CN106199250A - A kind of aviation work card electronic system and operational approach thereof - Google Patents
A kind of aviation work card electronic system and operational approach thereof Download PDFInfo
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- CN106199250A CN106199250A CN201610486906.8A CN201610486906A CN106199250A CN 106199250 A CN106199250 A CN 106199250A CN 201610486906 A CN201610486906 A CN 201610486906A CN 106199250 A CN106199250 A CN 106199250A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
Abstract
The present invention relates to a kind of aviation work card electronic system and operational approach thereof, including Auto-Test System, test adapter, test cable and test program set；Auto-Test System is made up of power subsystem, data communication subsystem, DAQ data acquisition subsystem, switch subsystem, interface matrix subsystem, human-machine operation subsystem；Its operating procedure is: be connected with test cable by special test adapter by test product；Start corresponding test program set, it is achieved the automatic test to test product performance；Test data realize structured storage on program backstage；Program backstage manages system downloads corresponding work card template from electronics work card, and test data is inserted in work card according to bookmarked position；Typing is completed by program backstage electronics work card last time is to electronics work card management system.Present invention saves the work card data craft typing time of operator and coroner, avoid human error and the anthropic factor being likely to occur in Data Input Process completely.
Description
Technical field
The present invention relates to robot dynamical system technical field, specifically a kind of aviation work card electronic system and
Operational approach.
Background technology
In Aeronautic Equipment Repair enterprise, work card is generally used to realize the record detecting data in maintenance process, tradition
Recording process be in operator's manual transcription paper feed matter work card, it is slow not only to copy speed, and mistake, additionally data easily occur
Verity also lack and review reliably.
Summary of the invention
For the defect of above-mentioned technology, the present invention proposes a kind of aviation work card electronic system and operational approach thereof.
A kind of aviation work card electronic system, including Auto-Test System, test adapter, test cable and test journey
Sequence collection；Described Auto-Test System is by power subsystem, data communication subsystem, DAQ data acquisition subsystem, switch subsystem
System, interface matrix subsystem, human-machine operation subsystem composition.
Described power subsystem includes that 1 UPS uninterrupted power source instrument, 2 road program-control DC power instruments, 2 tunnels three are intersected
Stream programmable power supply instrument.UPS uninterrupted power source instrument is in parallel with program-control DC power instrument and three-phase alternating current programmable power supply instrument, and
And connection has PCI industrial computer.
Described data communication subsystem includes 2 road GJB-289A data bus interface boards, 8 road RS422 data interface boards
Card, 8 road RS232 data-interface boards, 10 road ARINC429 data-interface boards, 1 road gpib interface board, 2 road GJB-289A
Data bus interface board, 8 road RS422 data-interface boards, 8 road RS232 data-interface boards, 10 road ARINC429 data connect
Oralia card, 1 road gpib interface board are parallel with one another.In addition to gpib interface board is for the hardware instruments of control system, other
Data communication board is used to provide test product interface testing.
Described DAQ data acquisition subsystem include 8 road D/A interface boards, 8 road A/D interface boards, 1 road multimeter board,
64 road IO input interface boards, 128 road IO output interface boards.Described 8 road D/A interface boards, 8 road A/D interface boards, 1 tunnel
Multimeter board, 64 road IO input interface boards, 128 road IO output interface boards are parallel with one another.
Described switch subsystem includes 2 piece of 4 × 10 matrix switch board, 1 piece of 2 double 16 × 1 road multiplexer switch of line system
Board, 1 piece of 10 passage SPST power switch board, 1 piece of 16 passage SPDT power switch board.Described 2 piece of 4 × 10 matrix switch
Board, 1 piece of 2 line system double 16 × 1 road multiplexer switch boards, 1 piece of 10 passage SPST power switch board, 1 piece of 16 passage
SPDT power switch board is parallel with one another.
Described interface matrix subsystem include 16 road 50A power interface connectors, 96 road 10A power interface connectors,
1400 road 3A signal circuit interface connectors, 16 road coaxial signal interface connectors.Described 16 road 50A power interface connectors,
96 road 10A power interface connectors, 1400 road 3A signal circuit interface connectors, 16 road coaxial signal interface connectors are the most also
Connection.
Described human-machine operation subsystem composition includes 1 set PXI cabinet, 1 set display, key Mus, 1 set CPI industrial computer.Described
PXI cabinet installs PDM system, EOS system and office system.
Described display, key Mus are all connected with CPI industrial computer, and described CPI industrial computer controls card and power supply subsystem by CPI
System is connected.Described power subsystem is connected with interface matrix subsystem, and described PXI cabinet passes through data communication subsystem, DAQ number
It is connected with interface matrix subsystem according to acquisition subsystem, switch subsystem.Described test program set is in CPI industrial computer.
Described interface matrix subsystem is connected with test product by test cable.
Described 10 road ARINC429 data-interface boards include 5 receipts 5.
The operational approach of a kind of aviation work card electronic system, comprises the following steps:
The first step: test product is connected with test cable by special test adapter；
Second step: start corresponding test program set, it is achieved the automatic test to test product performance；
3rd step: test data realize structured storage on program backstage；
4th step: program backstage from electronics work card manage system downloads corresponding work card template, and will test data according to
Bookmarked position is inserted in work card；
5th step: typing is completed by program backstage electronics work card last time to electronics work card management system, and in instantiation
Store in work card classification and file.
The invention has the beneficial effects as follows:
Present invention saves the work card data craft typing time of operator and coroner, avoid Data Input Process completely
In the human error that is likely to occur and anthropic factor, it is ensured that the trackability of test data, be effectively increased aeronautical product dimension
Repair efficiency.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the electronics work card system annexation figure of the present invention；
Fig. 2 is the workflow diagram of the present invention.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below right
The present invention is expanded on further.
As depicted in figs. 1 and 2, a kind of aviation work card electronic system, including Auto-Test System, test adapter, survey
Examination cable and test program set；Described Auto-Test System is by power subsystem, data communication subsystem, DAQ data acquisition
Subsystem, switch subsystem, interface matrix subsystem, human-machine operation subsystem form.
Described power subsystem includes that 1 UPS uninterrupted power source instrument, 2 road program-control DC power instruments, 2 tunnels three are intersected
Stream programmable power supply instrument.UPS uninterrupted power source instrument is in parallel with program-control DC power instrument and three-phase alternating current programmable power supply instrument, and
And connection has PCI industrial computer.
Described data communication subsystem includes 2 road GJB-289A data bus interface boards, 8 road RS422 data interface boards
Card, 8 road RS232 data-interface boards, 10 road ARINC429 data-interface boards, 1 road gpib interface board, 2 road GJB-289A
Data bus interface board, 8 road RS422 data-interface boards, 8 road RS232 data-interface boards, 10 road ARINC429 data connect
Oralia card, 1 road gpib interface board are parallel with one another.In addition to gpib interface board is for the hardware instruments of control system, other
Data communication board is used to provide test product interface testing.
Described DAQ data acquisition subsystem include 8 road D/A interface boards, 8 road A/D interface boards, 1 road multimeter board,
64 road IO input interface boards, 128 road IO output interface boards.Described 8 road D/A interface boards, 8 road A/D interface boards, 1 tunnel
Multimeter board, 64 road IO input interface boards, 128 road IO output interface boards are parallel with one another.
Described switch subsystem includes 2 piece of 4 × 10 matrix switch board, 1 piece of 2 double 16 × 1 road multiplexer switch of line system
Board, 1 piece of 10 passage SPST power switch board, 1 piece of 16 passage SPDT power switch board.Described 2 piece of 4 × 10 matrix switch
Board, 1 piece of 2 line system double 16 × 1 road multiplexer switch boards, 1 piece of 10 passage SPST power switch board, 1 piece of 16 passage
SPDT power switch board is parallel with one another.
Described interface matrix subsystem include 16 road 50A power interface connectors, 96 road 10A power interface connectors,
1400 road 3A signal circuit interface connectors, 16 road coaxial signal interface connectors.Described 16 road 50A power interface connectors,
96 road 10A power interface connectors, 1400 road 3A signal circuit interface connectors, 16 road coaxial signal interface connectors are the most also
Connection.
Described human-machine operation subsystem composition includes 1 set PXI cabinet, 1 set display, key Mus, 1 set CPI industrial computer.
Described display, key Mus are all connected with CPI industrial computer, and described CPI industrial computer controls card and power supply subsystem by CPI
System is connected.Described power subsystem is connected with interface matrix subsystem, and described PXI cabinet passes through data communication subsystem, DAQ number
It is connected with interface matrix subsystem according to acquisition subsystem, switch subsystem.Described test program set is in CPI industrial computer.
Described interface matrix subsystem is connected with test product by test cable.
Described 10 road ARINC429 data-interface boards include 5 receipts 5.
The operational approach of a kind of aviation work card electronic system, comprises the following steps:
The first step: test product is connected with test cable by special test adapter；
Second step: start corresponding test program set, it is achieved the automatic test to test product performance；
3rd step: test data realize structured storage on program backstage；
4th step: program backstage from electronics work card manage system downloads corresponding work card template, and will test data according to
Bookmarked position is inserted in work card；
5th step: typing is completed by program backstage electronics work card last time to electronics work card management system, and in instantiation
Store in work card classification and file.
Described PXI cabinet installs PDM system, EOS system and office system.
During use, in order to be able to the job content of above-mentioned five steps, to PDM system, EOS system, the tool of office system
Body requires:
Described PDM system is supported therefore the examination & approval function of inspection job card template, stores function.Group when supporting therefore examine information processing
The examination & approval function of the non-routine troubleshooting card born.
Printing function in described work card management system, support by instantiation thus inspection work card print, print simultaneously
Complete preservation and the version management of all instantiation job cards.
Office word in described office system supports the single-sign-on with EOS system.Support thus inspection work complete
Cheng Hou, therefore inspection conclusion and the filling in of handling suggestion.During preservation trigger derive from preserve thus inspection transmission card and EOS in thus inspection flow of information
Journey.
Described EOS system support realizes the integrated of webservice with office word, and support process is by office
Word triggers.Derivative in office word therefore inspection transmission card link is added in EOS flow chart automatically.
The ultimate principle of the present invention, principal character and advantages of the present invention have more than been shown and described.The technology of the industry
The personnel simply present invention it should be appreciated that the present invention is not restricted to the described embodiments, described in above-described embodiment and description
Principle, without departing from the spirit and scope of the present invention, the present invention also has various changes and modifications, these change and
Improvement both falls within claimed invention.Claimed scope is by appending claims and equivalent circle thereof
Fixed.
Claims (4)
1. an aviation work card electronic system, it is characterised in that: include Auto-Test System, test adapter, test cable
And test program set；Described Auto-Test System by power subsystem, data communication subsystem, DAQ data acquisition subsystem,
Switch subsystem, interface matrix subsystem, human-machine operation subsystem form；
Described power subsystem includes 1 UPS uninterrupted power source instrument, 2 road program-control DC power instruments, 2 road three-phase alternating current journeys
Control power supply instrument；UPS uninterrupted power source instrument is in parallel with program-control DC power instrument and three-phase alternating current programmable power supply instrument, and and connects
It is connected to PCI industrial computer；
Described data communication subsystem include 2 road GJB-289A data bus interface boards, 8 road RS422 data-interface boards, 8
Road RS232 data-interface board, 10 road ARINC429 data-interface boards, 1 road gpib interface board, 2 road GJB-289A data
EBI board, 8 road RS422 data-interface boards, 8 road RS232 data-interface boards, 10 road ARINC429 data interface boards
Card, 1 road gpib interface board are parallel with one another；In addition to gpib interface board is for the hardware instruments of control system, other data
Communication Card is used to provide test product interface testing；
Described DAQ data acquisition subsystem includes 8 road D/A interface boards, 8 road A/D interface boards, 1 road multimeter board, 64 tunnels
IO input interface board, 128 road IO output interface boards；Described 8 road D/A interface boards, 8 road A/D interface boards, 1 tunnel are multiplex
Dash board card, 64 road IO input interface boards, 128 road IO output interface boards are parallel with one another；
Described switch subsystem include 2 piece of 4 × 10 matrix switch board, 1 piece of 2 double 16 × 1 road multiplexer switch board of line system,
1 piece of 10 passage SPST power switch board, 1 piece of 16 passage SPDT power switch board；Described 2 piece of 4 × 10 matrix switch board,
1 piece of 2 line system double 16 × 1 road multiplexer switch boards, 1 piece of 10 passage SPST power switch board, 1 piece of 16 passage SPDT power
Switch board is parallel with one another；
Described interface matrix subsystem includes 16 road 50A power interface connectors, 96 road 10A power interface connectors, 1400 tunnels
3A signal circuit interface connector, 16 road coaxial signal interface connectors；Described 16 road 50A power interface connectors, 96 road 10A
Power interface connector, 1400 road 3A signal circuit interface connectors, 16 road coaxial signal interface connectors are parallel with one another；
Described human-machine operation subsystem composition includes 1 set PXI cabinet, 1 set display, key Mus, 1 set CPI industrial computer；
Described display, key Mus are all connected with CPI industrial computer, and described CPI industrial computer controls card and power subsystem phase by CPI
Even；Described power subsystem is connected with interface matrix subsystem, and described PXI cabinet passes through data communication subsystem, DAQ data acquisition
Subsystem, switch subsystem are connected with interface matrix subsystem；Described test program set is in CPI industrial computer；
Described interface matrix subsystem is connected with test product by test cable.
A kind of aviation work card electronic system the most according to claim 1, it is characterised in that: described 10 road ARINC429 numbers
5 receipts 5 are included according to interface board.
The operational approach of a kind of aviation work card electronic system the most according to claim 1 and 2, it is characterised in that: include
Following steps:
The first step: test product is connected with test cable by special test adapter；
Second step: start corresponding test program set, it is achieved the automatic test to test product performance；
3rd step: test data realize structured storage on program backstage；
4th step: program backstage manages system downloads corresponding work card template from electronics work card, and will test data according to bookmark
Mark position is inserted in work card；
5th step: typing is completed by program backstage electronics work card last time to electronics work card management system, and at instantiation work card
Store in classification and file.
The operational approach of a kind of aviation work card electronic system the most according to claim 3, it is characterised in that: described PXI
Cabinet installs PDM system, EOS system and office system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610486906.8A CN106199250B (en) | 2016-06-28 | 2016-06-28 | A kind of aviation work card electronic system and its operating method |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610486906.8A CN106199250B (en) | 2016-06-28 | 2016-06-28 | A kind of aviation work card electronic system and its operating method |
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| Publication Number | Publication Date |
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| CN106199250A true CN106199250A (en) | 2016-12-07 |
| CN106199250B CN106199250B (en) | 2018-12-11 |
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| US5036479A (en) * | 1989-04-20 | 1991-07-30 | Trw Inc. | Modular automated avionics test system |
| CN101575011A (en) * | 2009-05-05 | 2009-11-11 | 中国民航大学 | Automatic test equipment of boeing series aircraft audio management unit and method thereof |
| CN201532421U (en) * | 2009-05-31 | 2010-07-21 | 广州飞机维修工程有限公司 | Audio control panel test device for airliners in civil aviation |
| CN203070097U (en) * | 2013-02-07 | 2013-07-17 | 四川海特高新技术股份有限公司 | Comprehensive test device based on aviation flight management control display assembly |
| CN103414529A (en) * | 2013-08-26 | 2013-11-27 | 华北计算技术研究所 | Universal automatic testing and fault diagnosis system |
| CN203422426U (en) * | 2013-06-09 | 2014-02-05 | 广州飞机维修工程有限公司 | Universal comprehensive automatic test system of airborne computer of civilian airliner |
-
2016
- 2016-06-28 CN CN201610486906.8A patent/CN106199250B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5036479A (en) * | 1989-04-20 | 1991-07-30 | Trw Inc. | Modular automated avionics test system |
| CN101575011A (en) * | 2009-05-05 | 2009-11-11 | 中国民航大学 | Automatic test equipment of boeing series aircraft audio management unit and method thereof |
| CN201532421U (en) * | 2009-05-31 | 2010-07-21 | 广州飞机维修工程有限公司 | Audio control panel test device for airliners in civil aviation |
| CN203070097U (en) * | 2013-02-07 | 2013-07-17 | 四川海特高新技术股份有限公司 | Comprehensive test device based on aviation flight management control display assembly |
| CN203422426U (en) * | 2013-06-09 | 2014-02-05 | 广州飞机维修工程有限公司 | Universal comprehensive automatic test system of airborne computer of civilian airliner |
| CN103414529A (en) * | 2013-08-26 | 2013-11-27 | 华北计算技术研究所 | Universal automatic testing and fault diagnosis system |
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| CN106199250B (en) | 2018-12-11 |
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Effective date of registration: 20190321 Address after: 241000 Yongjiang community, Qingshui street, Jiujiang District, Wuhu, Anhui Patentee after: Wuhu Tian hang Equipment Technology Co., Ltd. Address before: 241000 Wanli Airport, Wuhu City, Anhui Province Patentee before: State run Wuhu machinery plant |