CN210777306U - Simulator for aircraft control display assembly - Google Patents
Simulator for aircraft control display assembly Download PDFInfo
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- CN210777306U CN210777306U CN201921329892.4U CN201921329892U CN210777306U CN 210777306 U CN210777306 U CN 210777306U CN 201921329892 U CN201921329892 U CN 201921329892U CN 210777306 U CN210777306 U CN 210777306U
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Abstract
The utility model relates to an aircraft control display module simulator, including the casing, install button subassembly on the casing, be provided with power module and control assembly in the casing, button subassembly includes the key circuit board, and control assembly includes control panel and display screen, is provided with microprocessor on the control panel, key circuit board and microprocessor's input electric connection, microprocessor's output and display screen electric connection, microprocessor still are used for communicating with data terminal. The utility model relates to a rationally, the cost is lower and the durability is strong, be convenient for maintain, the fidelity is high, the simulation effect is showing, good experience effect has, make control display module simulator easy to maintain through key circuit board and control panel, installation convenient to use, occupation space is little, each module or whole dismouting mode all are unanimous with the control display module of true aircraft on this control display module simulator, provide a more true control display module study operational environment for the flight student.
Description
Technical Field
The utility model belongs to the technical field of the technique of flight emulation and specifically relates to an aircraft control display module simulator.
Background
With the high-speed development of the current civil aviation industry, the maintenance personnel and flight personnel of the civil aircraft are seriously lacked, the corresponding civil aviation talent training industry develops vigorously, and the corresponding training equipment is produced. The control display assembly, which is the most important component of an aircraft cockpit, appears in various forms at the relevant training authorities. With the discovery of science and technology and the improvement of teaching level, the simulation reproduction technology of the control display component of the airplane cockpit is also greatly improved.
The technical specialties such as the knowledge ability required to be mastered by the training subjects of the civil aviation training institutions and the like are relatively strong, and the experience is accumulated by the actual operation within a certain time. For example, aircraft maintenance personnel need to be skilled in mastering the functions and operation methods of the control display assembly in the aircraft cockpit; for the pilot to have more control over the meaning represented by the operating method and indicator lights of the control display assembly, which is the tool for the aircraft pilot to interact with the flight management computer of the aircraft, is the most used component of the pilot, there is a need for a training facility to provide a real or near-real aircraft cockpit control display assembly for training trainees to learn and operate with hands.
Currently, most training institutions use simulation equipment which uses a computer display to display the picture of a cockpit control display component, uses simulation software, and uses a mouse to operate keys, knobs and the like on the control display component. The simulation mode cannot provide a real cockpit environment, cannot feel the operation feeling of each button on the control display component, and cannot obtain a good learning effect.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an aircraft control display module simulator solves the aircraft control display module simulator on the existing market and can only use mouse to operate, does not have three-dimensional sensation, and unable true touch influences the technical problem of learning effect.
The utility model provides a technical scheme that its technical problem adopted is:
the utility model provides an aircraft control display module simulator, includes the casing, install button subassembly on the casing, be provided with power module and control assembly in the casing, button subassembly includes the key circuit board, control assembly includes control panel and display screen, be provided with microprocessor on the control panel, key circuit board and microprocessor's input electric connection, microprocessor's output and display screen electric connection, microprocessor still is used for communicating with data terminal.
Further, the button subassembly still includes shell, keyboard, button leaded light module, button circuit board and the button circuit board gusset plate that sets gradually from top to bottom.
Furthermore, the keys on the keyboard are composite keys of acrylic glue and silica gel.
Further, the control assembly comprises a frame, the display screen is installed on a square groove of the frame, and the control panel is installed below the frame.
Further, still be provided with step-down module on the control panel, power module is used for supplying power for the control panel, step-down module on the control panel steps down the voltage that power module provided to supply power for display screen and button leaded light module.
Further, the lower left corner region of display screen is the draft line, be provided with on the keyboard and select button, function button, letter and swift button, number button and prompt information pilot lamp on the line, the line is selected the button and is set up the both sides at the display screen respectively including controlling each 6 buttons, the function button includes the button of 14 different functions, sets up the left downside at the display screen, letter and swift button set up the right downside at the display screen, the number button sets up the downside at the function button, letter and swift button, number button are used for the input character, prompt information pilot lamp sets up the downside at the line selection button respectively including controlling each two pilot lamps.
Furthermore, a brightness indicator lamp and a brightness adjusting knob are arranged on the lower right side of the display screen and on the upper sides of the letters and the shortcut keys, the brightness adjusting knob is used for adjusting the brightness of the display screen and the key light guide module, and the brightness indicator lamp is used for indicating the brightness.
Furthermore, an execution indicator light and an execution key are arranged on the lower right side of the display screen and on the upper sides of the letters and the shortcut keys, the execution key is pressed to enable the modified data to take effect and turn off the execution indicator light, and the execution indicator light is turned on and used for indicating that the data is modified but not executed.
Furthermore, handles are arranged on two sides of the keyboard respectively.
Further, the display screen adopts a full-color LCD display screen.
The utility model has the advantages that: the utility model relates to a rationally, the cost is lower and the durability is strong, be convenient for maintain, the fidelity is high, the simulation effect is showing, good experience effect has, make control display module simulator easy to maintain through key circuit board and control panel, installation convenient to use, occupation space is little, each module or whole dismouting mode all are unanimous with the control display module of true aircraft on this control display module simulator, provide a more true control display module study operational environment for the flight student.
Drawings
The embodiments of the present invention will be further described with reference to the accompanying drawings:
fig. 1 is an exploded view of a preferred embodiment of the present invention;
fig. 2 is an exploded view of the key assembly of the preferred embodiment of the present invention;
fig. 3 is an exploded view of the control assembly of the preferred embodiment of the present invention;
FIG. 4 is a block diagram of the working principle of the preferred embodiment of the present invention;
fig. 5 is a schematic plan view of a keyboard according to a preferred embodiment of the present invention.
Detailed Description
In order to make the technical solution of the present invention better understood, the technical solution of the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings, and obviously, the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
Referring to fig. 1-4, the simulator for aircraft control display module of the present embodiment includes a housing 300, a key assembly 100 is installed on the housing 300, a power module and a control assembly 200 are installed in the housing 300, the key assembly 100 includes a key circuit board 140, the control assembly 200 includes a control board 220 and a display screen 210, a microprocessor is installed on the control board, the key circuit board 140 is electrically connected to an input end of the microprocessor, an output end of the microprocessor is electrically connected to the display screen 210, the microprocessor on the control board 220 receives input data of the key circuit board 140 and drives the display screen 210 to display, the microprocessor is connected to a data terminal through a USB2.0 interface, the communication can be carried out through software such as PMDG, iFly, ProSim, Project Magenta and the like, so that the real-time updating of data is ensured, and the real feedback simulates the display effect of the control display component in flight.
The key assembly 100 further includes a housing 110, a keyboard 120, a key light guide module 130, a key circuit board 140, and a key circuit board stress board 150, which are sequentially disposed from top to bottom. Wherein the outer shell 110 has an all aluminum alloy panel structure, and a stainless steel back shell, which has higher strength and durability than the plastic panel structure that is mainstream in the market. The keys on the keyboard 120 adopt composite keys of acrylic glue and silica gel, are close to the design of real aeronautical materials, and have real hand feeling consistent with that of the aeronautical materials; the transparent key light guide module 130 can transmit the backlight from the key circuit board 140 to the surface of the keyboard 120, so as to achieve the backlight keyboard effect with adjustable luminance as in an airplane. The key circuit board 140 is a circuit board designed independently, and is reasonable in design, an array mode is adopted, input and output interfaces are saved, and filtering processing is added, so that stability and accuracy of input are greatly improved. The utility model discloses still innovatively design the key circuit board gusset plate 150 at rear portion, can stabilize anterior button leaded light module 130 and key circuit board 140 on shell 110 for whole key assembly 100 is firm firmly, and the reliability strengthens.
The control assembly 200 includes a frame 230, a display screen 210 mounted on a square slot of the frame 230, and a control board 220 mounted under the frame 230. The frame 230 is made of aluminum alloy, so that the display screen 210 and the control panel 220 can be firmly fixed on the frame 230, and the reliability is high. The display screen 210 is a full-color LCD display screen. The LCD has 65K color, 32-level brightness adjustment, a colorful screen as high as 200nit, higher resolution, different from nixie tube display on the market, can display more and more accurate symbols, has the same color as that of a real airplane, has multi-level brightness adjustment as the keyboard 120, adopts an SPI high-speed interface, can well complete the display of various characters and the like, and has high page refreshing response speed and no pause feeling.
The control board 220 is further provided with a voltage reduction module, the power supply module provides a 5V 8A direct current power supply for the control board 220, and the voltage reduction module reduces the 5V voltage to 3.3V and supplies power to the display screen 210 and the key light guide module 130.
Referring to FIG. 5, a display screen 210 is used to display the flight management system data page, and a draft line 1 is located in the bottom left corner area of the display screen 210 for displaying draft information input to the control display assembly. The keyboard 120 is provided with a row selection key 2, a function key 3, a letter and shortcut key 8, a number key 9 and a prompt information indicator light 10:
the row selection key 2 comprises a left key and a right key which are respectively 6, the keys are respectively arranged on two sides of the display screen 210, and the following functions can be achieved by pressing the row selection key 2: 1. data is moved from draft line 1 to the selected line; 2. data is moved from the selected row to draft row 1; 3. selecting a proper page, program or performance mode; 4. When draft line 1 displays DELETE, DELETE data of the selected line;
the function keys 3 include 14 keys of different functions, are provided on the lower left side of the display screen 210, and include:
1. starting reference (initref): displaying a data start page or a reference data page;
2. fairway (RTE): displaying an airway page to enter or modify a departure airport, a destination airport, or an airway;
3. climb (CLB): displaying a climb page to view or change climb data;
4. cruise (CRZ): displaying a cruise page to view or change cruise data;
5. descent (DES): displaying a drop page to view or change drop data;
6. MENU (MENU): a subsystem displaying a menu page to select a CDU (control display unit) control;
7. LEG (LEG): displaying the leg page to: a. evaluating or modifying the horizontal and vertical data, b, controlling the plan mode display;
8. departure/approach (DEP ARR): displaying an departure/approach page to input or change departure and approach procedures;
9. wait (HOLD): displaying a waiting page to establish a waiting pattern and displaying waiting pattern data;
10. process (PROG): displaying a progress page to view dynamic flight and navigation data, including waypoint and destination airport estimated arrival times, remaining fuel amounts, and estimated approach conditions;
11. n1 LIMIT (N1 LIMIT): displaying an N1 limit page to view or change the N1 thrust limit;
12. anchor point (FIX): displaying a positioning point page to establish a reference point on a map display;
13. upper PAGE (PREV PAGE): displaying a previous page (such as a flight page) of the related page;
14. lower PAGE (NEXT PAGE): displaying a next page of the related page;
letter and shortcut key 8 set up the right downside at display screen 210, and number button 9 sets up the downside at function key 3, and letter button, number button 9 are used for the character of input selection at draft line 1, and the shortcut key includes: a slash (/) key to enter a "/" symbol on draft line 1; plus-minus (+/-) keys, the first press will enter a "-" sign on draft line 1, followed by each press alternately showing "+" and "-" signs; DELETE (DEL) key, entering DELETE (DELETE) at draft line 1; a Clear (CLR) key to clear the last character of the draft line 1 or clear the draft line information, pressing and holding data that will clear all draft lines 1; a Space (SP) key for inputting a space on draft line 1;
the prompt information indicator light 10 includes two left and right indicator lights, which are respectively arranged at the lower side of the row selection key 2, and includes: an information (MSG) light that is white when lit and indicates that the draft line has information displayed; an Offset (OFST) lamp which is white when lighted, and indicates that horizontal navigation provides guidance for horizontal route offset; a Failure (FAIL) light that is amber only illuminated during testing and not illuminated when the flight management computer is failed; a CALL (CALL) light, which is white when illuminated, indicates that a subsystem other than the FMC (flight management computer) requests control of the display components.
The lower right side of the display screen 210 and the upper side of the letter and shortcut key 8 are provided with a brightness indicator lamp 4 and a brightness adjusting knob 5, the brightness adjusting knob 5 is used for adjusting the brightness of the display screen 210 and the key light guide module 130, and the brightness indicator lamp 4 is used for indicating the brightness.
And an execution indicator lamp 6 and an execution key 7 are arranged on the lower right side of the display screen 210 and on the upper side of the letter and shortcut key 8, and after the execution key 7 is pressed, the execution indicator lamp 6 is turned off to enable the modified data to be effective, and the execution indicator lamp 6 is turned on to indicate that the data is modified but not executed.
The utility model discloses a key subassembly 100 and control assembly 200 separately design make control display module simulator have very high expansibility, not only can realize on P3D or FSX with the data butt joint of PMDG, iFly, ProSim, Project Magenta etc. also can carry out higher-end expansibility development to control display module according to the customer's demand simultaneously.
In summary, the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those skilled in the art; the technical solutions described in the foregoing embodiments can be modified or equivalent replaced without losing the technical features, and such modifications or replacements do not depart from the spirit and scope of the technical solutions of the embodiments of the present invention.
Claims (10)
1. An aircraft control display assembly simulator, characterized by: the button switch comprises a housing, install the button subassembly on the casing, be provided with power module and control assembly in the casing, the button subassembly includes key circuit board, control assembly includes control panel and display screen, be provided with microprocessor on the control panel, key circuit board and microprocessor's input electric connection, microprocessor's output and display screen electric connection, microprocessor still is used for communicating with data terminal.
2. The aircraft control display assembly simulator of claim 1, wherein: the key assembly further comprises a shell, a keyboard, a key light guide module, a key circuit board and a key circuit board stressing board which are sequentially arranged from top to bottom.
3. An aircraft control display assembly simulator according to claim 2, in which: the keys on the keyboard are composite keys of acrylic glue and silica gel.
4. The aircraft control display assembly simulator of claim 1, wherein: the control assembly comprises a frame, the display screen is installed on a square groove of the frame, and the control panel is installed below the frame.
5. The aircraft control display assembly simulator of claim 1, wherein: the control panel is also provided with a voltage reduction module, the power module is used for supplying power to the control panel, the voltage reduction module on the control panel reduces the voltage provided by the power module and supplies power to the display screen and the key light guide module.
6. An aircraft control display assembly simulator according to claim 2, in which: the lower left corner region of display screen is the draft line, be provided with on the keyboard and select button, function button, letter and swift button, number button and prompt information pilot lamp in the line, the line is selected the button and is set up the both sides at the display screen respectively including controlling each 6 buttons, the function button includes the button of 14 different functions, sets up the left downside at the display screen, letter and swift button set up the right downside at the display screen, the number button sets up the downside at the function button, letter and swift button, number button are used for the input character, prompt information pilot lamp sets up the downside at the line selection button respectively including controlling each two pilot lamps.
7. An aircraft control display assembly simulator according to claim 6, in which: the display screen is characterized in that a brightness indicator lamp and a brightness adjusting knob are arranged on the lower right side of the display screen and on the upper sides of the letters and the shortcut keys, the brightness adjusting knob is used for adjusting the brightness of the display screen and the key light guide module, and the brightness indicator lamp is used for indicating the brightness.
8. An aircraft control display assembly simulator according to claim 6, in which: and an execution indicator light and an execution key are arranged on the lower right side of the display screen and on the upper sides of the letters and the shortcut keys, after the execution key is pressed, the execution indicator light is used for realizing that the modified data takes effect and turning off the execution indicator light, and the execution indicator light is turned on and used for indicating that the data is modified but not executed.
9. An aircraft control display assembly simulator according to claim 6, in which: handles are arranged on two sides of the keyboard respectively.
10. The aircraft control display assembly simulator of claim 1, wherein: the display screen adopts a full-color LCD display screen.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921329892.4U CN210777306U (en) | 2019-08-16 | 2019-08-16 | Simulator for aircraft control display assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921329892.4U CN210777306U (en) | 2019-08-16 | 2019-08-16 | Simulator for aircraft control display assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210777306U true CN210777306U (en) | 2020-06-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921329892.4U Active CN210777306U (en) | 2019-08-16 | 2019-08-16 | Simulator for aircraft control display assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210777306U (en) |
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2019
- 2019-08-16 CN CN201921329892.4U patent/CN210777306U/en active Active
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