CN218767881U - Aircraft external lighting control box simulation device - Google Patents
Aircraft external lighting control box simulation device Download PDFInfo
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- CN218767881U CN218767881U CN202223588162.0U CN202223588162U CN218767881U CN 218767881 U CN218767881 U CN 218767881U CN 202223588162 U CN202223588162 U CN 202223588162U CN 218767881 U CN218767881 U CN 218767881U
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Abstract
The utility model discloses an aircraft external lighting control box analogue means, include and form the inside shell body that is the rectangle form that has the device and hold the cavity by front panel and back housing interconnect, set up side by side in the front panel openly lean on the navigation light of last position bright dark switch, the navigation light steadily dodges the switch, formation lamp option knob and crashproof lamp/pull option switch, set up side by side in the front panel openly leans on the outer main lighting switch of lower position, refuel the lighting switch in the air, refuel illumination brightness control knob and crashproof lamp option knob in the air, settle in the device holds the control circuit board in the cavity, and dispose the interface module on the back housing. The utility model discloses utilize electronic circuit structural design external lighting to dial shelves switch and rotary switch and simulate the operating function of the external lighting control box on owl dragon model right control platform, realize the simplification to real quick-witted physical structure operating element, for the user provide with real quick-witted operation does not basically have the use of difference and experience, reduced the manufacturing cost of device.
Description
Technical Field
The utility model relates to a flight simulation equipment, specifically say, relate to an aircraft external lighting control box analogue means, mainly used for the simulation of external lighting control box EXT _ LIG on owl dragon model right control platform.
Background
With the rapid development of civil aviation industry in China, the opening of airspace in China and the relaxation of personal flight driving licenses, various flight experience equipment and flight simulators become more concerned, and the model simulation is gradually expanded from a civil model to a battle model. The owl dragon model is one of the disclosed classical models, and can provide a simulation operation basis for pilot training and flight enthusiasts to know and experience fighter operations.
The existing flight simulator is mainly in a flight simulation software form, various operation panels of the existing flight simulator basically adopt a virtual key mode of a touch screen, the experience feeling of a user is poor, and the mode of adopting real machine equipment for experience is high in cost and is not suitable for wide use; on the other hand, flight simulation equipment specially aiming at the owl dragon fighter type is not available in the market at present. Therefore design operation experience and feel outstanding and low-cost flight analog device is the needs of pressing need in this field, the utility model relates to a simulation of outer lighting control box on owl dragon model right control cabinet of mainly used.
SUMMERY OF THE UTILITY MODEL
To the problem that above-mentioned prior art exists, the utility model provides an aircraft external lighting control box analogue means of mainly used owl dragon model has realized simulating the right control cabinet external lighting control box of owl dragon model through low-cost structural design, makes things convenient for pilot training and flight fan to experience the fighter operation.
In order to realize the purpose, the utility model discloses a technical scheme as follows:
the simulator comprises a rectangular shell, a navigation light brightness switch, a navigation light steady flashing switch, a formation light selection knob, an anti-collision light/traction selection switch, an external main lighting switch, an air refueling lighting brightness adjustment knob and an anti-collision light selection knob, wherein the shell is formed by mutually connecting a front panel and a rear cover, the navigation light brightness switch, the navigation light steady flashing switch, the formation light selection knob and the anti-collision light/traction selection switch are arranged in parallel at the upper position of the front surface of the front panel, the external main lighting switch, the air refueling lighting brightness adjustment knob and the anti-collision light selection knob are arranged in the front surface of the front panel, the control circuit board is arranged in the device accommodating cavity and used for bearing the switches and the adjustment knob, and an interface assembly is arranged on the rear cover and electrically connected with the control circuit board, wherein an operation signal acquisition circuit and a data processing module are arranged on the control circuit board, the operation signal acquisition circuit is used for acquiring input signals of the navigation light brightness switch, the navigation light steady flashing switch, the formation light selection knob, the anti-collision light/traction selection switch, the main external lighting switch, the air refueling lighting switch, the anti-collision light illumination brightness adjustment knob and the anti-collision light selection knob, and the interface assembly is used for supplying power to the data processing module and outputting the input signals to the external processing module.
Specifically, the navigation light and darkness switch and the main external lighting switch are three-gear button switches and are electrically connected with the operation signal acquisition circuit, and the deflector rod of the navigation light and darkness switch extends out of the front face plate through a hollow hole arranged in a corresponding position on the front face plate.
Specifically, the navigation light steady flashing switch, the anti-collision light/traction selection switch and the air refueling lighting switch adopt two-gear button switches and are electrically connected with the operation signal acquisition circuit, and the deflector rod of the navigation light steady flashing switch extends out of the front face of the front panel through a hollow hole arranged at a corresponding position on the front panel.
Specifically, formation lamp selection knob and crashproof lamp selection knob adopt the multi-gear knob switch that the model is RS17, all configure to six grades to all be connected with the operating signal acquisition circuit electricity, its swing arm stretches out in the front panel openly through the fretwork hole that corresponds the position configuration on the front panel, and dispose the knob cap on its swing arm.
Specifically, the air refueling illumination brightness adjustment knob adopts a rotary encoder with the model number of EC11 and is electrically connected with the operation signal acquisition circuit, a rotary rod of the air refueling illumination brightness adjustment knob extends out of the front face of the front panel through a hollow hole arranged at a corresponding position on the front panel, and a knob cap is arranged on the rotary rod.
Specifically, the operation signal acquisition circuit adopts a register chip with the model 74HC165D to acquire input signals of each button switch, the multi-gear button switch and the rotary encoder.
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.
Specifically, the positions of the front panel corresponding to a navigation light bright and dark switch, a navigation light steady flashing switch, a formation light selection knob, an anti-collision light/traction selection switch, an external main lighting switch, an air refueling lighting brightness adjustment knob and an anti-collision light selection knob are provided with light-transmitting indication parts for indicating the functions of each switch and each knob, the control circuit board is provided with backlight LED lamps corresponding to the light-transmitting indication parts, and the backlight LED lamps are all electrically connected with the data processing module.
Compared with the prior art, the utility model discloses following beneficial effect has:
(1) The utility model discloses utilize electronic circuit structural design external lighting to dial shelves switch and rotary switch and simulate the operating function of the external lighting control box on owl dragon model right control platform, thereby realize the simplification to real quick-witted physical structure operating elements, cooperation signal acquisition circuit and data processing module are to driving lever and knob operating signal's collection and processing, the function that combines external flight analog system can realize the simulation of owl dragon model right control platform external lighting control box effectively and use, thereby for the user provide with real machine demonstration and operate indiscriminate use experience basically, the manufacturing cost of device has greatly been reduced. The utility model relates to an ingenious, simple structure, low cost, convenient to use is suitable for and uses in flight analog device.
(2) The utility model discloses lighting control's such as main illumination outside the machine, navigation light, crashproof lamp actual operation mode designs two shelves or three shelves toggle, many shelves rotary switch respectively pertinence ground and operates the device simulation, has both guaranteed the low cost that electronic device replaced, and accurate simulation has realized each operating function again to realized the knob regulation analog function to the lighting control box outside the real machine reliably, improved user's immersive experience.
(3) The utility model discloses a STM32 development board has reduced the hardware cost effectively as data processing module's core on guaranteeing the performance of use basis, adopts the interface of USB/Type-C interface as signal transmission and power supply simultaneously, can conveniently and simply hookup with other flight analog device.
Drawings
Fig. 1 is a schematic diagram of an external structure of an embodiment of the present invention.
Fig. 2 is a front structural view of a front panel according to an embodiment of the present invention.
Fig. 3 is a schematic structural diagram of a control circuit board according to an embodiment of the present invention.
Fig. 4 is a schematic circuit diagram of a toggle switch according to an embodiment of the present invention.
Fig. 5 is a schematic circuit diagram of an RS17 multi-stage rotary switch according to an embodiment of the present invention.
Fig. 6 is a schematic circuit diagram of a rotary encoder according to an embodiment of the present invention.
Fig. 7 is a schematic circuit diagram of a register chip according to an embodiment of the present invention.
Fig. 8 is a schematic circuit interface diagram of a data processing module according to an embodiment of the present invention.
Detailed Description
The present invention will be further described with reference to the following drawings and examples, and embodiments of the present invention include, but are not limited to, the following examples.
Examples
As shown in fig. 1 to 8, the simulator for the external illumination control box of the aircraft is mainly used for flight simulation operation of the external illumination control box on the right console of the owl dragon model, and comprises a rectangular outer shell formed by connecting a front panel 1 and a rear housing 2, an aircraft light and dark switch 3, an aircraft light steady flashing switch 4, a formation light selection knob 5 and an anti-collision light/traction selection switch 6 which are arranged in parallel at the upper position of the front panel, an external main illumination switch 7, an air refueling illumination switch 8, an air refueling illumination brightness adjustment knob 9 and an anti-collision light selection knob 10 which are arranged in parallel at the lower position of the front panel, a control circuit board 11 which is arranged in the device housing and used for bearing the switches and the adjustment knobs, and an interface component which is arranged on the rear housing and electrically connected with the control circuit board, wherein the control circuit board is provided with an operation signal acquisition circuit and a data processing module, the operation signal acquisition circuit is used for acquiring the aircraft light and dark switches, the aircraft light steady flashing switch, the formation light selection knob, the anti-collision light/traction selection knob, the main illumination switch, the oil refueling illumination switch and the anti-collision light selection knob are used for acquiring data processing module for acquiring and inputting data to the air refueling data processing module.
Specifically, the navigation light brightness switch and the main lighting switch outside the aircraft adopt a three-gear button switch 13, the navigation light steady flashing switch, the anti-collision light/traction selection switch and the air refueling lighting switch adopt two-gear button switches 14 and are electrically connected with the operation signal acquisition circuit, and a deflector rod of the navigation light brightness switch and the main lighting switch outside the aircraft extends out of the front surface of the front panel through a hollow hole 12 arranged at a corresponding position on the front panel. As shown in the circuit schematic diagram of the button switch in FIG. 4, the symbols BRT, ANTI-COL, NORMAL, FLASH, AAR-ON represent the corresponding button switches with their corresponding functions, and the interfaces K1-K6 and K21 are used for connecting the operation signal acquisition circuit.
Specifically, formation lamp selection knob and crashproof lamp selection knob adopt the multi-gear knob switch 15 that the model is RS17, all configure to six grades to all be connected with the operating signal acquisition circuit electricity, its swing arm stretches out in the front panel openly through the fretwork hole that corresponds the position configuration on the front panel, and dispose the knob cap on its swing arm. As shown in the schematic circuit diagram of a multi-gear knob switch in FIG. 5, the symbol format represents the multi-gear knob switch with its corresponding function, and the interfaces K9-K14 are used to connect the operation signal acquisition circuit.
Specifically, the air refueling illumination brightness adjustment knob adopts a rotary encoder 16 with the model of EC11, and is electrically connected with the operation signal acquisition circuit, a rotary rod of the knob extends out of the front face of the front panel through a hollow hole arranged at a corresponding position on the front panel, and a knob cap is arranged on the rotary rod. As shown in the schematic circuit diagram of the rotary encoder shown in fig. 6, the symbol AAR-BRT represents the rotary encoder with its corresponding function, and the interfaces K7 and K8 are used for connecting the operation signal acquisition circuit.
Specifically, the operation signal acquisition circuit adopts a register chip with the model of 74HC165D to acquire input signals of each button switch, the multi-gear button switch and the rotary encoder, the register chip with the model of 8-bit input is adopted, and for 21 interfaces of each button switch, the multi-gear button switch and the rotary encoder, the input signal acquisition is realized in a cascading mode of three register chips. As shown in fig. 7, which is a schematic circuit diagram of a register chip, the interfaces K15 to K21 are respectively used for connecting corresponding 5 interfaces to realize operation signal acquisition, the interfaces 165DATA, 165LATCH, and 165CLK are used for connecting corresponding interfaces of the DATA processing module STM32, and the SI pin is used for connecting a QH pin of a previous register chip to realize cascade input.
Specifically, the DATA processing module adopts an STM32 development board as a core, as shown in fig. 8, the interfaces 165DATA, 165LATCH and 165CLK are used for connecting a key position signal acquisition circuit, and the interfaces USBD + and USBD-are used for connecting an interface component for signal transmission.
Specifically, the interface assembly adopts a USB interface or a Type-C interface, and can simultaneously realize signal transmission and power supply.
In addition, the backlight LED lamps can be configured on the control circuit board according to actual use requirements, and the backlight simulation effect of the panel is achieved.
The utility model discloses need cooperate corresponding other analog device to use during the use to need to connect the computer of installing flight simulation software and fly simulation training or experience. The system is characterized in that a USB or type-C interface is externally connected with power supply and flight simulation software for signal data transmission, a navigation light bright and dark switch, a navigation light stable flashing switch, a formation light selection knob, an anti-collision light/traction selection switch, an external main lighting switch, an air refueling lighting brightness adjusting knob and an anti-collision light selection knob are turned or rotated to realize the operation of corresponding functions, and operation signals are collected by an operation signal collecting circuit and then transmitted to an external flight simulation system through a data processing module and an interface component to realize the corresponding external lighting control.
The above-mentioned embodiment is only the preferred embodiment of the present invention, and is not a limitation to the protection scope of the present invention, but all the changes made by adopting the design principle of the present invention and performing non-creative work on this basis should belong to the protection scope of the present invention.
Claims (9)
1. The simulation device is characterized by comprising a rectangular outer shell, a navigation light brightness switch, a navigation light steady flashing switch, a formation light selection knob, an anti-collision light/traction selection switch, an external main lighting switch, an air refueling lighting brightness adjustment knob and an anti-collision light selection knob, wherein the outer shell is formed by mutually connecting a front panel and a rear cover and internally provided with a device accommodating cavity, the navigation light brightness switch, the navigation light steady flashing switch, the formation light selection knob and the anti-collision light/traction selection switch are arranged at the upper position of the front surface of the front panel side by side, a control circuit board is arranged in the device accommodating cavity and used for bearing the switches and the adjustment knob, and an interface component is arranged on the rear cover and electrically connected with the control circuit board, wherein an operating signal acquisition circuit and a data processing module are arranged on the control circuit board, the operating signal acquisition circuit is used for acquiring input signals of the navigation light brightness switch, the navigation light steady flashing switch, the formation light selection knob, the anti-collision light/traction selection switch, the external main lighting switch, the air refueling lighting brightness adjustment knob and the anti-collision light selection switch and the interface component are used for outputting the input signals to the data processing module.
2. The simulator of claim 1, wherein the navigation light switch, the anti-collision light/traction selection switch and the main off-board lighting switch are three-position toggle switches and are electrically connected to the operation signal acquisition circuit, and the shift lever thereof extends out of the front surface of the front panel through a hollow hole disposed at a corresponding position on the front panel.
3. The simulator of claim 2, wherein the navigation light flashing switch, the anti-collision light/traction selection switch and the air refueling lighting switch are two-stage button switches and are electrically connected with the operation signal acquisition circuit, and the deflector rod of the simulator extends out of the front surface of the front panel through a hollow hole arranged at a corresponding position on the front panel.
4. The aircraft outboard lighting control box simulation device of claim 3, wherein the formation lamp selection knob and the anti-collision lamp selection knob are multi-shift knob switches with model number RS17, are configured to six shifts, and are electrically connected to the operation signal acquisition circuit, the rotary rod of the rotary rod extends out of the front surface of the front panel through a hollow hole configured at a corresponding position on the front panel, and a knob cap is configured on the rotary rod.
5. The aircraft outboard lighting control box simulation device of claim 4, wherein said air refueling lighting brightness adjusting knob is a rotary encoder of type EC11 and is electrically connected with the operation signal acquisition circuit, a rotary rod thereof extends out of the front face of the front panel through a hollow hole disposed at a corresponding position on the front panel, and a rotary rod thereof is disposed with a knob cap.
6. The aircraft off-board lighting control box simulation device of claim 5, wherein the operation signal acquisition circuit adopts a register chip of type 74HC165D to acquire input signals of each of the toggle switch, the multi-gear knob switch and the rotary encoder.
7. The aircraft outboard lighting control box simulation device of claim 6, wherein said data processing module uses an STM32 development board as a core.
8. The aircraft external lighting control box simulation device of claim 7, wherein the interface component adopts a USB interface or a Type-C interface.
9. The simulation device of an aircraft external illumination control box according to claim 8, wherein light-transmitting indicators are disposed on the front panel at positions corresponding to the position of the navigation light on/off switch, the navigation light steady flashing switch, the formation light selection knob, the anti-collision light/traction selection switch, the external main illumination switch, the air refueling illumination brightness adjustment knob and the anti-collision light selection knob for indicating the functions of each switch and knob, and the control circuit board is provided with backlight LED lamps corresponding to the light-transmitting indicators, and the backlight LED lamps are electrically connected with the data processing module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223588162.0U CN218767881U (en) | 2022-12-31 | 2022-12-31 | Aircraft external lighting control box simulation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223588162.0U CN218767881U (en) | 2022-12-31 | 2022-12-31 | Aircraft external lighting control box simulation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218767881U true CN218767881U (en) | 2023-03-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223588162.0U Active CN218767881U (en) | 2022-12-31 | 2022-12-31 | Aircraft external lighting control box simulation device |
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| CN (1) | CN218767881U (en) |
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- 2022-12-31 CN CN202223588162.0U patent/CN218767881U/en active Active
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