CN204595489U - Based on the navigation airborne power supply human-computer exchange device of CAN - Google Patents
Based on the navigation airborne power supply human-computer exchange device of CAN Download PDFInfo
- Publication number
- CN204595489U CN204595489U CN201520267913.XU CN201520267913U CN204595489U CN 204595489 U CN204595489 U CN 204595489U CN 201520267913 U CN201520267913 U CN 201520267913U CN 204595489 U CN204595489 U CN 204595489U
- Authority
- CN
- China
- Prior art keywords
- power supply
- module
- transceiver
- touch screen
- control chip
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Power Sources (AREA)
Abstract
Based on the navigation airborne power supply human-computer exchange device of CAN, its structure is: on control chip, be connected with LCD Touch Screen, EEPROM module, power supply monitoring module and CAN transceiver, the other end of CAN transceiver is connected with aircraft controller, charger and BMS power-supply management system, and power module is control chip, LCD Touch Screen, EEPROM module, power supply monitoring module and CAN transceiver are powered.The utility model achieves the exchange of man-machine information bidirectional by arranging LCD Touch Screen, CAN transceiver by the information transmission that receives to control chip, thus be presented on LCD Touch Screen, solve in prior art to be connected with computer and just can look into battery information and the technical matters using very complicated caused.The utility model, while reaching navigation power detecting standard, can realize the exchange of people's machine information, easy to use.
Description
Technical field
The utility model relates to a kind of human-computer exchange device, especially a kind of navigation airborne power supply human-computer exchange device based on CAN.
Background technology
General Aviation refers to that the Civil Aviation Activities beyond public air transport is engaged in by use civil aircraft, due to specific application, to the management of the more civilian power supply of technical requirement of power management and detection with detect stricter, so existing common power system be not suitable for navigation equipment.The equipment can checking battery information fast that existing navigation battery management system is not supporting with it, even if can be connected with computer, it is also cumbersome for using, and directly can not realize the exchange of people's machine information fast.
Summary of the invention
In order to solve the problems of the technologies described above, the utility model provides a kind of navigation airborne power supply human-computer exchange device based on CAN, the exchange of man-machine information bidirectional is achieved by arranging LCD Touch Screen, CAN transceiver is set by the information transmission that receives to control chip, thus be presented on LCD Touch Screen, solve in prior art to be connected with computer and just can look into battery information and the technical matters using very complicated caused.
To achieve these goals, the technical solution used in the present invention is the navigation airborne power supply human-computer exchange device based on CAN, it is characterized in that: on control chip, be connected with LCD Touch Screen, EEPROM module, power supply monitoring module and CAN transceiver, the other end of CAN transceiver is connected with aircraft controller, charger and BMS power-supply management system, and power module is control chip, LCD Touch Screen, EEPROM module, power supply monitoring module and CAN transceiver are powered.
Described power module is the DC-DC module that 18V-36V input turns 5V and 9V output.
Described CAN transceiver is isolated CAN transceiver.
Described LCD Touch Screen is OCM800600T104-2C touching display screen, carries out the transmitted in both directions of information data with control chip (5).
The A/D module ADS1115 of described power supply monitoring module to be model be delta-sigma type, is used for monitoring the supply voltage of the voltage of input power, electric current and chip.
The beneficial effects of the utility model are: the utility model provides a kind of navigation airborne power supply human-computer exchange device based on CAN, the exchange of man-machine information bidirectional is achieved by arranging LCD Touch Screen, CAN transceiver is set by the information transmission that receives to control chip, thus be presented on LCD Touch Screen, solve in prior art to be connected with computer and just can look into battery information and the technical matters using very complicated caused.The utility model, can the exchange of time people machine information while can reaching navigation power detecting standard, easy to use.
Accompanying drawing explanation
Fig. 1: be hardware frame figure of the present utility model.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in detail.
The navigation airborne power supply human-computer exchange device based on CAN as shown in Figure 1, it is characterized in that: on control chip 5, be connected with LCD Touch Screen 3, EEPROM module 7, power supply monitoring module 4 and CAN transceiver 6, the other end of CAN transceiver 6 is connected with aircraft controller 9, charger 10 and BMS power-supply management system 11, and power module 8 is powered for control chip 5, LCD Touch Screen 3, EEPROM module 7, power supply monitoring module 4 and CAN transceiver 6.
Described control chip 5 model is C8051F580, as the main control chip of man-machine interface, the information needing process CAN transceiver 6 to receive also sends information to LCD Touch Screen 3, simultaneously temporally interval by data stored in EEPROM module 7, also to control the power supply state of power supply monitoring module 4 monitoring equipment.
The OCM800600T104-2C touching display screen that described LCD Touch Screen 3 is 8 inches, resolution is 600 × 800, carry out the transmitted in both directions of information data with control chip 5.Not only LCD Touch Screen 3 is as show media but also as import pathway, can control by control chip 5 relevant position data being shown to screen during display, during input, user selects different display pages by touch-control, touch information is returned to control chip 5 by screen, and control chip 5 determines the content that will show according to the information returned.
Described EEPROM module 7 model is M95512.EEPROM module is used for storing the information received from CAN transceiver 6, also as power supply status registering instrument during flight, can do flying quality analysis after facilitating flight to terminate.
Described power supply monitoring module 4 model is the A/D module of ADS1115, be used for monitoring the supply voltage of the voltage of input power, electric current and chip, data are given to control chip 5, control chip 5 can judge after obtaining these values whether the power supply state of each module of man-machine interface and inside has exception, when finding that there is exception on screen display alarm information.
Described CAN transceiver 6 is isolated CAN transceiver, and model is ISO1050.
The DC-DC module that described power module 8 turns 5V and 9V export for 18V-36V inputs.
Described aircraft controller 9, charger 10 and BMS power-supply management system 11 is input equipment of the present utility model.
In use, in control chip 5, be integrated with the bus interface such as CAN, UART, SPI, IIC, can 24MHz be operated in.Mainboard is provided with the power supply monitoring module 4 of CAN transceiver 6, the 512Kbit EEPROM module 7 of SPI interface, the delta-sigma type of IIC interface.Control chip 5 by CAN transceiver 6 receive CAN send come up information, EEPROM module 7 is as storage medium, control chip 5 temporally can be stored into so that data analysis in EEPROM module 7 in interval by data, and power supply monitoring module 4 is measured the input voltage of master control borad, the voltage of electric current and chip power supply, LCD Touch Screen 3 and to be connected with master control borad by UART mouth and controlled.The human-computer exchange device that the utility model adopts and BMS power-supply management system 11 with the use of, aircraft controller 9 and charger 10 can also be accessed.The quick, convenient of BMS power-supply management system 11 information can be realized when human-computer exchange device is connected with BMS power-supply management system 11 check; When connecting BMS power-supply management system 11 with aircraft controller 9, can be used as power supply status registering instrument during flight, during record-setting flight, voltage, electric current, the power equivalent of power supply, facilitate post-flight debriefing data simultaneously; When connecting BMS power-supply management system 11 with charger 10 simultaneously; can be used as monitor; monitor the charged state of battery, comprising: the information such as charging voltage, charging current, residual capacity, battery temperature, guard mode, can the charging unusual condition of Timeliness coverage battery.
Claims (5)
1. based on the navigation airborne power supply human-computer exchange device of CAN, it is characterized in that: on control chip (5), be connected with LCD Touch Screen (3), EEPROM module (7), power supply monitoring module (4) and CAN transceiver (6), the other end of CAN transceiver (6) is connected with aircraft controller (9), charger (10) and BMS power-supply management system (11), and power module (8) is control chip (5), the power supply of LCD Touch Screen (3), EEPROM module (7), power supply monitoring module (4) and CAN transceiver (6).
2. the navigation airborne power supply human-computer exchange device based on CAN according to claim 1, is characterized in that: the DC-DC module that described power module (8) turns 5V and 9V export for 18V-36V inputs.
3. the navigation airborne power supply human-computer exchange device based on CAN according to claim 1, is characterized in that: described CAN transceiver (6) is isolated CAN transceiver.
4. the navigation airborne power supply human-computer exchange device based on CAN according to claim 1, it is characterized in that: described LCD Touch Screen (3) is OCM800600T104-2C touching display screen, carries out the transmitted in both directions of information data with control chip (5).
5. the navigation airborne power supply human-computer exchange device based on CAN according to claim 1, it is characterized in that: described power supply monitoring module (4) is the A/D module ADS1115 of delta-sigma type for model, be used for monitoring the supply voltage of the voltage of input power, electric current and chip.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520267913.XU CN204595489U (en) | 2015-04-29 | 2015-04-29 | Based on the navigation airborne power supply human-computer exchange device of CAN |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520267913.XU CN204595489U (en) | 2015-04-29 | 2015-04-29 | Based on the navigation airborne power supply human-computer exchange device of CAN |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204595489U true CN204595489U (en) | 2015-08-26 |
Family
ID=53931625
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520267913.XU Active CN204595489U (en) | 2015-04-29 | 2015-04-29 | Based on the navigation airborne power supply human-computer exchange device of CAN |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204595489U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112199321A (en) * | 2020-09-28 | 2021-01-08 | 中国航空工业集团公司雷华电子技术研究所 | Method for processing power failure data by using XRAM and FLASH in single chip microcomputer |
-
2015
- 2015-04-29 CN CN201520267913.XU patent/CN204595489U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112199321A (en) * | 2020-09-28 | 2021-01-08 | 中国航空工业集团公司雷华电子技术研究所 | Method for processing power failure data by using XRAM and FLASH in single chip microcomputer |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202837403U (en) | Portable tester for mud resistivity | |
| CN112256501A (en) | Expansion equipment interface detection circuit, interface expansion device and expansion dock | |
| CN106842152A (en) | Airborne fire control radar online system failure diagnosis | |
| CN206573706U (en) | The detection means of integral battery management system | |
| CN102738903A (en) | Alternating current-direct current integrated power monitoring device used for station | |
| CN204750596U (en) | Aircraft in situ test equipment | |
| CN204595489U (en) | Based on the navigation airborne power supply human-computer exchange device of CAN | |
| CN105501455B (en) | A kind of unmanned aerial vehicle comprehensive power integrated system and method | |
| CN205864448U (en) | A kind of hand-held CAN analyser of electric automobile | |
| CN203481895U (en) | Power calculation and display system for portable power source, and portable power source thereof | |
| CN202057736U (en) | Handheld power load control equipment fault detector | |
| CN211148867U (en) | Battery pack diagnostic device for electric vehicle | |
| CN204203438U (en) | Storage battery discharge tester | |
| CN203350383U (en) | Handheld debugging instrument of BMS (Battery Management System) | |
| CN207457823U (en) | A kind of fly-by-wire flight control system detection device | |
| CN201035357Y (en) | Feeder line distant place terminal | |
| CN203070094U (en) | A CAN communication test calibrating device of an electric vehicle charging interface | |
| CN206020574U (en) | A kind of automobile power cell Beam Detector | |
| CN204964713U (en) | Portable multi -functional battery test system of holding | |
| CN200986437Y (en) | Digitalized experiment system | |
| CN204043705U (en) | A kind of portable warm Humidity Detection equipment | |
| CN201311472Y (en) | Monitoring apparatus vehicle-carrying cable insulation detecting system | |
| CN105866538A (en) | Electric quantity measuring instrument for electric power system | |
| CN106323376A (en) | Coal mine fire monitoring device | |
| CN202735432U (en) | electric meter device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150930 Address after: 110000 No. 28-9 Guanyin Road, Huanggu District, Liaoning, Shenyang Patentee after: Shenyang Jun Weixinneng Science and Technology Ltd. Address before: 110000, Guanyin Road, Guanyin Private Development Zone, East Street, Huanggu District, Liaoning, Shenyang, 28-9 Patentee before: Liaoning is precious along golden a word used in place name science and technology limited Company |