CN218767880U - Aircraft cabin lighting control box analogue means - Google Patents
Aircraft cabin lighting control box analogue means Download PDFInfo
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- CN218767880U CN218767880U CN202223581405.8U CN202223581405U CN218767880U CN 218767880 U CN218767880 U CN 218767880U CN 202223581405 U CN202223581405 U CN 202223581405U CN 218767880 U CN218767880 U CN 218767880U
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Abstract
The utility model discloses an aircraft cabin lighting control box analogue means, including being the back lid shell that the rectangle form just has the device and hold the cavity, settle in the apron that the closure device holds the cavity on the back lid shell, paste and put in the positive indicator panel of apron, three side by side and set up the fretwork hole on indicator panel and apron with running through, settle the instrument illumination knob subassembly in three fretwork hole respectively, control cabinet illumination knob subassembly and floodlight knob subassembly, settle in the device and hold the control circuit board in the cavity to and settle the interface module that is connected on the back lid shell and with the control circuit board electricity. The utility model discloses utilize the electronic circuit structure knob subassembly that rotatory potentiometre constitutes to simulate the operating function of owl dragon model passenger cabin lighting control box to the realization is to the simplification of the real quick-witted physical structure operating means of passenger cabin lighting control box, for the user provide with real quick-witted demonstration and operate the use experience that does not basically have the difference, reduced the manufacturing cost of device.
Description
Technical Field
The utility model relates to a flight simulation equipment, specifically say, relate to an aircraft cabin lighting control box analogue means, the cabin lighting control box INT _ LTS simulation on the right control cabinet of mainly used owl dragon model.
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 application; 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 and need for urgent need in this field, the utility model relates to a simulation of passenger cabin lighting control box on owl dragon model right control cabinet is mainly used for.
SUMMERY OF THE UTILITY MODEL
To the problem that above-mentioned prior art exists, the utility model provides an aircraft passenger cabin lighting control box analogue means of mainly used owl dragon model has realized the simulation to the passenger cabin lighting control box on owl dragon model right control cabinet 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 adopts the technical scheme as follows:
the utility model provides an aircraft cabin lighting control box analogue means, including being the rectangle form and having the back cover shell that the device holds the cavity, settle in the back cover shell on the closed device hold the cavity the apron, paste the instruction panel of putting in the apron openly, three fretwork hole that sets up in instruction panel and apron side by side and run through, instrument illumination knob subassembly, control cabinet illumination knob subassembly and floodlight knob subassembly that settle respectively in three fretwork hole, settle in the device holds the control circuit board that the cavity is used for bearing instrument illumination knob subassembly, control cabinet illumination knob subassembly and floodlight knob subassembly, and dispose on the back cover shell and the interface module of being connected with the control circuit board electricity, wherein, dispose knob signal acquisition circuit and data processing module on the control circuit board, this knob signal acquisition circuit is used for gathering instrument illumination knob subassembly, control cabinet illumination knob subassembly and floodlight knob subassembly's input signal and transmitting for data processing module, the interface module is used for the power supply and outwards exports the input signal after data processing module is handled.
Specifically, instrument illumination knob subassembly, control cabinet illumination knob subassembly and floodlight knob subassembly all adopt the rotatory potentiometre that the model is RK097NS to all be connected with knob signal acquisition circuit electricity, the fretwork hole that the swing arm of rotatory potentiometre passes through its corresponding position stretches out in the indicating panel openly, and disposes the knob cap on the swing arm.
Specifically, the knob signal acquisition circuit adopts a register chip with the model 74HC165D to respectively acquire the signal output by each rotary potentiometer.
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 position that corresponds instrument illumination knob subassembly, control cabinet illumination knob subassembly and floodlight knob subassembly on the indicator panel disposes printing opacity indicating part for instruct every knob subassembly's function, be provided with the LED lamp in a poor light that corresponds with printing opacity indicating part on the control circuit board, these LED lamps in a poor light all are connected with data processing module electricity.
Compared with the prior art, the utility model discloses following beneficial effect has:
(1) The utility model discloses utilize the electronic circuit structure knob subassembly that rotatory potentiometre constitutes to simulate the operating function of owl dragon model passenger cabin lighting control box, thereby realize the simplification to the real quick-witted physical structure operating unit of passenger cabin lighting control box, cooperation signal acquisition circuit and data processing module gather and handle the operating signal of knob subassembly, the function that combines external flight analog system can realize the simulation of owl dragon model passenger cabin lighting control box effectively and use, thereby for the user provide with the real machine show 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 use the direct electronization ground of rotatory potentiometre to simulate the function that has realized instrument illumination knob, control cabinet illumination knob and floodlight knob, structurally combine casing and the fretwork hole above that to have guaranteed the unanimity with owl dragon model cabin lighting control box on the device appearance, improved user's immersive experience.
(3) The utility model discloses a signal acquisition of rotatory potentiometre is realized to 74HC 165D's register chip to adopt STM32 development board as data processing module's core, reduced the hardware cost effectively on guaranteeing the basis of performance, adopt USB/Type-C interface as the interface of signal transmission and power supply simultaneously, can conveniently couple with other flight analog device simply.
Drawings
Fig. 1 is a schematic diagram of an external structure of an embodiment of the present invention.
Fig. 2 is a schematic front structural diagram of an indication panel in an embodiment of the present invention.
Fig. 3 is a schematic circuit diagram of a rotary potentiometer according to an embodiment of the present invention.
Fig. 4 is a schematic circuit diagram of a register chip according to an embodiment of the present invention.
Fig. 5 is a schematic circuit interface diagram of a data processing module according to an embodiment of the present invention.
Fig. 6 is a schematic circuit diagram of a backlight LED lamp portion 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 6, the aircraft cockpit lighting control box simulator is mainly used for flight simulation operation of a cockpit lighting control box on a owl type right console, and comprises a rectangular rear cover shell 1 with a device accommodating cavity, a cover plate 2 which is arranged on the rear cover shell through screws and is used for closing the device accommodating cavity, an indicating panel 3 attached to the front surface of the cover plate, three hollowed holes 4 which are arranged on the indicating panel and the cover plate side by side and penetrate through, an instrument lighting knob assembly 4, an operation console lighting knob assembly 5 and a floodlight knob assembly 7 which are respectively arranged in the three hollowed holes, a control circuit board which is arranged in the device accommodating cavity and is used for bearing input signals of the instrument lighting knob assembly, the operation console lighting knob assembly and the floodlight knob assembly, and an interface assembly which is arranged on the rear cover shell and is electrically connected with the control circuit board, wherein a knob signal acquisition circuit and a data processing module are arranged on the control circuit board, the knob signal acquisition circuit is used for acquiring input signals of the instrument lighting knob assembly, the operation console lighting knob assembly and the floodlight knob assembly and transmitting the input signals to the data processing module, and the interface assembly is used for outputting the input signals to the data processing module.
Specifically, instrument illumination knob subassembly, control cabinet illumination knob subassembly and floodlight knob subassembly all adopt the rotatory potentiometre that the model is RK097NS to all be connected with knob signal acquisition circuit electricity, the fretwork hole that the swing arm of rotatory potentiometre passes through its corresponding position stretches out in the indicating panel openly, and disposes the knob cap on the swing arm. As shown in fig. 3, which is a schematic circuit diagram of a rotary potentiometer, symbols INST/DISPLAY, connections, and FLOOD represent the corresponding rotary potentiometer with their corresponding functions, and the interfaces K1 to K6 are used to connect a knob signal acquisition circuit.
Specifically, the knob signal acquisition circuit adopts a register chip with the model of 74HC165D to respectively acquire signals output by each rotary potentiometer, and the register chip with the model of 8-bit input can complete signal acquisition of three rotary potentiometers by adopting one register chip. As shown in fig. 4, which is a schematic circuit diagram of a register chip, the interfaces K1 to K6 are used for connecting corresponding rotary potentiometers to realize operation signal acquisition, and the interfaces 165DATA2, 165LATCH, and 165CLK are used for connecting corresponding interfaces of the DATA processing module STM 32.
Specifically, the DATA processing module adopts an STM32 development board as a core, as shown in fig. 5, the interfaces 165DATA2, 165LATCH, and 165CLK are used for connecting a knob signal acquisition circuit, and the interfaces USBD +, USBD-are used for connecting interface components 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.
For convenience of operation indication, a backlight LED lamp for light transmission indication at a designated position on the indication panel may be disposed on the control circuit board, as shown in fig. 6, 10 light emitting diodes D11 to D20 are connected in parallel, and are controlled to be turned on and off by the data processing module through power supply.
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 power supply and flight simulation software signal data transmission are externally connected through a USB (universal serial bus) or type-C (type-computer) interface, the corresponding functions of an adjusting instrument lighting knob, a console lighting knob and a floodlight knob are operated, operating signals are collected by a knob signal acquisition circuit and transmitted to an external flight simulation system through a data processing module to realize the corresponding functions, and a user can directly observe the indicating position of a knob cap and can also visually obtain the state indication of 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 (6)
1. The simulation device is characterized by comprising a rectangular rear cover shell with a device accommodating cavity, a cover plate arranged on the rear cover shell and used for closing the device accommodating cavity, an indicating panel attached to the front surface of the cover plate, three hollowed-out holes arranged on the indicating panel and the cover plate side by side and penetrating through the hollowed-out holes, an instrument illuminating knob component, a console illuminating knob component and a floodlight knob component which are arranged in the three hollowed-out holes respectively, a floodlight control circuit board arranged in the device accommodating cavity and used for bearing the instrument illuminating knob component, the console illuminating knob component and the floodlight knob component, and an interface component arranged on the rear cover shell and electrically connected with the control circuit board, wherein the control circuit board is provided with a knob signal acquisition circuit and a data processing module, the knob signal acquisition circuit is used for acquiring input signals of the instrument illuminating knob component, the console illuminating knob component and the floodlight knob component and transmitting the input signals to the data processing module, and the interface component is used for supplying power and outputting the input signals processed by the data processing module outwards.
2. The aircraft cockpit lighting control box simulator of claim 1, wherein the instrument lighting knob assembly, the console lighting knob assembly and the floodlight knob assembly each employ a rotary potentiometer of type RK097NS and are electrically connected to the knob signal acquisition circuit, a rotary rod of the rotary potentiometer extends out of the front face of the indication panel through a hollow hole at a corresponding position of the rotary potentiometer, and a knob cap is disposed on the rotary rod.
3. The aircraft cabin lighting control box simulation device of claim 2, wherein the knob signal acquisition circuit adopts a register chip with a model number of 74HC165D to respectively acquire the signal output by each rotary potentiometer.
4. The aircraft cabin lighting control box simulation device of claim 3, wherein the data processing module uses an STM32 development board as a core.
5. The aircraft cabin lighting control box simulation device of claim 4, wherein the interface component employs a USB interface or a Type-C interface.
6. The aircraft cockpit lighting control box simulator of claim 5, wherein light-transmitting indicators are disposed on said indicator panel at positions corresponding to said instrument lighting knob assembly, said console lighting knob assembly, and said floodlight knob assembly for indicating the functions of each of said knob assemblies, and said control circuit board has backlight LED lights corresponding to said light-transmitting indicators, said backlight LED lights being electrically connected to said data processing module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223581405.8U CN218767880U (en) | 2022-12-31 | 2022-12-31 | Aircraft cabin lighting control box analogue means |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223581405.8U CN218767880U (en) | 2022-12-31 | 2022-12-31 | Aircraft cabin lighting control box analogue means |
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| CN218767880U true CN218767880U (en) | 2023-03-28 |
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| CN202223581405.8U Active CN218767880U (en) | 2022-12-31 | 2022-12-31 | Aircraft cabin lighting control box analogue means |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113324550A (en) * | 2021-06-30 | 2021-08-31 | 维飞科技有限公司 | Flight path correction method based on improved flight path integral and storage medium |
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- 2022-12-31 CN CN202223581405.8U patent/CN218767880U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113324550A (en) * | 2021-06-30 | 2021-08-31 | 维飞科技有限公司 | Flight path correction method based on improved flight path integral and storage medium |
| CN113324550B (en) * | 2021-06-30 | 2024-03-26 | 维飞科技有限公司 | Track correction method based on improved track integration and storage medium |
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