CN203812422U - Simulated training system for airplane communication equipment - Google Patents
Simulated training system for airplane communication equipment Download PDFInfo
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- CN203812422U CN203812422U CN201420115598.4U CN201420115598U CN203812422U CN 203812422 U CN203812422 U CN 203812422U CN 201420115598 U CN201420115598 U CN 201420115598U CN 203812422 U CN203812422 U CN 203812422U
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Abstract
The utility model relates to a simulated training platform for airplane communication equipment. The simulated training system for the airplane communication equipment is mainly composed of a microcomputer system, an adaptive circuit, a radio comprehensive tester and a power system; the microcomputer system is integrated with a controller, a digital I/O module, an analog quantity output module, a matrix switch, a multiplexer, a power switch and a GPIB communication card by utilization of a data bus module on the platform of an industrial control computer; the radio comprehensive tester is connected with the industrial control computer through a GPIB bus; the power system provides working power for the microcomputer system and the radio comprehensive tester; and the microcomputer system is connected with communication equipment through the port adaptive circuit and an interface circuit. The simulated training platform for the airplane communication equipment is simple in structure and scientific and reasonable in design, can assist simulated training of the airplane communication equipment, and has the advantages of low investment cost and good training effect.
Description
Technical field
The utility model relates to a kind of aircraft communication equipment simulating training platform, specifically, has related to a kind of aircraft communication equipment simulating training system.
Background technology
Aircraft communications system plays vital effect for the shipping safety of aircraft.Therefore, the operation to aircraft communication equipment and use are important steps that is related to aircraft shipping safety.Mainly by training to the logical galvanoscopic method of aircraft communication equipment in outfield to the operation training of aircraft communication equipment at present, shortcoming is that training cost is high, and the Aerial Electronic Equipment of fragile aircraft needs multi-specialized personnel to coordinate training, the training degree of depth is inadequate, and effect is unpredictable.
Therefore, if can propose a kind of simulated training system of aircraft communication equipment, can be good at addressing this problem, and can reduce the input of training, strengthen training effect.
Summary of the invention
The purpose of this utility model is for prior art deficiency, and a kind of simple in structure, aircraft communication equipment simulating training system that design science is reasonable, practical is provided.
The technical scheme that the utility model adopts:
A kind of aircraft communication equipment simulating training system, mainly by microsystem, adapter circuit, radio comprehensive measurement instrument and power-supply system composition, described microsystem is taking industrial control computer as platform, utilize data bus module integrated controller, numeral I/O module, analog output module, matrix switch, multiplexer, power switch, GPIB communication card, described radio comprehensive measurement instrument is connected with industrial control computer by gpib bus, power-supply system provides working power for described microsystem and radio comprehensive measurement instrument, described microsystem is connected communication facilities by port adapter circuit with interface circuit.
Described aircraft communication equipment simulating training system, described communication facilities comprises short-wave radio set transceiver, ultrashort wave radio set transceiver, the power added device of ultrashort wave radio set transceiver, U/V chain transceiver and power added device and radio frequency conversion equipment, and the data that described communication apparatus communication interface sends are simulated by the integrated controller of data bus module.
Described aircraft communication equipment simulating training system, data bus is selected the AEC429-CPCI-88(8R8T of Advantech company limited) digital I/O module is selected and is ground magnificent PCI-1718 data collecting card described in the PCI-1553-M 1553B bus module of ARINC429/422/485 module and Chengdu Ying Beite science and technology limited Company: 16 passage 5V/TTL/COMS numeral I/O modules; Described digital I/O module is for simulating the switching value signal of each communication device interface; Analog output module is selected PCI-1718 data collecting card, provides 32 tunnels analogy amount outputs, for simulating the analog output of each communication facilities external interface.
Described aircraft communication equipment simulating training system, described power-supply system comprises gpib bus programme-controlled dc power and AC power, programme-controlled dc power is selected Agilent 6674A, programmable AC power supply is selected JD1792-D100, described power-supply system supervisory circuit comprises battery main switch, voltage detecting circuit, overvoltage pilot lamp, under-voltage pilot lamp, indicating circuit, fan, contactor, I/O driving circuit, electrical relay group on power transfer relay group and internal electric source and GPIB instrument, described programme-controlled dc power and AC power are simultaneously for simulating the power supply output of each communication facilities, radio comprehensive measurement instrument is for simulating radio frequency and the sound signal of each communication facilities output.
The beneficial effects of the utility model:
1, the utility model aircraft communication equipment simulating training system, simple in structure, design science is reasonable, can assist the simulated training of aircraft communication equipment, has input cost low, the advantage that training effect is good.
2,the utility model aircraft communication equipment simulating training system, signal content is abundant, and communication modes is various, powerful, and has power supply supervisory circuit, safe and reliable, has stronger practical value.
Brief description of the drawings
Fig. 1 is the utility model aircraft communication equipment simulating training system composition frame chart.
Fig. 2 is power supply supervisory circuit composition frame chart.
Embodiment
Below by embodiment, the technical solution of the utility model is described in further detail.
Embodiment 1
As shown in Figure 1, the utility model aircraft communication equipment simulating training system, mainly by microsystem, adapter circuit, radio comprehensive measurement instrument and power-supply system composition, described microsystem is taking industrial control computer as platform, utilize data bus module integrated controller, numeral I/O module, analog output module, matrix switch, multiplexer, power switch, GPIB communication card, described radio comprehensive measurement instrument is connected with industrial control computer by gpib bus, power-supply system provides working power for described microsystem and radio comprehensive measurement instrument, described microsystem is connected communication facilities by port adapter circuit with interface circuit.Described communication facilities comprises short-wave radio set transceiver, ultrashort wave radio set transceiver, the power added device of ultrashort wave radio set transceiver, U/V chain transceiver and power added device and radio frequency conversion equipment, and the data that described communication apparatus communication interface sends are simulated by the integrated controller of data bus module.
Described port adapter circuit is the bridge that microsystem is connected with each communication device interface of platform front panel with GPIB resource, complete the level adapted of switching value and put and determine, the functions such as the level comparison of analog quantity, the guiding of signal trend and control, power supply supply, to meet the demand of each communication device interface electrical specification simulation.
Embodiment 2
Referring to Fig. 1, the aircraft communication equipment simulating training system of the present embodiment, as different from Example 1: data bus is selected the AEC429-CPCI-88(8R8T of Advantech company limited) described in the PCI-1553-M 1553B bus module of ARINC429/422/485 module and Chengdu Ying Beite science and technology limited Company, digital I/O module is selected and is ground magnificent PCI-1718 data collecting card: 16 passage 5V/TTL/COMS numeral I/O modules; Described digital I/O module is for simulating the switching value signal of each communication device interface; Analog output module is selected PCI-1718 data collecting card, provides 32 tunnels analogy amount outputs, for simulating the analog output of each communication facilities external interface.
The utility model aircraft communication equipment simulating training system, microsystem, taking industrial computer as platform, taking various boards as simulation resource, utilizes bussing technique to form the control core of simulated training system.
The function of microsystem various piece is as follows:
1, main control computer
Main control computer is selected and is ground magnificent 610H industrial control computer, and keyboard and mouse is selected radio keyboard mouse external member.
2, power switch
For simulating the break-make of each communication facilities power interface power supply, it is mainly made up of high power relay.
3, matrix switch
Matrix switch is to become 64 2 × 16(1 lines by relay configuration) matrix switch module of form, for Dynamic Establishing or cancel message analog channel, realize the switching that inputs or outputs of all low frequency signals.
4, digital I/O module
Select the PCI-1718 data collecting card of Advantech company limited: 16 passage 5V/TTL/COMS numeral I/O modules.Numeral I/O module is for simulating the switching value signal of each communication device interface.
5, normal data bus module
Between communication facilities and controller (or CCU), carry out message exchange by data bus.The data that data bus module sends for simulating each communication apparatus communication interface.Microsystem provides RS-422, RS-232, ARINC429,1553B normal data bus module, selects the AEC429-CPCI-88(8R8T of Advantech company limited) the PCI-1553-M 1553B bus module of ARINC429/422/485 module and Chengdu Ying Beite science and technology limited Company.
6, analog output module
Analog output module is selected PCI-1718 data collecting card, and 32 tunnels analogy amount outputs can be provided, and output voltage range is :-10V～+ 10V.Analog output module is for simulating the analog output of each communication facilities external interface.
7, multiplexer
It is identical that there is the characteristic of a lot of signals each communication facilities external interface the inside, the signal that these are had identical characteristics by multiplexer is optimized and integrates, the signal of identical characteristics only takies a signal imitation resource, can effectively save limited signal imitation resource.
8, GPIB communication card
GPIB communication card communicates for realizing with the surveying instrument with gpib interface function, realizes function control and data transmission to GPIB instrument.
Embodiment 3
Aircraft communication equipment simulating training system described in the present embodiment, is with the difference of embodiment 2: the configuration of GPIB instrument resource Main Resources is as follows: (1) radio comprehensive measurement instrument: select IFR2945B.(2) programme-controlled dc power: select Agilent 6674A.(3) programmable AC power supply: select JD1792-D100.
Gpib bus instrument, for generation, measurement and the control of some distinctive signals, also comprises gpib bus programme-controlled dc power and AC power simultaneously.Radio comprehensive measurement instrument is for simulating radio frequency and the sound signal of each communication facilities output; Program control AC/DC power supply is for simulating the power supply output of each communication facilities, and also feed system self uses simultaneously.
Power supply supervisory circuit shown in Fig. 2 is mainly by alternating current 220V input voltage and electric current are detected, the function such as upper electric control of electric control and GPIB instrument on electric control on completion system, the control of inside/outside electrical source exchange, internal electric source.Its composition frame chart as shown in Figure 2, mainly comprises the part such as electrical relay group on battery main switch, voltage detecting circuit, overvoltage pilot lamp, under-voltage pilot lamp, indicating circuit, fan, contactor, I/O driving circuit, power transfer relay group and internal electric source and GPIB instrument.
Claims (4)
1. an aircraft communication equipment simulating training system, mainly by microsystem, adapter circuit, radio comprehensive measurement instrument and power-supply system composition, it is characterized in that: described microsystem is taking industrial control computer as platform, utilize data bus module integrated controller, numeral I/O module, analog output module, matrix switch, multiplexer, power switch, GPIB communication card, described radio comprehensive measurement instrument is connected with industrial control computer by gpib bus, power-supply system provides working power for described microsystem and radio comprehensive measurement instrument, described microsystem is connected communication facilities by port adapter circuit with interface circuit.
2. aircraft communication equipment simulating training system according to claim 1, it is characterized in that: described communication facilities comprises short-wave radio set transceiver, ultrashort wave radio set transceiver, the power added device of ultrashort wave radio set transceiver, U/V chain transceiver and power added device and radio frequency conversion equipment, the data that described communication apparatus communication interface sends are simulated by the integrated controller of data bus module.
3. aircraft communication equipment simulating training system according to claim 1 and 2, is characterized in that: data bus is selected described in the AEC429-CPCI-88ARINC429/422/485 module of Advantech company limited and the PCI-1553-M 1553B bus module of Chengdu Ying Beite science and technology limited Company digital I/O module to select and ground magnificent PCI-1718 data collecting card: 16 passage 5V/TTL/COMS numeral I/O modules; Described digital I/O module is for simulating the switching value signal of each communication device interface; Analog output module is selected PCI-1718 data collecting card, provides 32 tunnels analogy amount outputs, for simulating the analog output of each communication facilities external interface.
4. aircraft communication equipment simulating training system according to claim 3, it is characterized in that: described power-supply system comprises gpib bus programme-controlled dc power and AC power, programme-controlled dc power is selected Agilent 6674A, programmable AC power supply is selected JD1792-D100, described power-supply system supervisory circuit comprises battery main switch, voltage detecting circuit, overvoltage pilot lamp, under-voltage pilot lamp, indicating circuit, fan, contactor, I/O driving circuit, electrical relay group on power transfer relay group and internal electric source and GPIB instrument, described programme-controlled dc power and AC power are simultaneously for simulating the power supply output of each communication facilities, radio comprehensive measurement instrument is for simulating radio frequency and the sound signal of each communication facilities output.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420115598.4U CN203812422U (en) | 2014-03-14 | 2014-03-14 | Simulated training system for airplane communication equipment |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420115598.4U CN203812422U (en) | 2014-03-14 | 2014-03-14 | Simulated training system for airplane communication equipment |
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| CN203812422U true CN203812422U (en) | 2014-09-03 |
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| CN201420115598.4U Expired - Fee Related CN203812422U (en) | 2014-03-14 | 2014-03-14 | Simulated training system for airplane communication equipment |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106373451A (en) * | 2016-11-15 | 2017-02-01 | 薛雪东 | Missile launching vehicle electronic control simulation training system and method |
| CN109584670A (en) * | 2019-01-28 | 2019-04-05 | 陈喜春 | A kind of communication system for simulation training device |
| CN109733643A (en) * | 2019-02-22 | 2019-05-10 | 中国人民解放军空军工程大学航空机务士官学校 | A kind of aircraft navigation attitude device test system |
| CN112557799A (en) * | 2020-12-12 | 2021-03-26 | 江西洪都航空工业集团有限责任公司 | Comprehensive CNI system testing device |
| CN114077225A (en) * | 2020-08-11 | 2022-02-22 | 北京机械设备研究所 | Universal embedded servo controller |
-
2014
- 2014-03-14 CN CN201420115598.4U patent/CN203812422U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106373451A (en) * | 2016-11-15 | 2017-02-01 | 薛雪东 | Missile launching vehicle electronic control simulation training system and method |
| CN109584670A (en) * | 2019-01-28 | 2019-04-05 | 陈喜春 | A kind of communication system for simulation training device |
| CN109733643A (en) * | 2019-02-22 | 2019-05-10 | 中国人民解放军空军工程大学航空机务士官学校 | A kind of aircraft navigation attitude device test system |
| CN109733643B (en) * | 2019-02-22 | 2024-04-02 | 中国人民解放军空军工程大学航空机务士官学校 | Airplane attitude equipment testing system |
| CN114077225A (en) * | 2020-08-11 | 2022-02-22 | 北京机械设备研究所 | Universal embedded servo controller |
| CN114077225B (en) * | 2020-08-11 | 2023-11-14 | 北京机械设备研究所 | Generalized embedded servo controller |
| CN112557799A (en) * | 2020-12-12 | 2021-03-26 | 江西洪都航空工业集团有限责任公司 | Comprehensive CNI system testing device |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140903 Termination date: 20150314 |
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| EXPY | Termination of patent right or utility model |