CN106441914A - Display control combination testing system based on gas turbine engine application - Google Patents
Display control combination testing system based on gas turbine engine application Download PDFInfo
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- CN106441914A CN106441914A CN201610880230.0A CN201610880230A CN106441914A CN 106441914 A CN106441914 A CN 106441914A CN 201610880230 A CN201610880230 A CN 201610880230A CN 106441914 A CN106441914 A CN 106441914A
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- control
- display
- display control
- panel
- turbine engine
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M15/00—Testing of engines
- G01M15/04—Testing internal-combustion engines
- G01M15/05—Testing internal-combustion engines by combined monitoring of two or more different engine parameters
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Control Of Turbines (AREA)
Abstract
The invention discloses a display control combination testing system based on a gas turbine engine application. The system comprises a testing instrument, the testing instrument comprises a display control combination panel and one or more sets of external interfaces, the display control combination panel is composed of an information display panel and a control panel, and the control panel comprises multiple sets of functional control switches. The display control combination testing system based on a gas turbine engine can achieve detection and adjustment of overall performance of display control combination, and inspection and acceptance overall technical parameters of the display control combination, conduct localization and clearing on failures of the display control combination, conduct in-situ detection and failure clearing on the display control combination used in the outfield, and detect conditions of a system control signal.
Description
Technical field
The present invention relates to aobvious control combine detection technical field, more particularly, to a kind of aobvious based on gas turbine engine applications
Show control combination test system.
Background technology
At present, the production of display control combination (referred to as aobvious control combination), inspection do not have special tester.Grind for meeting
The demand that system produces, needs a powerful tester.
Content of the invention
It is an object of the invention to provide a kind of display control combined test system based on gas turbine engine applications,
Effectively solving above-mentioned technical problem.
For effectively solving above-mentioned technical problem, the technical scheme that the present invention takes is as follows：
Based on the display control combined test system of gas turbine engine applications, including a tester, described tester
Including aobvious control assembled panel and one or more groups of external-connected port, described aobvious control assembled panel is by information display panel and control panel
Composition, described control panel includes multiple function controlling switch.
Particularly, described information display floater is display, and described display shows the row of gas-turbine unit automatically
Totally 29 kinds of " failure code " information that temperature degree engine speed, number of starts information and system produce, described " failure code "
Set by different simulation input codes by aobvious control combined test instrument and verified.
Particularly, described external-connected port input direct-current analog power and message code, to simulate gas turbo-generator set
The control signal of each assembly in system, and detect the accuracy of display function.
Particularly, described control panel test aobvious control obtains message code and realizes excitation control when combining each specific function
System, and each specific function is combined in aobvious control and " message code " all has one-to-one relationship, after each functional test terminates, profit
Carry out " clearing " with " message code " to the various fault status informations of aobvious control combination display to process.
Beneficial effects of the present invention are：The display control combination based on gas turbine engine applications that the present invention provides is surveyed
Test system, can achieve the overall performance of detection debugging aobvious control combination；Check and accept the general technical parameter of aobvious control combination；To aobvious control combination
Fault positioned and excluded；To outfield with aobvious control combination carry out Site Detection and with troubleshooting and detecting system can control and believe
Number situation.
The present invention is described in detail below in conjunction with the accompanying drawings.
Brief description
Fig. 1 is the structural representation of the display control combined test system based on gas turbine engine applications of the present invention
Figure；
Fig. 2 is of the present invention based on control group aobvious in the display control combined test system of gas turbine engine applications
Close tester panel composition structural representation.
Specific embodiment
Embodiment 1：
Referring to Fig. 1-2, the disclosed display control combined test system based on gas turbine engine applications of the present embodiment,
Based on the display control combined test system of gas turbine engine applications, including a tester, described tester includes aobvious control
Assembled panel and one or more groups of external-connected port, described aobvious control assembled panel is made up of information display panel and control panel, institute
State control panel and include multiple function controlling switch.
Described information display floater is display, and described display shows that the delivery temperature of gas-turbine unit is sent out automatically
Totally 29 kinds of " failure code " information that motivation rotating speed, number of starts information and system produce.Described " failure code " is by aobvious control group
Close tester to be verified by different simulation input code settings.Described external-connected port input direct-current analog power and information generation
Code, to simulate the control signal of each assembly in gas turbo-generator set system, and detects the accuracy of display function.Described control
The aobvious control of panel test processed is combined and is obtained message code during each specific function and realize encouraging control, and each is special to show control combination
Function and " message code " all have one-to-one relationship, after each functional test terminates, using " message code " to aobvious control group
The various fault status informations closing display carry out " clearing " process.
Applicant state, person of ordinary skill in the field on the basis of above-described embodiment, by above-described embodiment
Step, combined with the technical scheme of Summary, thus produce new method, be also the present invention record scope it
One, the application is to make specification simple and clear, no longer enumerates the other embodiment of these steps.
The technology path being different from prior art in the present embodiment is：
In different port input direct-current analog power and the message code of tester, to simulate gas turbo-generator set system
The control signal of each assembly in system.And the accuracy of various display functions can be detected.Any on aobvious control assembled panel when connecting
During one functional switch, all can in tester panel corresponding Port detecting to corresponding voltage signal；Give in tester and produce
When product apply various " message codes " and add corresponding clock signal, the respective display on aobvious control assembled panel will show automatically
Show that information such as " delivery temperatures ", " engine speed ", " number of starts " of gas-turbine unit and system produce totally 29
" failure code " information of kind.
Core technology principle is as described below：
When each specific function is combined in the aobvious control of 1 test, the excitation of " message code " controls.
The corresponding relation of each specific function and " message code " is combined in 2 aobvious controls.
3 after each functional test terminates, using " message code " the various fault status informations to aobvious control combination display
" clearing " method.
The another statement of applicant, the present invention illustrates implementation method and the apparatus structure of the present invention by above-described embodiment,
But the invention is not limited in above-mentioned embodiment, that is, do not mean that the present invention has to rely on said method and structure could be real
Apply.Person of ordinary skill in the field it will be clearly understood that any improvement in the present invention, to implementation method selected by the present invention etc.
The interpolation of effect replacement and step, selection of concrete mode etc., within the scope of all falling within protection scope of the present invention and disclosure.
The present invention is not limited to above-mentioned embodiment, all to realize the present invention using with analog structure of the present invention and its method
All embodiments of purpose are all within the scope of the present invention.
Claims (4)
1. the display control combined test system based on gas turbine engine applications is it is characterised in that include a tester, institute
State tester and include aobvious control assembled panel and one or more groups of external-connected port, described aobvious control assembled panel by information display panel and
Control panel forms, and described control panel includes multiple function controlling switch.
2. the display control combined test system based on gas turbine engine applications according to claim 1, its feature
It is, described information display floater is display, described display shows that the delivery temperature of gas-turbine unit is started automatically
Totally 29 kinds of " failure code " information that machine rotating speed, number of starts information and system produce, described " failure code " is by aobvious control combination
Tester is set by different simulation input codes and is verified.
3. the display control combined test system based on gas turbine engine applications according to claim 1, its feature
It is, described external-connected port input direct-current analog power and message code, to simulate each group in gas turbo-generator set system
The control signal of part, and detect the accuracy of display function.
4. the display control combined test system based on gas turbine engine applications according to claim 1, its feature
It is, described control panel test obtains message code and realizes encouraging control when showing control each specific function of combination, and shows control
Combining each specific function all has one-to-one relationship with " message code ", after each functional test terminates, utilizes " information generation
Code " carries out " clearing " to the various fault status informations of aobvious control combination display and processes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610880230.0A CN106441914A (en) | 2016-10-09 | 2016-10-09 | Display control combination testing system based on gas turbine engine application |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610880230.0A CN106441914A (en) | 2016-10-09 | 2016-10-09 | Display control combination testing system based on gas turbine engine application |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106441914A true CN106441914A (en) | 2017-02-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201610880230.0A Pending CN106441914A (en) | 2016-10-09 | 2016-10-09 | Display control combination testing system based on gas turbine engine application |
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| CN (1) | CN106441914A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109696907A (en) * | 2019-01-29 | 2019-04-30 | 株洲耀辉光机电研究开发有限公司 | A kind of test macro of gas-turbine unit electricity generation system YHKZ-1 control combination |
| CN113093692A (en) * | 2021-03-16 | 2021-07-09 | 上海机电工程研究所 | Automatic testing method and system for ignition control system |
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| CN201489062U (en) * | 2009-03-27 | 2010-05-26 | 北京安达维尔科技有限公司 | Detecting system of aviation electronic display |
| CN201488749U (en) * | 2009-09-01 | 2010-05-26 | 芜湖华泰汽车仪表有限公司 | Novel meter detection equipment |
| CN202749014U (en) * | 2012-07-25 | 2013-02-20 | 南昌大学 | Common rail diesel engine experiment teaching system |
| CN202886104U (en) * | 2012-11-09 | 2013-04-17 | 东风汽车股份有限公司 | Fault diagnosis system for electric control engine bench test process |
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Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN2735324Y (en) * | 2004-09-17 | 2005-10-19 | 太原艾逖汽车检测设备有限公司 | Integrated test bench for engine, automatic transmission, ABS |
| CN201145987Y (en) * | 2007-12-26 | 2008-11-05 | 天津市圣威科技发展有限公司 | Car engine test stand |
| CN201489062U (en) * | 2009-03-27 | 2010-05-26 | 北京安达维尔科技有限公司 | Detecting system of aviation electronic display |
| CN201488749U (en) * | 2009-09-01 | 2010-05-26 | 芜湖华泰汽车仪表有限公司 | Novel meter detection equipment |
| CN202749014U (en) * | 2012-07-25 | 2013-02-20 | 南昌大学 | Common rail diesel engine experiment teaching system |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109696907A (en) * | 2019-01-29 | 2019-04-30 | 株洲耀辉光机电研究开发有限公司 | A kind of test macro of gas-turbine unit electricity generation system YHKZ-1 control combination |
| CN113093692A (en) * | 2021-03-16 | 2021-07-09 | 上海机电工程研究所 | Automatic testing method and system for ignition control system |
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Application publication date: 20170222 |