CN110377010A - A kind of arbitrarily extensible DCS system automatic test device and test method - Google Patents

A kind of arbitrarily extensible DCS system automatic test device and test method Download PDF

Info

Publication number
CN110377010A
CN110377010A CN201910743717.8A CN201910743717A CN110377010A CN 110377010 A CN110377010 A CN 110377010A CN 201910743717 A CN201910743717 A CN 201910743717A CN 110377010 A CN110377010 A CN 110377010A
Authority
CN
China
Prior art keywords
test
module
signal
dcs system
dcs
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
CN201910743717.8A
Other languages
Chinese (zh)
Inventor
文景
马权
肖鹏
刘明明
贺先建
罗庚
徐世豪
陈阳
陈钊
王小雨
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.)
CHINA NUCLEAR CONTROL SYSTEM ENGINEERING Co.,Ltd.
Original Assignee
Nuclear Power Institute of China
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 Nuclear Power Institute of China filed Critical Nuclear Power Institute of China
Priority to CN201910743717.8A priority Critical patent/CN110377010A/en
Publication of CN110377010A publication Critical patent/CN110377010A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00Testing or monitoring of control systems or parts thereof
    • G05B23/02Electric testing or monitoring
    • G05B23/0205Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0208Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the configuration of the monitoring system
    • G05B23/0213Modular or universal configuration of the monitoring system, e.g. monitoring system having modules that may be combined to build monitoring program; monitoring system that can be applied to legacy systems; adaptable monitoring system; using different communication protocols
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00Program-control systems
    • G05B2219/20Pc systems
    • G05B2219/24Pc safety
    • G05B2219/24065Real time diagnostics

Abstract

The invention discloses a kind of arbitrarily extensible DCS system automatic test devices, including host computer, test output input cabinet;Master controller is divided into test I/O module transfer signal and test network transmission signal for that will test signal, and test is transferred to the I/O module of DCS system with I/O module transfer signal by the hardwire of I/O module, and test is transferred to the network communication module of DCS system with network transmission signal by the optical fiber that DCS docks network communication module, after testing signal by above-mentioned transmission, so that the master controller of DCS system passes through its I/O module respectively and network communication module obtains test signal, the master controller of DCS system modifies to its IO variable according to test signal;Master controller is also used to after DCS system makes feedback, when forming state parameter, is docked network communication module by the test output input I/O module of cabinet itself, DCS respectively and is obtained and is returned after the state parameter of DCS system to host computer.

Description

A kind of arbitrarily extensible DCS system automatic test device and test method
Technical field
The present invention relates to the fields nuclear power station security level DCS, and in particular to a kind of arbitrarily extensible DCS system automation survey Trial assembly is set and its test method.
Background technique
Existing nuclear power plant DCS I &C equipment automatic test device mainly simulates live input signal, and acquisition subject is set Standby output signal, and back production signal is compared with desired value, to verify whether tested device function meets the requirements.It is formed It mainly include the hardware devices such as industrial personal computer, display, main controller module, power module, communication module, I/O module.When DCS system When I O point quantity of uniting is more than the I O point number of test device, test device can then be unable to satisfy test request.Common method is to expand Test device scale purchases new cabinet and I/O module.The method higher cost, increases wiring workload, and cannot and When solve the problems, such as.
Summary of the invention
The purpose of the present invention is to provide a kind of arbitrarily extensible DCS system automatic test devices and its test side Method;This method can cover the gearing test of all of the port and logic with lower cost.
The specific technical proposal of the invention is:
A kind of arbitrarily extensible DCS system automatic test device, including host computer, test output input cabinet;
Test output input cabinet includes that master controller and master controller establish the I/O module of data transmission link, DCS Network communication module, host computer docking network communication module are docked, wherein host computer docking network communication module is built with host computer Vertical network communication, DCS docking network communication module are used to establish network communication with the network communication module of DCS system;I/O module It is connect for the I/O module with DCS system;
Host computer is used to obtain test case post analysis and obtains test signal and anticipatory data and pass through test signal Position machine docking network communication module is distributed to master controller;
Master controller is divided into test I/O module transfer signal and test network transmission signal for that will test signal, And test is transferred to the I/O module of DCS system with I/O module transfer signal by the hardwire of I/O module, and test is used Network transmission signal is transferred to the network communication module of DCS system by the optical fiber that DCS docks network communication module, by above-mentioned After transmission test signal, the master controller of DCS system is made to pass through its I/O module and network communication module acquisition test letter respectively Number, the master controller of DCS system modifies to its IO variable according to test signal;
Master controller is also used to pass through test output input respectively after DCS system makes feedback, when forming state parameter It is returned after the I/O module of cabinet itself, the state parameter of DCS docking network communication module acquisition DCS system to host computer;
Host computer generates test report after being also used to be compared according to state parameter with anticipatory data.
Design principle of the invention are as follows:
Due to more than DCS system I O point quantity (a large amount of signal (signal up to ten thousand) test requirements documents, existing test device it is defeated Outgoing interface and input interface are few, cannot achieve all standing requirement to test point, use to solve this method prior art 2 kinds of mentalities of designing, the first is carried out using the method for increasing interface module, in the way of mould group, is needing more tests When point, increase interface module, this method it is at high cost, need to be arranged according to different test cases different interface connections, therefore survey Try inefficiency.Second of test method is whole network data test method, i.e., network interface is arranged in test device, passes through Network interface issues data and passback feedback data is communicated with DCS system, and there are a deadly defects for this method, i.e., can only carry out The verification test of DCS system logic, the transmission of data are all to be directly over network module to enter in the master controller of DCS, are not had Have and communicated by I/O mouthfuls, therefore complete test in the case where I/O port transmission can not be formed in, lacks scientific feasibility.
In order to guarantee that test is scientific and solve the problems, such as that interface deficiency, the present invention are provided with main control in test device Device, and the data-interface for docking with DCS is provided with 2 kinds of designs coexisted, one is conventional I/O port transmission form, One is the transmission forms of network interface, not simple to rely on any transmission form in test, but two kinds transmit Form carries out simultaneously, needs interface excessively in the current unappeasable situation of test device I/O interface in test case, from Network interface configures test data, so that the data transmission that cannot provide interface provides network interface and completes, core is in master Under the control of controller, the transmission of network data and I/O data is synchronously completed, wherein extension is realized pair using network communication The modification and reading of IO variable, reduce the dependence to test device IO physical points in DCS system.The device can reduce wiring Workload reduces cost, improves testing efficiency.
Preferably,
The I/O module of the test output input cabinet includes analog output module, switching value output module, analog quantity Input module, switching input module.
The analog output module, switching value output module, Analog input mModule, switching input module selection are same Walk module of the time no more than 5ms.
Since the form that network transmission and I/O are transmitted is different, there are problems that time delay, and DCS system is needed same One moment provided corresponding feedback according to test signal, if there is time delay, will lead to feedback signal disorder, leads to test errors And failure, in order to solve this problem, present applicant proposes at least following two solution, the core concepts of following two schemes It is the time delay by calculating two kinds of accesses, calculation delay is poor, delay inequality counted when controlling signal and sending, so that The signal for reaching DCS system can be solved the above problems with this in synchronization.
Preferably, the first solves delay problem are as follows:
Master controller is T1 at the time of sending and testing with I/O module transfer signal to I/O module, and master controller is being sent Test is T2 at the time of docking network communication module to DCS with network transmission signal, before wherein master controller setting T2 is T1 At the time of, the difference between T2 and T1 is to ensure that DCS system receives test I/O module transfer signal and test in synchronization Calculating acquisition is carried out with the actual conditions of network transmission signal.
Mode at the time of master controller is arranged before T2 is T1 is that T2, T1 is arranged using programmed method.
This method is realized due to the method for software programming, is first tested master controller and is sent test I/O module biography After defeated signal, DCS system receives the time delay that I/O module transfer signal is used in test, and then re-test master controller sends test After network transmission signal, DCS system receives the time delay of test network transmission signal, and the difference of 2 time delays is calculated Out, it to go the difference of control T2, T1, thus can solve delay problem, guarantee that DCS can be synchronized and receive 2 accesses and send Signal.
Preferably, second of solution delay problem are as follows:
The I/O module of test output input cabinet is T11 at the time of sending and testing I/O module transfer signal, test The DCS docking network communication module of output input cabinet is T12 at the time of sending test network transmission signal, wherein T12 At the time of for before T11, the difference between T12 and T11 is passed with ensureing that DCS system receives test I/O module in synchronization The actual conditions of defeated signal and test network transmission signal carry out calculating acquisition.
Mode at the time of setting before T12 is T11 are as follows: obtain test in the I/O module that test exports input cabinet and use Delay circuit is set before I/O module transfer signal or after obtaining test I/O module transfer signal.
The core of the method for the solution time delay is that the delay circuit of hardware is arranged, controls signal by delay circuit and send Moment, likewise, DCS system receives test I/ after it first tests master controller transmission test I/O module transfer signal O module transmits the time delay of signal, and after then re-test master controller sends test network transmission signal, DCS system is received The test time delay of network transmission signal, the difference of 2 time delays is calculated, to go the difference of control T12, T11, in this way Delay problem can be solved, guarantees that DCS can be synchronized and receives the signal that 2 accesses are sent.
In principal it is also possible at the time of resolving test signal by master controller in setting DCS system, thus delay of control Problem, but as testing experiment, do not allow generally to be configured equipment under test, therefore this method is as worst alternative approach.
It preferably, further include from extension cabinet when test interface is also insufficient;The test output inputs cabinet and further includes From expansion card, test output input cabinet master controller is by establishing communication link, main control from expansion card with from extension cabinet Test signal is also divided into test with from expansion I/O module transfer signal by device, is provided with main expansion card, I/O out of extension cabinet Module, test are extended in cabinet with from expansion I/O module transfer signal by being transferred to from the main expansion card in extension cabinet I/O module, then by the I/O module transfer in extension cabinet to DCS system.It is arranged from the purpose of extension cabinet and setting and tests The principle of the I/O module of output input cabinet is consistent, and increases I/O interface quantity, and purpose is all simulation SOP/BUP/ LEVEL0 layers of external system device, it is required that being configured with analog signals and digital quantity signal, analog spot sensor, core instrument Table signal, safety hand operation panel and Safety actuator and acquisition shutdown breaker signal.
Preferably, when being tested using only test output input cabinet:
A kind of test method based on arbitrarily extensible DCS system automatic test device, comprising the following steps:
After the external testing use-case obtained by host computer, test case is resolved into survey using test case processing software Trial signal and anticipatory data;
Signal, which will be tested, by master controller resolves to test I/O module transfer signal and survey according to transmission path difference Network transmission signal on probation;
The I/ that DCS system is sent to I/O module transfer signal will be tested by the I/O module that test exports input cabinet O module,
Network communication module is docked by the DCS that test exports input cabinet to be sent to test with network transmission signal The network communication module of DCS system;
DCS system repairs its IO variable with network transmission signal according to test I/O module transfer signal and test Change;
The I/O module of input cabinet is exported by test, DCS docks network communication module acquisition DCS system and IO is become State parameter out is fed back after amount variation;
By exporting test report with after anticipatory data comparison after host computer back production state parameter.
When using test output input cabinet and from extension cabinet:
A kind of test method based on arbitrarily extensible DCS system automatic test device, comprising the following steps:
After the external testing use-case obtained by host computer, test case is resolved into survey using test case processing software Trial signal and anticipatory data;
Signal, which will be tested, by master controller resolves to test I/O module transfer signal and survey according to transmission path difference On probation network transmission signal, test are with from expansion I/O module transfer signal;
The I/ that DCS system is sent to I/O module transfer signal will be tested by the I/O module that test exports input cabinet O module,
Network communication module is docked by the DCS that test exports input cabinet to be sent to test with network transmission signal The network communication module of DCS system;
It will be tested by the slave expansion card that test exports input cabinet and be sent to from expansion I/O module transfer signal from expansion Cabinet is opened up, then will be tested with the I/O for being sent to DCS system from expansion I/O module transfer signal by the I/O module from extension cabinet Module;
DCS system is according to test I/O module transfer signal and test network transmission signal, test with from expansion I/O Module transfer signal modifies to its IO variable;
The input I/O module of cabinet is exported by test, DCS docks network communication module, from the I/O module of extension cabinet DCS system is obtained for feeding back state parameter out after IO variable change;
By exporting test report with after anticipatory data comparison after host computer back production state parameter.
Compared with prior art, the present invention having the following advantages and benefits: during testing certain DCS system, Since the DCS system I O point is more, needs automatic test device to configure a large amount of I/O module, thus bring testing cost Increase, test the problems such as wiring workload increases, efficiency reduces.Using automatic test device extend function after, overcome with The reduction of upper disadvantage, raising and cost for testing efficiency has remarkable result.
Detailed description of the invention
Attached drawing described herein is used to provide to further understand the embodiment of the present invention, constitutes one of the application Point, do not constitute the restriction to the embodiment of the present invention.In the accompanying drawings:
Fig. 1 is structural schematic diagram of the invention.
Fig. 2 is specific link schematic diagram of the invention.
Specific embodiment
To make the objectives, technical solutions, and advantages of the present invention clearer, the present invention is made below with reference to embodiment Further to be described in detail, exemplary embodiment of the invention and its explanation for explaining only the invention, are not intended as to this The restriction of invention.
Embodiment 1
It is as shown in Figure 1 and Figure 2:
A kind of arbitrarily extensible DCS system automatic test device, including host computer, test output input cabinet;
Test output input cabinet includes that master controller and master controller establish the I/O module of data transmission link, DCS Network communication module, host computer docking network communication module are docked, wherein host computer docking network communication module is built with host computer Vertical network communication, DCS docking network communication module are used to establish network communication with the network communication module of DCS system;I/O module It is connect for the I/O module with DCS system;
Host computer is used to obtain test case post analysis and obtains test signal and anticipatory data and pass through test signal Position machine docking network communication module is distributed to master controller;
Master controller is divided into test I/O module transfer signal and test network transmission signal for that will test signal, And test is transferred to the I/O module of DCS system with I/O module transfer signal by the hardwire of I/O module, and test is used Network transmission signal is transferred to the network communication module of DCS system by the optical fiber that DCS docks network communication module, by above-mentioned After transmission test signal, the master controller of DCS system is made to pass through its I/O module and network communication module acquisition test letter respectively Number, the master controller of DCS system modifies to its IO variable according to test signal;
Master controller is also used to pass through test output input respectively after DCS system makes feedback, when forming state parameter It is returned after the I/O module of cabinet itself, the state parameter of DCS docking network communication module acquisition DCS system to host computer;
Host computer generates test report after being also used to be compared according to state parameter with anticipatory data.
Design principle of the invention are as follows:
Due to more than DCS system I O point quantity (a large amount of signal (signal up to ten thousand) test requirements documents, existing test device it is defeated Outgoing interface and input interface are few, cannot achieve all standing requirement to test point, use to solve this method prior art 2 kinds of mentalities of designing, the first is carried out using the method for increasing interface module, in the way of mould group, is needing more tests When point, increase interface module, this method it is at high cost, need to be arranged according to different test cases different interface connections, therefore survey Try inefficiency.Second of test method is whole network data test method, i.e., network interface is arranged in test device, passes through Network interface issues data and passback feedback data is communicated with DCS system, and there are a deadly defects for this method, i.e., can only carry out The verification test of DCS system logic, the transmission of data are all to be directly over network module to enter in the master controller of DCS, are not had Have and communicated by I/O mouthfuls, therefore complete test in the case where I/O port transmission can not be formed in, lacks scientific feasibility.
In order to guarantee that test is scientific and solve the problems, such as that interface deficiency, the present invention are provided with main control in test device Device, and the data-interface for docking with DCS is provided with 2 kinds of designs coexisted, one is conventional I/O port transmission form, One is the transmission forms of network interface, not simple to rely on any transmission form in test, but two kinds transmit Form carries out simultaneously, needs interface excessively in the current unappeasable situation of test device I/O interface in test case, from Network interface configures test data, so that the data transmission that cannot provide interface provides network interface and completes, core is in master Under the control of controller, the transmission of network data and I/O data is synchronously completed, wherein extension is realized pair using network communication The modification and reading of IO variable, reduce the dependence to test device IO physical points in DCS system.The device can reduce wiring Workload reduces cost, improves testing efficiency.
Embodiment 2
It is as shown in Figure 1 and Figure 2:
Preferably, on the basis of embodiment 1,
The I/O module of the test output input cabinet includes analog output module, switching value output module, analog quantity Input module, switching input module.
The analog output module, switching value output module, Analog input mModule, switching input module selection are same Walk module of the time no more than 5ms.
Embodiment 3
It is as shown in Figure 1 and Figure 2:
Preferably, on the basis of embodiment 1,
Since the form that network transmission and I/O are transmitted is different, there are problems that time delay, and DCS system is needed same One moment provided corresponding feedback according to test signal, if there is time delay, will lead to feedback signal disorder, leads to test errors And failure, in order to solve this problem, present applicant proposes at least following two solution, the core concepts of following two schemes It is the time delay by calculating two kinds of accesses, calculation delay is poor, delay inequality counted when controlling signal and sending, so that The signal for reaching DCS system can be solved the above problems with this in synchronization.
Preferably, the first solves delay problem are as follows:
Master controller is T1 at the time of sending and testing with I/O module transfer signal to I/O module, and master controller is being sent Test is T2 at the time of docking network communication module to DCS with network transmission signal, before wherein master controller setting T2 is T1 At the time of, the difference between T2 and T1 is to ensure that DCS system receives test I/O module transfer signal and test in synchronization Calculating acquisition is carried out with the actual conditions of network transmission signal.
Mode at the time of master controller is arranged before T2 is T1 is that T2, T1 is arranged using programmed method.
This method is realized due to the method for software programming, is first tested master controller and is sent test I/O module biography After defeated signal, DCS system receives the time delay that I/O module transfer signal is used in test, and then re-test master controller sends test After network transmission signal, DCS system receives the time delay of test network transmission signal, and the difference of 2 time delays is calculated Out, it to go the difference of control T2, T1, thus can solve delay problem, guarantee that DCS can be synchronized and receive 2 accesses and send Signal.
Preferably, second of solution delay problem are as follows:
The I/O module of test output input cabinet is T11 at the time of sending and testing I/O module transfer signal, test The DCS docking network communication module of output input cabinet is T12 at the time of sending test network transmission signal, wherein T12 At the time of for before T11, the difference between T12 and T11 is passed with ensureing that DCS system receives test I/O module in synchronization The actual conditions of defeated signal and test network transmission signal carry out calculating acquisition.
Mode at the time of setting before T12 is T11 are as follows: obtain test in the I/O module that test exports input cabinet and use Delay circuit is set before I/O module transfer signal or after obtaining test I/O module transfer signal.
The core of the method for the solution time delay is that the delay circuit of hardware is arranged, controls signal by delay circuit and send Moment, likewise, DCS system receives test I/ after it first tests master controller transmission test I/O module transfer signal O module transmits the time delay of signal, and after then re-test master controller sends test network transmission signal, DCS system is received The test time delay of network transmission signal, the difference of 2 time delays is calculated, to go the difference of control T12, T11, in this way Delay problem can be solved, guarantees that DCS can be synchronized and receives the signal that 2 accesses are sent.
In principal it is also possible at the time of resolving test signal by master controller in setting DCS system, thus delay of control Problem, but as testing experiment, do not allow generally to be configured equipment under test, therefore this method is as worst alternative approach.
Embodiment 4
It is as shown in Figure 1 and Figure 2:
Preferably, on the basis of embodiment 1,
It preferably, further include from extension cabinet when test interface is also insufficient;The test output inputs cabinet and further includes From expansion card, test output input cabinet master controller is by establishing communication link, main control from expansion card with from extension cabinet Test signal is also divided into test with from expansion I/O module transfer signal by device, is provided with main expansion card, I/O out of extension cabinet Module, test are extended in cabinet with from expansion I/O module transfer signal by being transferred to from the main expansion card in extension cabinet I/O module, then by the I/O module transfer in extension cabinet to DCS system.It is arranged from the purpose of extension cabinet and setting and tests The principle of the I/O module of output input cabinet is consistent, and increases I/O interface quantity, and purpose is all simulation SOP/BUP/ LEVEL0 layers of external system device, it is required that being configured with analog signals and digital quantity signal, analog spot sensor, core instrument Table signal, safety hand operation panel and Safety actuator and acquisition shutdown breaker signal.
Embodiment 5
It is as shown in Figure 1 and Figure 2:
Preferably, when being tested using only test output input cabinet:
A kind of test method based on arbitrarily extensible DCS system automatic test device, comprising the following steps:
After the external testing use-case obtained by host computer, test case is resolved into survey using test case processing software Trial signal and anticipatory data;
Signal, which will be tested, by master controller resolves to test I/O module transfer signal and survey according to transmission path difference Network transmission signal on probation;
The I/ that DCS system is sent to I/O module transfer signal will be tested by the I/O module that test exports input cabinet O module,
Network communication module is docked by the DCS that test exports input cabinet to be sent to test with network transmission signal The network communication module of DCS system;
DCS system repairs its IO variable with network transmission signal according to test I/O module transfer signal and test Change;
The I/O module of input cabinet is exported by test, DCS docks network communication module acquisition DCS system and IO is become State parameter out is fed back after amount variation;
Embodiment 6
It is as shown in Figure 1 and Figure 2:
By exporting test report with after anticipatory data comparison after host computer back production state parameter.
When using test output input cabinet and from extension cabinet:
A kind of test method based on arbitrarily extensible DCS system automatic test device, comprising the following steps:
After the external testing use-case obtained by host computer, test case is resolved into survey using test case processing software Trial signal and anticipatory data;
Signal, which will be tested, by master controller resolves to test I/O module transfer signal and survey according to transmission path difference On probation network transmission signal, test are with from expansion I/O module transfer signal;
The I/ that DCS system is sent to I/O module transfer signal will be tested by the I/O module that test exports input cabinet O module,
Network communication module is docked by the DCS that test exports input cabinet to be sent to test with network transmission signal The network communication module of DCS system;
It will be tested by the slave expansion card that test exports input cabinet and be sent to from expansion I/O module transfer signal from expansion Cabinet is opened up, then will be tested with the I/O for being sent to DCS system from expansion I/O module transfer signal by the I/O module from extension cabinet Module;
DCS system is according to test I/O module transfer signal and test network transmission signal, test with from expansion I/O Module transfer signal modifies to its IO variable;
The input I/O module of cabinet is exported by test, DCS docks network communication module, from the I/O module of extension cabinet DCS system is obtained for feeding back state parameter out after IO variable change;
By exporting test report with after anticipatory data comparison after host computer back production state parameter.
In above-described embodiment, the cabinet 1 in figure is test output input cabinet, and cabinet 1 is from extension cabinet.
Further,
In the above-described embodiments:
Host computer: using standard industry computer, and control centre of the host computer as whole system has human-computer interaction, Test software is write, the functions such as test equipment configuration, test equipment self diagnosis, passes through the master control cartoon in Ethernet and cabinet 1 Letter realizes the interaction of real-time system and non real-time system;Login password can be arranged in host computer, and it is automatic to can be realized test data It records, automatically save, will not illegally be distorted;
Cabinet 1:SOP/BUP/LEVEL0 external system simulator, configured with master control card module (master controller), from expansion Open up module (from expansion card), communication module (DCS docks network communication module, host computer docks network communication module), analog quantity With On-off signal output module (I/O module), wherein the type of module and quantity can carry out flexible configuration according to actual needs. Analog spot sensor, Nuclear Instrument signal and acquisition shutdown breaker signal, and read gateway signal;As DCS system IO It when point quantity is more than the I O point number of test device, is communicated by master controller expanding communication module, so that tested DCS system IO variable in modification and reading system is realized in connection, to extend the quantity of test I O point to meet test request.
Cabinet 2:SOP/BUP/LEVEL0 external system simulator is configured with analog signals and digital quantity signal, can Spot sensor, Nuclear Instrument signal, safety hand operation panel and Safety actuator and acquisition shutdown breaker signal are simulated, Gateway signal can be read.
Cabinet 1 can be used alone configured with main control card and from expansion card, and optical fiber can also be used and connect use with cabinet 2, even It is controlled after connecing by 1 real time operating system.Cabinet 2 connect use with cabinet 1 using expansion card, and energy is independent after being inserted into main control card It uses.
In addition, special door lock is arranged in cabinet, electrical equipment has earth leakage protective and surge protection etc..Automatic test device mould Analog quantity signal, on-off model synchronization time are no more than 5ms, and signal settling time is no more than 1ms, and the time of signal sampling does not surpass Cross 1ms.
Above-described specific embodiment has carried out further the purpose of the present invention, technical scheme and beneficial effects It is described in detail, it should be understood that being not intended to limit the present invention the foregoing is merely a specific embodiment of the invention Protection scope, all within the spirits and principles of the present invention, any modification, equivalent substitution, improvement and etc. done should all include Within protection scope of the present invention.

Claims (10)

1. a kind of arbitrarily extensible DCS system automatic test device, which is characterized in that defeated including host computer, test output Enter cabinet;
Test output input cabinet includes master controller, with master controller establish the I/O module of data transmission link, DCS is docked Network communication module, host computer dock network communication module, and wherein host computer docking network communication module and host computer establish net Network communication, DCS docking network communication module are used to establish network communication with the network communication module of DCS system;I/O module is used for It is connect with the I/O module of DCS system;
Host computer is for obtaining test case post analysis acquisition test signal and anticipatory data and test signal being passed through host computer Docking network communication module is distributed to master controller;
Master controller is divided into test I/O module transfer signal and test network transmission signal for that will test signal, and will Test is transferred to the I/O module of DCS system with I/O module transfer signal by the hardwire of I/O module, and by test network Transmission signal is transferred to the network communication module of DCS system by the optical fiber that DCS docks network communication module, passes through above-mentioned transmission After test signal, make the master controller of DCS system pass through respectively its I/O module and network communication module obtain test signal, The master controller of DCS system modifies to its IO variable according to test signal;
Master controller is also used to pass through test output input cabinet respectively after DCS system makes feedback, when forming state parameter It is returned after the I/O module of itself, the state parameter of DCS docking network communication module acquisition DCS system to host computer;
Host computer generates test report after being also used to be compared according to state parameter with anticipatory data.
2. the arbitrarily extensible DCS system automatic test device of one kind according to claim 1, which is characterized in that institute State test output input cabinet I/O module include analog output module, switching value output module, Analog input mModule, Switching input module.
3. the arbitrarily extensible DCS system automatic test device of one kind according to claim 2, which is characterized in that institute Stating analog output module, switching value output module, Analog input mModule, switching input module selects do not surpass synchronization time Cross the module of 5ms.
4. the arbitrarily extensible DCS system automatic test device of one kind according to claim 1, which is characterized in that main Controller is T1 at the time of sending and testing with I/O module transfer signal to I/O module, and master controller is sending test network For T2 at the time of transmitting a signal to DCS docking network communication module, at the time of before wherein master controller setting T2 is T1, T2 with Difference between T1 is to ensure that DCS system receives test with I/O module transfer signal and test network transmission in synchronization The actual conditions of signal carry out calculating acquisition.
5. the arbitrarily extensible DCS system automatic test device of one kind according to claim 4, which is characterized in that main Mode at the time of controller is arranged before T2 is T1 is that T2, T1 is arranged using programmed method.
6. the arbitrarily extensible DCS system automatic test device of one kind according to claim 1, which is characterized in that survey The I/O module of examination output input cabinet is T11 at the time of sending and testing I/O module transfer signal, test output input machine The DCS docking network communication module of cabinet is T12 at the time of sending test network transmission signal, before wherein T12 is T11 At the moment, the difference between T12 and T11 is to ensure that DCS system receives test I/O module transfer signal and test in synchronization Calculating acquisition is carried out with the actual conditions of network transmission signal.
7. the arbitrarily extensible DCS system automatic test device of one kind according to claim 6, which is characterized in that set Mode at the time of setting before T12 is T11 are as follows: obtain test I/O module transfer in the I/O module that test exports input cabinet Delay circuit is set before signal or after obtaining test I/O module transfer signal.
8. the arbitrarily extensible DCS system automatic test device of one kind according to any one of claims 1-7, It is characterized in that, further includes from extension cabinet;The test output input cabinet further includes from expansion card, test output input cabinet Master controller by establishing communication link from expansion card with from extension cabinet, master controller will also test signal be divided into test with from Expansion I/O module transfer signal, is provided with main expansion card, I/O module out of extension cabinet, and test is passed with from expansion I/O module Defeated signal by from extension cabinet in main expansion card be transferred to extension cabinet in I/O module, then by extension cabinet in I/O module transfer is to DCS system.
9. the test method based on a kind of arbitrarily extensible DCS system automatic test device, which is characterized in that including following Step:
After the external testing use-case obtained by host computer, test case is resolved into test letter using test case processing software Number and anticipatory data;
Test signal is resolved to according to transmission path difference by master controller and is tested with I/O module transfer signal and test use Network transmission signal;
The I/O mould that DCS system is sent to I/O module transfer signal will be tested by the I/O module that test exports input cabinet Block,
Network communication module is docked by the DCS that test exports input cabinet, and test is sent to DCS system with network transmission signal The network communication module of system;
DCS system modifies to its IO variable with network transmission signal according to test I/O module transfer signal and test;
The I/O module of input cabinet is exported by test, DCS docks network communication module acquisition DCS system and IO variable is become State parameter out is fed back after change;
By exporting test report with after anticipatory data comparison after host computer back production state parameter.
10. the test method based on a kind of arbitrarily extensible DCS system automatic test device, which is characterized in that including with Lower step:
After the external testing use-case obtained by host computer, test case is resolved into test letter using test case processing software Number and anticipatory data;
Test signal is resolved to according to transmission path difference by master controller and is tested with I/O module transfer signal and test use Network transmission signal, test are with from expansion I/O module transfer signal;
The I/O mould that DCS system is sent to I/O module transfer signal will be tested by the I/O module that test exports input cabinet Block,
Network communication module is docked by the DCS that test exports input cabinet, and test is sent to DCS system with network transmission signal The network communication module of system;
It will be tested by the slave expansion card that test exports input cabinet and be sent to from expansion I/O module transfer signal from striking machine Cabinet, then the I/O mould that DCS system is sent to from expansion I/O module transfer signal will be tested by the I/O module from extension cabinet Block;
DCS system is according to test I/O module transfer signal and test network transmission signal, test with from expansion I/O module Transmission signal modifies to its IO variable;
The I/O module of input cabinet is exported by test, DCS docks network communication module, obtains from the I/O module of extension cabinet DCS system is for feeding back state parameter out after IO variable change;
By exporting test report with after anticipatory data comparison after host computer back production state parameter.
CN201910743717.8A 2019-08-13 2019-08-13 A kind of arbitrarily extensible DCS system automatic test device and test method Pending CN110377010A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910743717.8A CN110377010A (en) 2019-08-13 2019-08-13 A kind of arbitrarily extensible DCS system automatic test device and test method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910743717.8A CN110377010A (en) 2019-08-13 2019-08-13 A kind of arbitrarily extensible DCS system automatic test device and test method

Publications (1)

Publication Number Publication Date
CN110377010A true CN110377010A (en) 2019-10-25

Family

ID=68259015

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910743717.8A Pending CN110377010A (en) 2019-08-13 2019-08-13 A kind of arbitrarily extensible DCS system automatic test device and test method

Country Status (1)

Country Link
CN (1) CN110377010A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111131477A (en) * 2019-12-28 2020-05-08 杭州和利时自动化有限公司 Data processing method, device and equipment
CN113467527A (en) * 2021-06-28 2021-10-01 华润电力湖南有限公司 Executing mechanism linkage method and device, DCS (distributed control System) and storage medium

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN205788161U (en) * 2016-06-13 2016-12-07 上海科梁信息工程股份有限公司 The test system of communication interface
CN106527406A (en) * 2016-12-20 2017-03-22 中核控制系统工程有限公司 Security-level DCS product automated testing device
WO2017115162A1 (en) * 2015-12-31 2017-07-06 Abb Schweiz Ag Method and system for testing distributed control systems of industrial plants
CN107544910A (en) * 2017-10-23 2018-01-05 南京大全电气研究院有限公司 A kind of intelligent distribution transformer terminals automatization test system and method based on LUA scripts
CN108181890A (en) * 2017-12-12 2018-06-19 中核控制系统工程有限公司 DCS automatic test devices based on virtual instrument
CN108958225A (en) * 2018-07-27 2018-12-07 中国核动力研究设计院 Npp safety grade DCS platform intergration test device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017115162A1 (en) * 2015-12-31 2017-07-06 Abb Schweiz Ag Method and system for testing distributed control systems of industrial plants
CN205788161U (en) * 2016-06-13 2016-12-07 上海科梁信息工程股份有限公司 The test system of communication interface
CN106527406A (en) * 2016-12-20 2017-03-22 中核控制系统工程有限公司 Security-level DCS product automated testing device
CN107544910A (en) * 2017-10-23 2018-01-05 南京大全电气研究院有限公司 A kind of intelligent distribution transformer terminals automatization test system and method based on LUA scripts
CN108181890A (en) * 2017-12-12 2018-06-19 中核控制系统工程有限公司 DCS automatic test devices based on virtual instrument
CN108958225A (en) * 2018-07-27 2018-12-07 中国核动力研究设计院 Npp safety grade DCS platform intergration test device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111131477A (en) * 2019-12-28 2020-05-08 杭州和利时自动化有限公司 Data processing method, device and equipment
CN111131477B (en) * 2019-12-28 2022-01-11 杭州和利时自动化有限公司 Data processing method, device and equipment
CN113467527A (en) * 2021-06-28 2021-10-01 华润电力湖南有限公司 Executing mechanism linkage method and device, DCS (distributed control System) and storage medium

Similar Documents

Publication Publication Date Title
CN103699112B (en) Based on avionics Autonomous test Authentication devices and the verification method thereof of I/O signal fault simulation
CN103439612B (en) Based on the intelligent substation Auto-Test System of SCD
CN104635669B (en) A kind of I&C system verification method
CN104407279A (en) Code type data, apparatus and test method for automatically testing chip MDIO bus protocol
CN110377010A (en) A kind of arbitrarily extensible DCS system automatic test device and test method
CN106776188A (en) Bus failure injected system based on DSP and FPGA
CN109193945A (en) A kind of method that intelligent substation remote action data configuration automated closed-loop is checked
CN101930314A (en) Touch control system in order to the control contact panel
CN103676661B (en) Multifunction emulation verifies system and its emulation verification method
CN202339718U (en) Extendible nuclear power DCS automatic testing device
CN110196391A (en) Digital circuit test device and method based on FPGA and DSP architecture
CN106406266A (en) Method used for simulating device controlled by nuclear power plant DCS system
CN105656204A (en) Intelligent substation remote-signaling closed-loop test method
CN101630158B (en) Industrial control system and serial communication method thereof
CN208796101U (en) Automobile audio entertainment systems automaticdiagnosis test macro
CN106844127B (en) A kind of highly reliable modular testing emulation platform
CN103576667A (en) Main control panel test method, device and system
CN109164329A (en) A kind of semiconductor memory product high/low temperature ageing testing method
CN105049311A (en) Two-bus communication method and system
CN103580971B (en) MVB countermeasure set
CN104569697A (en) Power supply interface detection method for minisatellite comprehensive test
CN209264906U (en) CVC-200T hardware intelligent test system
CN108072855A (en) A kind of test device and test system
CN209327868U (en) The test macro of Vehicle Controller
CN109324597B (en) Engineering adaptability test method for second-generation pressurized water reactor safety-level DCS of nuclear power station

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
TA01 Transfer of patent application right

Effective date of registration: 20201218

Address after: No.3, Hongda South Road, Beijing Economic and Technological Development Zone, Daxing District, Beijing

Applicant after: CHINA NUCLEAR CONTROL SYSTEM ENGINEERING Co.,Ltd.

Address before: 610000, No. three, 28 south section of Ring Road, Chengdu, Sichuan

Applicant before: NUCLEAR POWER INSTITUTE OF CHINA

TA01 Transfer of patent application right
RJ01 Rejection of invention patent application after publication

Application publication date: 20191025

RJ01 Rejection of invention patent application after publication