CN212484650U - Panel of airplane simulator - Google Patents
Panel of airplane simulator Download PDFInfo
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- CN212484650U CN212484650U CN202020760189.5U CN202020760189U CN212484650U CN 212484650 U CN212484650 U CN 212484650U CN 202020760189 U CN202020760189 U CN 202020760189U CN 212484650 U CN212484650 U CN 212484650U
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- control circuit
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- 239000002356 single layer Substances 0.000 claims description 3
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- 230000006978 adaptation Effects 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000009434 installation Methods 0.000 abstract description 2
- 238000012549 training Methods 0.000 description 8
- 238000004891 communication Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000006870 function Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
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- 238000001514 detection method Methods 0.000 description 1
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- 230000010354 integration Effects 0.000 description 1
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Abstract
The utility model discloses a panel about aircraft simulator relates to small-size aircraft simulator technical field. The panel shell is fixedly installed with the control circuit board and the panel lining plate; the ipad is installed between the control circuit board and the panel lining plate, a position adjusting block for adjusting the position of an ipad graphic is installed on the ipad, and the position adjusting block is connected with the control circuit board through a data line. The utility model discloses a technical scheme that embodiment provided can include following beneficial effect: the utility model discloses a simulation degree is high, adopts the method the same with real aircraft, and the operation is felt also truer. The practicality is high, and the installation degree of difficulty is little, and all can perfect adaptation with the instrument panel of general ser simulator. The structure is simpler, the cost is lower, and the device is very suitable for mass production.
Description
Technical Field
The utility model discloses a small-size aircraft simulator technical field especially relates to an aircraft simulator's panel.
Background
The flight training simulator is a device for training pilots, and generally comprises a cockpit, interface equipment, various instruments, a vision system and a training computer. The computer is the control center of the flight training simulator. When trainees train, the trainees can perform various operations while sitting in the cockpit: the electric door is opened, the accelerator is pushed and pulled, the flight lever and the rudder are operated, and various data such as flight speed, travel, position, height, wind direction, wind speed and the like can be obtained. The sight system can simulate the scenery where the student is located, the student feels the motions of diving, pitching and circling just like sitting in the airplane during operation, can see various scenery (cloud, fog, river and building) on and off the airplane, and can set various flight environments so as to comprehensively exercise the technology and learn and master various operations with high difficulty and danger. Therefore, as long as the simulation conditions are vivid, the trainees who pass the flight simulation training can fly the airplane to lift off for exercise immediately after the graduation.
In the simulated flight device or system, the operating component is the most important component, and all the simulated flight operations are completed through the operating component. Large aircraft such as Boeing 737, A320 and other aircraft types are very complicated to operate due to a large number of operating parts, and cannot be used as a learning object for common people to know flight; the simulation target most suitable for common people to learn simulated flight is a small aircraft for navigation, such as a small aircraft of the Seina series.
The Garmin1000 system (G1000 system for short) is a set of highly integrated general avionics systems produced by the United states of America Garmin corporation. The G1000 system integrates avionics equipment such as communication, navigation GPS and the like. The g1000 system has made a major breakthrough in functionality and practicability by being equipped with a large screen and a high-resolution display and combining with research results in the aspects of airplane operation, air data and Ethernet connection. G1000 system functions include providing attitude atmospheric data engine and body dynamics data and moving map displays from GPS, environmental references, terrain and obstacle warnings. Additionally the g1000 system includes complete very high frequency communication, omni-directional beacons, instrument landing system and transponder (VOR/ILS) functionality, and the system and user interface allows selection and control of system functions only through knobs and buttons on the flight main display (PFD) multi-function display (MFD) digital audio pad.
The united states defines an aircraft equipped with the g1000 system as an advanced aircraft and is heavily equipped. In China, airplanes equipped with g1000 equipment are also introduced in large quantities in recent years to be used as training machines. Because the g1000 device has high integration level and small volume for operation and control, the existing g1000 simulator has large volume and heavy weight, can not be well assembled and combined with an aircraft simulation cockpit, and has incomplete functions.
The significance of solving the technical problems is as follows: with the rapid development of aviation industry, particularly navigation, the training requirement of small airplanes is increasing day by day, each part of the simulator needs to be simulated 1:1 with a real airplane, so that an operator can experience the real airplane, and the training effect can be achieved.
SUMMERY OF THE UTILITY MODEL
To overcome the problems in the related art, the disclosed embodiments provide panels for aircraft simulators. The technical scheme is as follows:
the panel of the airplane simulator comprises a panel shell, wherein the panel shell is fixedly installed with a control circuit board and a panel lining plate;
the ipad is installed between the control circuit board and the panel lining plate, a position adjusting block for adjusting the position of the ipad is installed on the ipad, and the position adjusting block is connected with the control circuit board through a data line.
In one embodiment, buttons and knobs are mounted intermediate the control circuit board and the panel housing.
In one embodiment, a rear cover is snap-fit mounted on the panel housing.
In one embodiment, the ipad is connected to a display terminal for flight real-time data of the simulated flight app.
In one embodiment, a microcontroller is installed inside the control circuit board, and the microcontroller is connected with the single-layer rotary coding switches, the double-layer rotary coding switches and the multifunctional switch.
The utility model discloses a technical scheme that embodiment provided can include following beneficial effect: the utility model discloses a simulation degree is high, adopts the method the same with real aircraft, and the operation is felt also truer. The practicality is high, and the installation degree of difficulty is little, and all can perfect adaptation with the instrument panel of general ser simulator. The structure is simpler, the cost is lower, and the device is very suitable for mass production.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the disclosure.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the present disclosure and together with the description, serve to explain the principles of the disclosure.
Fig. 1 is an internal structural view of a panel of an aircraft simulator according to the present invention;
fig. 2 is a front view of a panel of an aircraft simulator in accordance with the present invention;
fig. 3 is a schematic circuit diagram of the main controller of the present invention;
fig. 4 is a power supply circuit diagram of the main controller of the present invention;
fig. 5 is a wiring terminal subgraph of the bluetooth module of the utility model;
fig. 6 is the utility model discloses main control unit and bluetooth intelligent object's connection schematic diagram.
Reference numerals:
1. panel shell 2, ipad 3 and button
4. Knob 5, control circuit board 6, back lid
7. Data line 8, panel lining board 9 and position adjusting block
Detailed Description
Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, like numbers in different drawings represent the same or similar elements unless otherwise indicated. The implementations described in the exemplary embodiments below are not intended to represent all implementations consistent with the present disclosure. Rather, they are merely examples of apparatus and methods consistent with certain aspects of the present disclosure, as detailed in the appended claims.
The panel of the aircraft simulator comprises: the panel shell 1, the control circuit board 5 and the panel lining board 8 are connected together through screws, the buttons 3 and the knobs 4 are placed at corresponding positions between the control circuit board 5 and the panel shell 1, the iPad graphic representations 2 are placed between the control circuit board 5 and the panel lining board 8, the positions of the iPad graphic representations 2 with different sizes are adjusted through the position adjusting blocks 9, and data connection with the control circuit board 5 is achieved through the data lines 7. Finally, a rear cover 6 is covered, and the whole is connected with the whole simulator by screws.
The method is characterized in that flight real-time data of a main display (PFD) or a multifunctional display (MFD) is simulated by utilizing simulated flight apps in the iPad, when an operator needs to operate, because display output is mainly carried out through the iPad illustration 2, the screen of the iPad illustration 2 is lightened firstly, at the moment, two keys (NOSEUP) (NOSEDN) in the shell 1 are pressed simultaneously, at the moment, the charging of the iPad illustration 2 is cut off, the screen is lightened automatically, at the moment, the relevant simulated flight apps are selected through touch, and then the circuit board 5 is controlled through the control button 3 and the knob 4, so that the adjusted data are reflected in the app program of the iPad through the relevant program and the data line 7 which are compiled in advance to be changed correspondingly. The purpose of simulating flight data is achieved. In addition, the usb port connected to the rear part provides power for the whole g1000 panel, and the usb port can charge the iPad in the g1000 panel and transmit related data (such as operation of upgrading the iPad).
A hardware circuit part of the product adopts a Texas Instruments MSP430F5438A microcontroller, as shown in FIG. 3, U1 is a main controller, is provided with 3 single-layer rotary coding switches, 5 double-layer coding switches and 1 multifunctional switch, and connects a detection state signal pin of the switch to a GPIO (general purpose input/output) of the main controller. The host controller is burned to read and process the GPIO data, and performs data communication with the Bluetooth intelligent module BLE1113 through UART communication as shown in figure 6. The Bluetooth intelligent module BLE113 performs data interaction with an IPAD provided with a "Simionic G1000" app designed by the company of China through a Bluetooth technology so as to realize the simulated experience of the G1000 panel of the Small-sized Sassner aircraft simulator.
Other embodiments of the disclosure will be apparent to those skilled in the art from consideration of the specification and practice of the disclosure disclosed herein. This application is intended to cover any variations, uses, or adaptations of the disclosure following, in general, the principles of the disclosure and including such departures from the present disclosure as come within known or customary practice within the art to which the disclosure pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the disclosure being indicated by the following claims.
It will be understood that the present disclosure is not limited to the precise arrangements described above and shown in the drawings and that various modifications and changes may be made without departing from the scope thereof. The scope of the present disclosure should be limited only by the attached claims.
Claims (5)
1. A panel of an aircraft simulator comprises a panel shell and is characterized in that the panel shell is fixedly installed with a control circuit board and a panel lining board;
the ipad is installed between the control circuit board and the panel lining plate, a position adjusting block for adjusting the position of the ipad is installed on the ipad, and the position adjusting block is connected with the control circuit board through a data line.
2. An aircraft simulator faceplate according to claim 1, wherein buttons and knobs are mounted intermediate said control circuit board and faceplate housing.
3. An aircraft simulator panel as claimed in claim 1 wherein a rear cover is snap fitted to the panel housing.
4. An aircraft simulator faceplate as defined in claim 1, wherein the ipad is connected to a display terminal for flight real-time data to the simulated flight app.
5. An aircraft simulator panel as claimed in claim 1 wherein a microcontroller is mounted within the control circuit board, the microcontroller being connected to the plurality of single layer rotary encoder switches, the plurality of double layer encoder switches and the multifunction switch.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202020760189.5U CN212484650U (en) | 2020-05-11 | 2020-05-11 | Panel of airplane simulator |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202020760189.5U CN212484650U (en) | 2020-05-11 | 2020-05-11 | Panel of airplane simulator |
Publications (1)
Publication Number | Publication Date |
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CN212484650U true CN212484650U (en) | 2021-02-05 |
Family
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Family Applications (1)
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CN202020760189.5U Active CN212484650U (en) | 2020-05-11 | 2020-05-11 | Panel of airplane simulator |
Country Status (1)
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CN (1) | CN212484650U (en) |
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2020
- 2020-05-11 CN CN202020760189.5U patent/CN212484650U/en active Active
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Address after: 3013, South 2nd Floor, No. 18 Haitai West Road, Huayuan Industrial Zone, Binhai New Area, Tianjin, 300000 Patentee after: TIANJIN SHIMIAO TECHNOLOGY Co.,Ltd. Address before: 2 / F, South, 18 Haitai West Road, Huayuan Industrial Park, Binhai New Area, Tianjin 300450 Patentee before: TIANJIN SHIMIAO TECHNOLOGY Co.,Ltd. |
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