CN104808087A - Power supply testing system for onboard advanced training equipment - Google Patents

Power supply testing system for onboard advanced training equipment Download PDF

Info

Publication number
CN104808087A
CN104808087A CN201510222405.4A CN201510222405A CN104808087A CN 104808087 A CN104808087 A CN 104808087A CN 201510222405 A CN201510222405 A CN 201510222405A CN 104808087 A CN104808087 A CN 104808087A
Authority
CN
China
Prior art keywords
test
module
testing
power supply
test mode
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.)
Pending
Application number
CN201510222405.4A
Other languages
Chinese (zh)
Inventor
翁敏捷
周水娇
万启星
万美龙
关华云
漆文彪
刘诚
刘茹萍
徐柳琴
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jiangxi Hongdu Aviation Industry Group Co Ltd
Original Assignee
Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Jiangxi Hongdu Aviation Industry Group Co Ltd filed Critical Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority to CN201510222405.4A priority Critical patent/CN104808087A/en
Publication of CN104808087A publication Critical patent/CN104808087A/en
Pending legal-status Critical Current

Links

Abstract

The invention discloses a power supply testing system for onboard advanced training equipment. The power supply testing system comprises a main interface, an automatic test mode module, a single-step test mode module, a data acquiring and resolving module and a test record displaying and judging module. The main interface is capable of uniformly calling multiple test items; each test item can call the automatic test mode module and the single-step test mode module to perform automatic testing, so that correctness of power supply circuit connection on an airplane, power supply logicality for each system on the airplane, correctness of state conversion and simulated statuses of multiple sensors on the airplane can be tested; the data acquiring and resolving module can be called to resolve the tested statuses into digital signals; finally test results and fault positions can be displayed and stored by the test record displaying and judging module. The power supply testing system for the onboard advanced training equipment has the advantages that degree of automation in a testing process is increased, testing efficiency and testing accuracy are improved greatly, human factors in the testing process are reduced, testing work is freed from complex manual testing, and research and development tasks of an advanced training machine are guaranteed smoothly.

Description

Higher education airborne equipment is for electricity detecting system
Technical field
The present invention relates to a kind of for electricity detecting system, particularly relate to a kind of higher education airborne equipment for electricity detecting system.
Background technology
Higher education machine is the domestic third generation advaced trainer newly developed, full machine have employed avionics system and the novel airborne electronic apparatus system of high integrity, test theory has had the change of essence, except the requirement tested before will meeting into annex dress, also to adapt to the integration test needs of important subsystem, system, wherein full machine each system airborne equipment energising detection is an important test link, directly affects the safety of aircraft.At present, special testing equipment is not had at general assembly test phase, only testing apparatus backwardness relatively, function is relatively single, most test assignment can only adopt very easy manual test method, because checking that job is various, greatly have impact on the effect of test, have impact on installation progress widely.Therefore be necessary that a set of new higher education airborne equipment of research and development is for electricity detecting system, solve the airborne equipment newly grinding type and to power test item problem.
Summary of the invention
The technical issues that need to address of the present invention are to provide a kind of higher education airborne equipment for electricity detecting system.Improve automaticity in test process, can greatly improve testing efficiency and accuracy, reduce the human factor in test process, testing is freed from loaded down with trivial details manual testing, has ensured new higher education machine development & production task smoothly.
For solving technical matters of the present invention, the technical solution used in the present invention is:
Higher education airborne equipment is for electricity detecting system, this confession electricity detecting system comprises main interface, automatic test mode module, single stepping test mode module, module and test record display judge module are resolved in data acquisition, main unify menu calls multiple test event, each test event can call automatic test mode module and single stepping test mode module detects automatically, detect the correctness that aircraft Ji Shang supply line connects, the logicality of each system power supply on aircraft, the state of multiple sensor on the correctness of State Transferring and simulated aircraft, calling data collection is resolved module and above-mentioned detected state solution is counted as digital signal, finally by test record display judge module display and store test results and abort situation.
Beneficial effect of the present invention: higher education airborne equipment meets the technical requirement of each system power supply performance of new higher education machine and electrical control Function detection completely for electricity detecting system, solve the current series of problems brought due to manual testing, improve automaticity in test process simultaneously, can greatly improve testing efficiency and accuracy, reduce the human factor in test process, testing is freed from loaded down with trivial details manual testing, has ensured new higher education machine development & production task smoothly.
Accompanying drawing explanation
Fig. 1 is theory diagram of the present invention.
Fig. 2 is that combined-voltage signals collecting of the present invention resolves process flow diagram.
Fig. 3 is that discrete signal of the present invention controls and process flow diagram is resolved in collection.
Fig. 4 is test data of the present invention display decision flow chart.
1, main interface, 2, automatically test mode module, 3, single stepping test mode module, 4, data acquisition resolves module, 5, test record display judge module.
Embodiment
Below in conjunction with the drawings and specific embodiments, the invention will be further described.Following examples, only for illustration of the present invention, are not used for limiting the scope of the invention.
Shown in Fig. 1, higher education airborne equipment of the present invention is for electricity detecting system, this confession electricity detecting system comprises main interface 1, automatic test mode module 2, single stepping test mode module 3, module 4 and test record display judge module 5 are resolved in data acquisition, the multiple test event of main interface 1 unified call, each test event can call automatic test mode module 2 and single stepping test mode module 3 detects automatically, detect the correctness that aircraft Ji Shang supply line connects, the logicality of each system power supply on aircraft, the state of multiple sensor on the correctness of State Transferring and simulated aircraft, calling data collection is resolved module 4 and above-mentioned detected state solution is counted as digital signal, show and store test results and abort situation finally by test record display judge module 5.
Each test event can call automatic test mode module and single stepping test mode module detects automatically, specific as follows:
Under automatic test mode, automatically test first check point that detection system can be set up from this test item, and the explanation of dependence test Operating Guideline is provided, first detection system can be extracted this check point content measurement and passes to data acquisition and resolve module, resolve the collection of module settling signal by data acquisition and resolve function, and data feedback is shown judge module to test record, test record display judge module can by test data with digital frame, the modes such as virtual pilot lamp and virtual switch show in this check point of test item interface " test mode ", and require test data automatic analysis according to energising Examined effect condition and technical parameter, whether qualifiedly the test of this check point is identified with " √ " or "×" in " result ".Then enter the test of next check point, will carry out successively testing by above-mentioned design cycle for all the other check point systems of this test item until complete the test of all check points.
Under single stepping test mode, system is designed to only to test certain check point of appointment according to testing process, just stops test after the test of this check point.This function for certain test event comprise more check point time, find that certain check point fault can use the state of this check point of test fast after single stepping test through maintenance adjustment, greatly improve testing efficiency.
The data acquisition of native system is resolved module 4 and has mainly been completed: 1, shown in Fig. 2, the collection of combined-voltage signal is resolved, by PCI-1710 gather relay multi channel selecting plate PCLD-788(combine exchange modular converter WBV462U01) data of corresponding check point passage, then according to reduction formula, data are resolved into corresponding combined-voltage signal; 2, discrete control, by digital quantity I/O card PCI-722 according to testing requirement sending controling instruction, the short circuit of pilot relay output board PCLD-785 respective channel or off-state; 3, shown in Fig. 3, digital quantity is measured: by digital quantity I/O card PCI-722 according to testing requirement sending controling instruction, the short circuit state of pilot relay output board PCLD-785 respective channel, again with check point passage corresponding to relay multi channel selecting plate PCLD-788 be combined into a loop, last PCI-1710 gather resolve this loop voltage condition to judge the conduction in this loop.
Shown in Fig. 4, test record display judge module 5 is mainly used to show the record of net result, this module can by test data with digital frame, the modes such as virtual pilot lamp and virtual switch show in this check point of test item interface " test mode ", whole test interface is friendly and attractive in appearance, and require test data automatic analysis according to energising Examined effect condition and technical parameter, whether qualifiedly the test of this check point is identified with " √ " or "×" in " result ", automaticity is high, greatly can improve testing efficiency, reduce the human factor of product test.
Each test event can call automatic test mode and single stepping test mode detects automatically, detect the correctness that on aircraft, supply line connects, the logicality of each system power supply on aircraft, the state of multiple sensor on the correctness of State Transferring and simulated aircraft, calling data collection is resolved module and above-mentioned detected state solution is counted as digital signal, finally by test record display judge module display and store test results and abort situation, improve automaticity in test process, greatly improve testing efficiency and accuracy, reduce the human factor in test process, testing is freed from loaded down with trivial details manual testing, ensure new higher education machine development & production task smoothly.

Claims (1)

1. higher education airborne equipment is for electricity detecting system, it is characterized in that: this confession electricity detecting system comprises main interface, automatic test mode module, single stepping test mode module, module and test record display judge module are resolved in data acquisition, main unify menu calls multiple test event, each test event can call automatic test mode module and single stepping test mode module detects automatically, detect the correctness that aircraft Ji Shang supply line connects, the logicality of each system power supply on aircraft, the state of multiple sensor on the correctness of State Transferring and simulated aircraft, calling data collection is resolved module and above-mentioned detected state solution is counted as digital signal, finally by test record display judge module display and store test results and abort situation.
CN201510222405.4A 2015-05-05 2015-05-05 Power supply testing system for onboard advanced training equipment Pending CN104808087A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510222405.4A CN104808087A (en) 2015-05-05 2015-05-05 Power supply testing system for onboard advanced training equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510222405.4A CN104808087A (en) 2015-05-05 2015-05-05 Power supply testing system for onboard advanced training equipment

Publications (1)

Publication Number Publication Date
CN104808087A true CN104808087A (en) 2015-07-29

Family

ID=53693085

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510222405.4A Pending CN104808087A (en) 2015-05-05 2015-05-05 Power supply testing system for onboard advanced training equipment

Country Status (1)

Country Link
CN (1) CN104808087A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111398840A (en) * 2018-12-17 2020-07-10 北京华航无线电测量研究所 Multi-power output normal indicating system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101169634A (en) * 2007-11-22 2008-04-30 江西洪都航空工业集团有限责任公司 Machine-mounted apparatus power supply detecting bench
CN201072597Y (en) * 2007-07-06 2008-06-11 上海凯迪克航空工程技术有限公司 Automatic detection instrument for aviation electronic flight instrument
CN201335775Y (en) * 2008-10-17 2009-10-28 四川海特高新技术股份有限公司 Airborne equipment comprehensive detection system

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201072597Y (en) * 2007-07-06 2008-06-11 上海凯迪克航空工程技术有限公司 Automatic detection instrument for aviation electronic flight instrument
CN101169634A (en) * 2007-11-22 2008-04-30 江西洪都航空工业集团有限责任公司 Machine-mounted apparatus power supply detecting bench
CN201335775Y (en) * 2008-10-17 2009-10-28 四川海特高新技术股份有限公司 Airborne equipment comprehensive detection system

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
吕永健 等: "基于PC/104总线的飞机综合告警系统自动测试设备", 《空军工程大学学报(自然科学版)》 *
曹乃森 等: "机载塔康设备综合检查仪设计", 《计算机测量与控制》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111398840A (en) * 2018-12-17 2020-07-10 北京华航无线电测量研究所 Multi-power output normal indicating system

Similar Documents

Publication Publication Date Title
CN102692598B (en) Electric cabinet logic tester device of railway vehicle
CN201917640U (en) PCB testing system
CN103336194A (en) Integrated automatic test system of on-board computer of civilian airliner
CN109884367B (en) Testing system and method for resident user load identification module
CN105158718A (en) Fault indicator comprehensive testing method and testing system
CN104849582A (en) System and method for overcurrent protection and voltage monitoring device burn-in test
CN103941207A (en) Electric power measurement automation terminal detection method and system
CN108803564B (en) Automatic testing system and method for communication control equipment
CN106443311A (en) Conduction and insulation test system and method of large aircraft automatic system
CN105223897A (en) A kind of rolling stock electrical control cabinet proving installation and method of testing
CN103616560A (en) Automatic power consumption parameter testing device and method applied to avionics device
CN201926754U (en) Intelligent function detecting device of distribution network short circuit fault indicator
CN104236614B (en) The method and apparatus for detecting vehicle-mounted CAN bus type automobile instrument endurance quality
CN202433505U (en) Automatic detection system of airplane start generator
CN109613418A (en) Thyristor valves high potential board test device and test method
CN103699113A (en) Circuit and method for self-detection of ADLC (advanced diesel locomotive controller)
CN203422426U (en) Universal comprehensive automatic test system of airborne computer of civilian airliner
CN201654186U (en) Large-scale signal detecting equipment
CN104808087A (en) Power supply testing system for onboard advanced training equipment
CN105629188A (en) Nuclear power plant inverter voltage monitoring card integrated test system and test method
CN111983546A (en) Ammeter detection configuration device and method
CN204043759U (en) Liquid level sensor automatic testing equipment
CN104316863A (en) Artificial intelligence-based universal circuit debugging and troubleshooting interaction system and method
CN103207618B (en) A kind of Electric Control System of Coal Cutter comprehensive detector
CN204256118U (en) Universal circuit debugging and fault maintenance interactive system

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20150729

WD01 Invention patent application deemed withdrawn after publication