), and the communication transmission indicator (5033) are all located on the front side of the housing (1); The power supply component (2) is connected to the communication transmission power switch (5031). The power indicator (5032) and the communication transmission indicator (5033) are both electrically connected to the power supply component (2) through the communication transmission power switch (5031). The communication transmission indicator (5033) is connected to the output port of the PLC controller (401).

10. A simulation training command and communication device adapted to a flight simulator according to claim 1, characterized in that: The housing (1) has symmetrically distributed heat dissipation windows (6) on both outer sides, and a heat dissipation fan vent (7) is provided on the rear side of the housing (1). A heat dissipation fan (8) is provided inside the housing (1) at the position corresponding to the heat dissipation fan vent (7). The heat dissipation fan (8) is connected to the power supply assembly (2).

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