CN220188885U - Aircraft switch panel analogue means - Google Patents

Abstract

The utility model discloses an airplane switch panel simulation device, which comprises a L-shaped substrate and an indication panel which are mutually attached, a control circuit board which is kept at a certain interval with the back of the substrate and is connected with the substrate through a stud, a standby battery switch assembly, a power supply switch assembly, a brightness adjusting knob assembly, a lamplight switch assembly and an auxiliary switch assembly which are arranged on the control circuit board and are exposed on the indication panel to form corresponding areas, and an interface assembly which is arranged on the control circuit board. The utility model utilizes the electronic circuit structure to design the switch component and the knob component to simulate the operation function of the switch panel of the Saussner C172 model, thereby simplifying the physical structure operation component of the real machine, and processing and feeding back the operation instructions of the switch, the knob and the like by matching with the built-in data processing module, thereby providing the use experience which is basically indiscriminate with the operation of the real machine for the user and greatly reducing the manufacturing cost of the device.

Description

Aircraft switch panel analogue means

Technical Field

The utility model relates to flight simulation equipment, in particular to an aircraft switch panel simulation device which is mainly used for simulating a switch panel of a C172 type.

Background

With the rapid development of civil aviation industry in China, the opening of airspace in China and the relaxation of personal flight driving license, various flight experience devices and flight simulators become attractive. For units such as aviation experience halls, aviation science and technology halls, aviation education and training institutions and the like, the flight experience of visiting personnel on different categories and different models is met. The Saussner C172 model is the smallest airplane with the highest successful production in history, is used in civil flight training until now, is the model which is most easily contacted with airplane piloting by flight lovers, and has a wide application base.

The virtual key mode of the touch screen, which is mostly adopted by the display panel, the operation panel and the like of the existing flight simulation software, is not strong in operation sense for flight lovers or flight experimenters, and is poor in flight simulation experience. The method of using the real machine equipment to experience is high in cost and not suitable for wide use, and especially for lovers or experiences who operate the initial contact aircraft, the real machine equipment is easy to cause the experience machine to malfunction, and high maintenance and insurance costs are generated. Therefore, developing a set of flight simulation equipment with good operation experience and low cost aiming at the C172 model is needed in the field, and the utility model is mainly used for the switch panel simulation of the C172 model.

Disclosure of Invention

Aiming at the problems in the prior art, the utility model provides the airplane switch panel simulation device mainly used for the model C172, realizes the switch panel simulation of the model C172 through the low-cost structural design, and is convenient for flight lovers, especially beginners to experience civil airplane operation.

In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows:

the utility model provides an aircraft switch panel analogue means, including being the positive instruction panel of L shape of base plate, paste in the base plate with being matchedly, dispose in reserve storage battery district on the instruction panel according to the operation function, power supply control district, brightness control district, light control district and auxiliary function control district, a plurality of fretwork holes of seting up on base plate and instruction panel are run through respectively according to the region, keep certain interval and pass through the control circuit board that stud and base plate are connected with the base plate back, place on control circuit board and present the reserve storage battery switch assembly in reserve storage battery district through corresponding fretwork hole, install and present the power supply switch assembly in power supply control district through corresponding fretwork hole on the base plate back and be connected with control circuit board electricity, install the brightness control knob assembly that presents in brightness control district and be connected with control circuit board through corresponding fretwork hole on the base plate back, place on control circuit board and present the auxiliary switch assembly in auxiliary function control district through corresponding fretwork hole, and place on control circuit board's interface module, wherein, dispose on control circuit board and present on the control circuit board and be used for signal processing module and data processing input data processing module and data processing input to the power supply module and data processing module.

Specifically, the standby battery cell area is configured at the position, close to the upper side, of the L-shaped vertical edge on the indication panel, the standby battery cell switch assembly comprises a standby battery cell switch electrically connected with the switch signal acquisition circuit and a test indication lamp electrically connected with the data processing module, the standby battery cell switch adopts a three-gear toggle switch, and a deflector rod of the three-gear toggle switch and the test indication lamp extend out of the front surface of the indication panel through hollowed holes in the corresponding positions of the deflector rod and the test indication lamp.

Specifically, the power supply control area is configured at the middle position of the L-shaped vertical edge on the indication panel, the power supply switch assembly comprises a main electric gate generator switch, a battery switch, a first system change-over switch and a second system change-over switch which are electrically connected with the switch signal acquisition circuit, the main electric gate generator switch and the battery switch share a double-gear double-position ship-shaped switch, the first system change-over switch and the second system change-over switch share a double-gear double-position ship-shaped switch, the double-gear double-position ship-shaped switch is fixedly connected with the substrate, and the keycaps of the double-gear double-position ship-shaped switch are exposed out of the front surface of the indication panel through hollowed holes at the corresponding positions of the double-gear double-position ship-shaped switch.

Specifically, the brightness adjusting area is configured at the position of the L-shaped vertical edge on the indication panel, the brightness adjusting knob assembly comprises a panel brightness adjusting knob, a standby brightness adjusting knob, a base brightness adjusting knob and an avionic brightness adjusting knob which are electrically connected with the data processing module and are arranged in a matrix, a rotary encoder with the model EC11 is adopted, a rotary rod of the rotary encoder extends out of the front face of the indication panel through a hollowed hole at the corresponding position of the rotary rod, and a knob cap is configured on the rotary rod.

Specifically, the light control area is configured at the upper position of the L-shaped horizontal edge on the indication panel, the light switch assembly comprises an anti-collision light switch, a landing light switch, a sliding light switch, a navigation light switch and a stroboscopic light switch which are electrically connected with the switch signal acquisition circuit and are arranged in a horizontal row, two-gear toggle switches are adopted, and a deflector rod of each of the two-gear toggle switches extends out of the front face of the indication panel through a hollowed hole in the corresponding position of the deflector rod.

Specifically, the auxiliary function control area is configured at the lower position of the L-shaped horizontal edge on the indication panel, the auxiliary switch assembly comprises a fuel pump switch, a pitot tube heating equipment switch, a cabin power switch and a propeller heating switch which are electrically connected with the switch signal acquisition circuit and are arranged in a horizontal row, two-gear toggle switches are adopted, and a deflector rod of the two-gear toggle switches extends out of the front face of the indication panel through hollowed holes in the corresponding positions of the deflector rod.

Specifically, the switch signal acquisition circuit adopts a register chip with the model of XL74HC165 to acquire signals output by corresponding two-gear toggle switches.

Specifically, the data processing module adopts an STM32 development board as a core.

Specifically, the interface component adopts a USB interface or a Type-C interface.

Further, the indication panel is provided with a light transmission indication part corresponding to the standby battery cell area, the power supply control area, the brightness adjustment area, the light control area and the auxiliary function control area, the light transmission indication part is used for indicating the name of each component function in each area, and the control circuit board is provided with backlight LED lamps corresponding to the light transmission indication part, and the backlight LED lamps are electrically connected with the data processing module.

Compared with the prior art, the utility model has the following beneficial effects:

(1) According to the utility model, the electronic circuit structure is used for designing the switch assembly and the knob assembly to simulate the operation function of the switch panel of the Saussner C172 type, so that simplification of the physical structure operation part of the real machine is realized, the built-in data processing module is matched for processing and feeding back operation instructions such as the switch and the knob, and the simulation use of the switch panel of the C172 type can be effectively realized by combining the functions of an external flight simulation system, thereby providing a use experience basically indistinguishable from the operation of the real machine for a user and greatly reducing the manufacturing cost of the device. The utility model has the advantages of ingenious design, simple structure, low cost and convenient use, and is suitable for being applied to flight simulation equipment.

(2) The utility model realizes the operation function of each switch on the C172 type switch panel by using the two-gear toggle switch, and the brightness adjustment function of the switch panel by using the rotary encoder, and simultaneously realizes the signal processing by combining the operation signals of the two-gear toggle switch of the switch signal acquisition circuit and the operation signals of the two-gear toggle switch of the data processing module, thereby ensuring the real adjustment operation touch feeling, simplifying the structural design and the circuit design and realizing the simulation with low cost.

(3) The utility model adopts the integral shell structure and combines the hollow hole designs corresponding to different areas on the indication panel and the base plate to form a switch panel pattern similar to the external appearance of a true machine, thereby facilitating the user to quickly familiarize and master the related operation of the Saunas C172 type switch panel and reducing the hand-up difficulty of a beginner.

(4) According to the utility model, the STM32 development board is used as the core of the data processing module, so that the hardware cost is effectively reduced on the basis of ensuring the use performance, and meanwhile, the USB/Type-C interface is used as an interface for signal transmission and power supply, so that the device can be conveniently and simply connected with other flight simulation equipment.

(5) The utility model also designs the light transmission indicating part and the corresponding backlight LED lamp, which are convenient for indicating the names of the functions of each component, can accurately identify the functions even under the condition of darker external light, and provides convenience for users to familiarize with the related operation of the C172 type switch panel.

Drawings

Fig. 1 is a schematic view of the external structure of an embodiment of the present utility model.

Fig. 2 is a schematic diagram of the front structure of the indication panel in the embodiment of the utility model.

Fig. 3 is a schematic structural diagram of a substrate according to an embodiment of the present utility model.

Fig. 4 is a schematic structural diagram of a control circuit board according to an embodiment of the present utility model.

Fig. 5 is a schematic circuit diagram of a spare battery switch assembly according to an embodiment of the present utility model.

Fig. 6 is a schematic circuit diagram of a power switch assembly in an embodiment of the utility model.

Fig. 7 is a schematic circuit diagram of a brightness adjustment knob assembly according to an embodiment of the utility model.

Fig. 8 is a schematic circuit diagram of a light switch assembly and an auxiliary switch assembly in an embodiment of the present utility model.

Fig. 9 is a schematic circuit diagram of a propeller heating switch in an embodiment of the present utility model.

Fig. 10 is a schematic circuit diagram of a portion of a switching signal acquisition circuit according to an embodiment of the present utility model.

Fig. 11 is a schematic circuit diagram of another part of the switching signal acquisition circuit in an embodiment of the present utility model.

Fig. 12 is a schematic circuit interface diagram of a data processing module according to an embodiment of the present utility model.

Fig. 13 is a schematic circuit diagram of a backlight LED lamp according to an embodiment of the present utility model.

Detailed Description

The utility model will now be further described with reference to the accompanying drawings and examples, embodiments of which include, but are not limited to, the following examples.

Examples

As shown in fig. 1 to 13, the aircraft switch panel simulation device is mainly used for performing flight simulation operation on a switch panel of a Saussner C172 type, and comprises an L-shaped substrate 2, an indication panel 3 which is attached to the front surface of the substrate in a matching manner, a standby battery area 4, a power supply control area 5, a brightness adjustment area 6, a light control area 7 and an auxiliary function control area 8 which are arranged on the indication panel according to operation functions, a plurality of hollow holes 9 which are respectively arranged on the substrate and the indication panel in a penetrating manner according to the areas, a control circuit board 10 which is kept at a certain interval with the back surface of the substrate and is connected with the substrate through studs, a standby battery switch assembly which is arranged on the control circuit board and is presented on the standby battery area through the corresponding hollow holes, a power supply switch assembly which is arranged on the back surface of the substrate through the corresponding hollow holes and is electrically connected with the control circuit board, a light control knob assembly which is arranged on the back surface of the substrate through the corresponding hollow holes, a light switch assembly which is presented on the light control area through the corresponding hollow holes, a light control module which is arranged on the control circuit board and is provided with the corresponding hollow holes, a data acquisition module which is arranged on the auxiliary battery module, a data acquisition module which acquires signals and the data, the data acquisition module which acquires the data, the data acquisition module and the data acquisition module which acquires the data, the interface component is used for supplying power and outputting the input signals after data processing.

Specifically, the standby battery area 4 is configured at the upper position of the L-shaped vertical edge on the indication panel, the standby battery switch assembly comprises a standby battery switch 11 electrically connected with the switch signal acquisition circuit, and a test indicator 12 electrically connected with the data processing module, the standby battery switch adopts a three-gear toggle switch, and the deflector rod and the test indicator of the three-gear toggle switch extend out of the front surface of the indication panel through hollow holes at corresponding positions of the deflector rod and the test indicator. As shown in fig. 5, which is a schematic circuit diagram of the spare battery switch assembly, symbols STDBY and TEST respectively represent the three-gear toggle switch and the TEST indicator lamp with corresponding functions, interfaces SW13 and SW14 are used for connecting the switch signal acquisition circuit, the intermediate spare gear corresponds to the OFF gear, and interface PC13 is used for receiving signals from the data processing module to perform TEST instructions.

Specifically, the power supply control area 5 is configured at the middle position of the L-shaped vertical edge on the indication panel, the power supply switch assembly comprises a main electric gate generator switch 13, a battery switch 14, a first system change-over switch 15 and a second system change-over switch 16 which are electrically connected with the switch signal acquisition circuit, the main electric gate generator switch and the battery switch share a double-gear double-position ship-shaped switch, the first system change-over switch and the second system change-over switch share a double-gear double-position ship-shaped switch, the double-gear double-position ship-shaped switch is fixedly connected with the substrate, and the keycaps of the double-gear double-position ship-shaped switch are exposed out of the indication panel through hollowed holes at the corresponding positions of the double-gear double-position ship-shaped switch; specifically, the upper edge of the double-gear double-position ship-shaped switch is clamped and fixed in the square hole-shaped hollowed hole at the position, the connector lug at the lower part is connected to the control circuit board through a wire, the corresponding hole can be formed at the position of the control circuit board in consideration of the placement space so as to ensure that the ship-shaped switch does not interfere with the control circuit board, and the upper end key cap of the double-gear double-position ship-shaped switch can be provided with a switch cap with a corresponding shape according to the appearance requirement of the simulation device. Referring to fig. 6, which shows a schematic circuit diagram of a power supply switch assembly, symbols MASTER and AVION represent dual-gear dual-bit boat-type switches, and interfaces SW9, SW10, SW11 and SW12 are used for connecting a switch signal acquisition circuit.

Specifically, the brightness adjusting area 6 is configured at a position of the lower vertical edge of the L shape on the indication panel, the brightness adjusting knob assembly includes a panel brightness adjusting knob 17, a standby brightness adjusting knob 18, a base brightness adjusting knob 19 and an avionic brightness adjusting knob 20 which are electrically connected with the data processing module and are arranged in a matrix, all adopt rotary encoders with the model EC11, the upper part of the rotary encoder is connected and fixed with the base plate, the connector lug at the lower part is connected to the control circuit board through a wire, a corresponding hole can be formed at the position of the control circuit board in consideration of the placement space to ensure that the rotary encoder does not interfere with the control circuit board, the rotary rod of the rotary encoder extends out of the front surface of the indication panel through the hollowed hole at the corresponding position of the rotary encoder, and the rotary rod is provided with a knob cap to facilitate the rotary adjusting operation. As shown in fig. 7, which is a schematic circuit diagram of the brightness adjustment knob assembly, symbols SWICB1, STBY1, PED1, AV1 respectively represent rotary encoders with their corresponding functions, and interfaces PA2, PA3, PA4, PA5 are used to connect the data processing modules.

Specifically, the light control area 7 is configured at the upper position of the L-shaped horizontal edge on the indication panel, the light switch assembly comprises an anti-collision light switch 21, a landing light switch 22, a sliding light switch 23, a navigation light switch 24 and a stroboscopic light switch 25 which are electrically connected with the switch signal acquisition circuit and are arranged in a horizontal row, two-gear toggle switches are adopted, and a deflector rod of each two-gear toggle switch extends out of the front surface of the indication panel through a hollowed hole at the corresponding position of the deflector rod. As shown in fig. 8, which is a schematic circuit diagram of the light switch assembly and the auxiliary switch assembly, the symbol BEACON, LAND, TAXI, NAV, STROBE respectively represents two-stage toggle switches with corresponding functions, and the interfaces SW1, SW2, SW3, SW4, SW8 are used for the switch signal acquisition circuit.

Specifically, the auxiliary function control area 8 is configured at a position on the indication panel, where the horizontal edge of the L shape is located below, and the auxiliary switch assembly includes a fuel pump switch 26, a pitot tube heating device switch 27, a cabin power switch 28, and a propeller heating switch 29, which are electrically connected with the switch signal acquisition circuit and are arranged in a horizontal row, and two-gear toggle switches are adopted, where a deflector rod of the two-gear toggle switch extends out of the front surface of the indication panel through a hollowed hole at a corresponding position of the deflector rod. As shown in fig. 8, which is a schematic circuit diagram of the light switch assembly and the auxiliary switch assembly, the symbol FUEL, PITOT, CABIN respectively represents two-gear toggle switches with corresponding functions, and the interfaces SW5, SW6 and SW7 are used for a switch signal acquisition circuit; as shown in fig. 9, which is a schematic circuit diagram of a heating switch of a propeller, symbol PROP represents the two-gear toggle switch, and interfaces SW15 and SW16 are used for connecting a switch signal acquisition circuit, and the middle of the switch signal acquisition circuit can be used for corresponding to an OFF gear by spare first-gear wiring.

Specifically, the switch signal acquisition circuit adopts a register chip with the model of XL74HC165 to acquire signals output by corresponding two-gear toggle switches, the model register chip is 8-bit input, so two register chips with the model are configured to acquire signals of each switch component, and the two register chips can be connected in cascade or respectively connected with the data processing module, and in the embodiment, a mode of respectively connecting the two register chips is adopted. As shown in fig. 10 and 11, which are schematic circuit diagrams of the switch signal acquisition circuit, interfaces SW1 to SW8 are respectively used for connecting corresponding two-gear button switches of the light switch assembly and the auxiliary switch assembly, interfaces PB12, PB13 and PB14 are respectively used for connecting the data processing module, interfaces SW9 to SW16 are respectively used for connecting a double-gear double-bit boat-shaped switch of the power supply switch assembly and corresponding two-gear button switches of the spare battery switch assembly and the auxiliary switch assembly, and interfaces PB5, PB8 and PB9 are respectively used for connecting the data processing module.

Specifically, the data processing module uses an STM32 development board as a core, as shown in fig. 12, an interface PC13 is used for connecting a test indicator of a spare battery switch assembly, interfaces PA2, PA3, PA4, PA5 are used for connecting a brightness adjusting knob assembly, interfaces PB5, PB8, PB9, PB12, PB13, PB14 are used for connecting two register chips of a switch signal acquisition circuit, interfaces PA11, PA12 are used for connecting an interface assembly for signal transmission, and interface PB0 is used for connecting a backlight LED lamp.

Specifically, the interface component adopts a USB interface or a Type-C interface, so that signal transmission and power supply can be realized simultaneously.

For convenient operation indication and check, the indication panel is provided with a light transmission indication part 30 corresponding to the standby battery cell area, the power supply control area, the brightness adjustment area, the light control area and the auxiliary function control area for indicating the name of each component function in each area, and the control circuit board is provided with backlight LED lamps 31 corresponding to the light transmission indication part, and the backlight LED lamps are electrically connected with the data processing module. Referring to fig. 13, a schematic circuit diagram of a backlight LED lamp is shown, and a similar number of backlight LED lamps, such as LED1, LED2, LED3, etc., are configured according to the backlight indication requirement, and are connected to the data processing module through an interface PB 0.

When the flight simulation system is used, the flight simulation system needs to be matched with corresponding other simulation equipment, and a computer provided with flight simulation software needs to be connected for flight simulation training or experience. The USB or type-C interface is externally connected with power supply and flight simulation software signal data transmission, the corresponding switch component is switched to realize the required function switch or switch, for example, a standby battery switch can be switched on when a main power supply system of an airplane fails, the standby battery is used for supplying power to the most important system (communication, navigation, engine ignition, engine indication system and the like) of the airplane so as to ensure the power consumption requirement of the minimum safe flight, for example, a main electric gate generator switch and a battery switch can be operated to restart a motor when the power supply of a generator is insufficient or no longer supplied, for example, the first system change-over switch and the second system change-over switch can switch the used system one (BUS 1) or system two (BUS 2), for example, each switch of the brightness adjusting area can carry out dimming adjustment control on a radio and a panel, for example, each switch of the light control area light can respectively carry out opening and closing control on an anti-collision lamp, a landing lamp, a sliding lamp, a navigation lamp, a stroboscopic lamp and the like, and each switch of the auxiliary function control area carries out opening and closing on corresponding functions, such as a fuel pump, a pitot tube heating device, a cabin power supply, a propeller heating and the like. After the operation signals of the switches are acquired by the switch signal acquisition circuit or the data processing module STM32, the operation signals are processed by the STM32 and transmitted to an external flight simulation system through an interface component, so that corresponding switch function control is realized.

The above embodiments are only preferred embodiments of the present utility model, and not intended to limit the scope of the present utility model, but all changes made by adopting the design principle of the present utility model and performing non-creative work on the basis thereof shall fall within the scope of the present utility model.

Claims (10)

1. The utility model provides an aircraft switch panel analogue means, a serial communication port, including being the base plate of L shape, paste the front instruction panel of arranging in the base plate in the front of ground, dispose in the spare battery district on the instruction panel according to the operation function, the power supply control district, brightness adjustment district, light control district and auxiliary function control district, a plurality of fretwork holes of seting up on base plate and instruction panel are run through respectively according to the region, keep certain interval and pass through the control circuit board that stud and base plate are connected with the base plate back, settle on the control circuit board and present the spare battery switch subassembly in spare battery district through corresponding fretwork holes, install at the base plate back and present at the power supply control district through corresponding fretwork holes and with the power supply switch subassembly that control circuit board electricity is connected, install at the base plate back and present at the light switch subassembly of light control district through corresponding fretwork holes, settle on the control circuit board and present at the auxiliary switch subassembly of auxiliary function control district through corresponding fretwork holes, and settle on the control circuit board interface subassembly, wherein, dispose on the control circuit board and present at the spare battery switch subassembly through corresponding fretwork holes and the power supply control circuit board electricity, the power supply module is used for signal processing module is input to the signal processing module and is used for sending data to the data input to the spare power supply module, the signal processing module is used for processing the data input to the data processing module.

2. The aircraft switch panel simulation device according to claim 1, wherein the standby battery area is configured at the upper position of the L-shaped vertical edge on the indication panel, the standby battery switch assembly comprises a standby battery switch electrically connected with the switch signal acquisition circuit, and a test indicator electrically connected with the data processing module, the standby battery switch adopts a three-gear toggle switch, and a deflector rod of the three-gear toggle switch and the test indicator extend out of the front surface of the indication panel through hollowed holes at corresponding positions of the deflector rod and the test indicator.

3. The aircraft switch panel simulation device according to claim 2, wherein the power supply control area is configured at an intermediate position of an L-shaped vertical edge on the indication panel, the power supply switch assembly comprises a main electric gate generator switch, a battery switch, a first system change-over switch and a second system change-over switch which are electrically connected with the switch signal acquisition circuit, the main electric gate generator switch and the battery switch share a double-gear double-position ship-shaped switch, the first system change-over switch and the second system change-over switch share a double-gear double-position ship-shaped switch, the double-gear double-position ship-shaped switch is fixedly connected with the substrate, and the keycaps of the double-gear double-position ship-shaped switch are exposed out of the indication panel through hollowed holes at corresponding positions of the double-gear double-position ship-shaped switch.

4. The aircraft switch panel simulation device according to claim 3, wherein the brightness adjustment area is configured at a position on the indication panel, which is located below the vertical edge of the L shape, the brightness adjustment knob assembly comprises a panel brightness adjustment knob, a standby brightness adjustment knob, a base brightness adjustment knob and an avionic brightness adjustment knob which are electrically connected with the data processing module and are arranged in a matrix, rotary encoders with model EC11 are adopted, a rotary rod of the rotary encoder extends out of the front face of the indication panel through hollowed holes at corresponding positions of the rotary encoder, and a knob cap is configured on the rotary rod.

5. The aircraft switch panel simulation device according to claim 4, wherein the light control area is configured at an upper position of an L-shaped transverse edge on the indication panel, the light switch assembly comprises an anti-collision light switch, a landing light switch, a sliding light switch, a navigation light switch and a stroboscopic light switch which are electrically connected with the switch signal acquisition circuit and are arranged in a transverse row, two-gear toggle switches are adopted, and a deflector rod of each of the two-gear toggle switches extends out of the front surface of the indication panel through a hollowed hole at a corresponding position of the deflector rod.

6. The aircraft switch panel simulation device according to claim 5, wherein the auxiliary function control area is configured at a position on the indication panel, which is close to the lower side of the L-shaped transverse edge, and the auxiliary switch assembly comprises a fuel pump switch, a pitot tube heating device switch, a cabin power switch and a propeller heating switch which are electrically connected with the switch signal acquisition circuit and are arranged in a transverse row, two-gear toggle switches are adopted, and a deflector rod of each of the two-gear toggle switches extends out of the front surface of the indication panel through a hollowed hole at the corresponding position of the deflector rod.

7. The aircraft switch panel simulation device according to claim 6, wherein the switch signal acquisition circuit acquires signals output by corresponding two-gear toggle switches by using a register chip with a model number of XL74HC 165.

8. The aircraft switch panel simulation device according to claim 7, wherein the data processing module is implemented using an STM32 development board as a core.

9. The aircraft switch panel simulation device according to claim 8, wherein the interface component employs a USB interface or a Type-C interface.

10. The aircraft switch panel simulation device according to any one of claims 1 to 9, wherein the indication panel is provided with a light-transmitting indication part corresponding to the standby battery cell area, the power supply control area, the brightness adjustment area, the light control area and the auxiliary function control area, the light-transmitting indication part is used for indicating the name of each component function in each area, and the control circuit board is provided with backlight LED lamps corresponding to the light-transmitting indication part, and the backlight LED lamps are electrically connected with the data processing module.