CN105373013A - Thermal power set DCS analog quantity control circuit simulation test system and method - Google Patents
Thermal power set DCS analog quantity control circuit simulation test system and method Download PDFInfo
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- CN105373013A CN105373013A CN201510893948.9A CN201510893948A CN105373013A CN 105373013 A CN105373013 A CN 105373013A CN 201510893948 A CN201510893948 A CN 201510893948A CN 105373013 A CN105373013 A CN 105373013A
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- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B17/00—Systems involving the use of models or simulators of said systems
- G05B17/02—Systems involving the use of models or simulators of said systems electric
Abstract
The invention relates to a thermal power set DCS analog quantity control circuit simulation test system and method. The system comprises a thermal power set excitation type simulation platform and a test DCS, wherein the thermal power set excitation type simulation platform comprises a simulation DCS and a simulation model which are mutually connected, and the test DCS and the simulation model employ trunk connection; and the test DCS sends a trunk control instruction to the simulation model, and after operation of the simulation model, simultaneously sends control parameters to the test DCS and the simulation DCS so as to realize a control closed loop. Compared to the prior art, the system and method provided by the in invention have the following advantages: a dynamic simulation test of an analog quantity loop is realized, the problems existing in logic configuration are discovered and solved timely, the implementation quality of control function configuration is improved, favorable conditions are created for control of actual system debugging and smooth application, and the like.
Description
Technical field
The present invention relates to the automation field of thermal power generation unit, especially relate to a kind of fired power generating unit DCS system Analog control loop simulation test macro and method.
Background technology
In fired power generating unit DCS system, Analog control loop mainly realizes the automatic regulation and control function of unit operation parameter, the steam temperature on upper strata, vapour pressure, the isoparametric control of generation load is controlled to, the controlling functions such as fast cutback when also comprising subsidiary engine device fails in addition from the water level of bottom, flow, rotating speed.Whether these controlling functions correctly can realize often having influence on the normal operation of safety of unit, so should carry out effective functional test before DCS system is dispatched from the factory.But at this moment DCS system not yet establishes the link with practical object, there is no formation control closed loop, more difficultly carry out effective functional test.At present two kinds of methods are mainly contained for analog quantity loop-around test, one is in DCS system, adopt configuration instrument to build the test of control object realistic model practical function (see patent of invention " method of fired power generating unit dcs control object simulation modeling ", the patent No.: ZL201010507102.4), another kind DCS system is fetched with the Building of Simulation Model chain of engineering unit to carry out functional test.The equal Shortcomings part of these two kinds of methods, first method due to object model complexity various, and the algorithm that configuration instrument provides is limited, can only realize the simplification emulation of control object and rough simulation, affect functional test effect.In second method, engineering unit not necessarily has realistic model, even if build realistic model also often lag behind DCS system, and all link (thousands of somes signals) with Building of Simulation Model and also waste time and energy, emulation testing cannot be completed before DCS field adjustable.
Summary of the invention
Object of the present invention be exactly in order to overcome above-mentioned prior art exist defect and a kind of fired power generating unit DCS system Analog control loop simulation test macro and method are provided.
Object of the present invention can be achieved through the following technical solutions:
A kind of fired power generating unit DCS system Analog control loop simulation test macro, it is characterized in that, comprise fired power generating unit Exciting-simulator system emulation platform and test DCS system, described fired power generating unit Exciting-simulator system emulation platform comprises interconnective emulation DCS system and realistic model, adopts trunk to link between described test DCS system and realistic model;
Trunk steering order is sent to realistic model by described test DCS system, by controling parameters to be sent back to after realistic model computing test DCS system and emulation DCS system simultaneously, realizes Control loop.
Also comprise for testing the Artificial switch that switches between DCS system and emulation DCS system, this Artificial switch respectively with test DCS system, emulate DCS system and realistic model is connected;
After described Artificial switch is switched to test DCS system, described realistic model no longer receives the trunk steering order that emulation DCS system sends, transfer the trunk steering order receiving test DCS system and send to, the controling parameters that described realistic model calculates then is sent to test DCS system and emulation DCS system simultaneously.
Described test DCS system is the DCS system that range is identical or range is different with emulation DCS system.
When described test DCS system and emulation DCS system are the different DCS system of range, between described test DCS system and realistic model, be provided with range swithching unit.
The trunk steering order being sent to realistic model by test DCS system comprises load instruction, steam turbine pitch opening degree instruction, feeder rotary speed instruction, speed of feedwater instruction, the instruction of pressure fan baffle opening, the instruction of induced draft fan baffle opening, the instruction of primary air fan baffle opening, the hot and cold throttle opening instruction of coal pulverizer, condensate water pitch opening degree instruction, heater condensate pitch opening degree instruction and condenser water replenishing pitch opening degree instruction.
Described test DCS system is with setting up outside trunk link between realistic model, other signals still maintain the link between original realistic model and emulation DCS system, and are run by realistic model by emulation DCS system.
A kind of fired power generating unit DCS system Analog control loop simulation method of testing, is characterized in that, comprise the following steps:
1) set up test DCS system to link with the trunk of realistic model;
2) Dynamic simulation platform, makes realistic model be between the loading zone of setting;
3) trunk link signal is switched to test DCS system, described realistic model starts to receive the trunk steering order signal tested DCS system and send;
4) Obj State after realistic model computing and operational factor send test DCS system back to, formation control closed loop;
5) under Control loop, emulation testing is carried out to Analog control loop, find and eliminate Problems existing in steering logic, tentatively controling parameters is set, improving configuration work quality.
Compared with prior art, present invention achieves a kind of brand-new analog quantity loop simulation method of testing, by general fired power generating unit Exciting-simulator system emulation platform, set up the trunk link between DCS system and Universal Simulation Model, model accuracy is much higher than the model built with DCS configuration instrument, adopt the mode of trunk link can formation control closed loop quickly and easily, realize the dynamic simulation test in analog quantity loop, find early and solve Problems existing in Logical Configuration, promote the implementation quality of controlling functions configuration, for the actual debugging of control system creates favorable conditions with coming into operation smoothly.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, be clearly and completely described the technical scheme in the embodiment of the present invention, obviously, described embodiment is a part of embodiment of the present invention, instead of whole embodiment.Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain under the prerequisite not making creative work, all should belong to the scope of protection of the invention.
The key of Validity Test is carried out to Analog control loop and the most important condition to set up the closed loop of control loop, namely steering order will issue certain control object, after the state change of control object, operational factor is changed, analog quantity loop according to this Parameters variation adjustment steering order, forms closed loop again.If there is no this closed loop, only effectively can not find to control Problems existing in configuration by static logical check, increase the real dynamic risk of unit equipment.Aforementioned first method can only realize the rough emulation of control object, and it can only be a kind of approximate simulation that Obj State changes the operational factor change caused, and can affect test effect.In addition, for different DCS system, need again to build simplification realistic model according to this DCS instrument of actual set, also need to debug simplified model.Can realize the accurate simulation of control object by second method, but realistic model construction often lags behind DCS system, and foundation all links time and effort consuming.
Consider that newly-built fired power generating unit is all generally adopt super (super-) critical technology, engineering unit can be represented completely by General Simulation Platform, and adopt a kind of brand-new trunk link method, main steering order is mail to emulation platform and realistic model by testing DCS system, by relevant operational factor being returned to test DCS system after model calculation, realize Control loop.Adopt in this way, the simulation accuracy of control object will be much higher than the simulation object that DCS instrument is built, in addition owing to adopting trunk on-link mode (OLM) can realize very easily testing the link between DCS system and realistic model, for the test of analog quantity loop dynamic brings convenience.
As shown in Figure 1, a kind of fired power generating unit DCS system Analog control loop simulation test macro, comprise fired power generating unit Exciting-simulator system emulation platform 1 and test DCS system 2, described fired power generating unit Exciting-simulator system emulation platform 1 comprises interconnective emulation DCS system 11 and realistic model 12.
The present invention also comprises for testing the Artificial switch 3 that switches between DCS system and emulation DCS system, this Artificial switch 3 respectively with test DCS system 2, emulate DCS system 11 and realistic model 12 is connected.
Exciting-simulator system emulation platform comprises emulation DCS system and realistic model two parts, except test DCS system is with setting up except trunk link between realistic model, other signals still maintain the link between original realistic model and emulation DCS, and by emulation DCS, model running is got up, solve the initialization matter of realistic model.In addition, the capacitance grade of test unit can be not identical with Exciting-simulator system emulation platform, as long as now carry out suitable range swithching to trunk link signal.
The step of Analog control loop being carried out to emulation testing is as follows:
Set up the trunk link of test DCS system and realistic model, carry out suitable range swithching if desired;
Dynamic simulation platform, makes emulation unit be between certain loading zone;
Trunk link signal is switched to test DCS system, and realistic model starts the trunk command signal that acceptance test DCS system sends;
Obj State after model calculation and operational factor send test DCS system back to, formation control closed loop;
Under Control loop, emulation testing is carried out to Analog control loop, find and eliminate Problems existing in steering logic, tentatively controling parameters is set, improving configuration work quality.
For a certain newly-built 600MW ultra supercritical coal-fired unit, DCS adopts the raw Ovation system of Ai Mo, after completing DCS controlling functions and monitored picture configuration, dynamic test is carried out to DCS system Analog control loop, check whether correct controlling functions and AM/BAM link, to find early and to deal with problems, shorten actual debug time.
By the 1000MW ultra supercritical general fired power generating unit Exciting-simulator system emulation platform built, set up the data exchange channels between realistic model and test DCS system, adopt the mode of trunk link, the steering order being sent to realistic model by test DCS system mainly contains load instruction, steam turbine pitch opening degree instruction, feeder rotary speed instruction, speed of feedwater instruction, the instruction of pressure fan baffle opening, the instruction of induced draft fan baffle opening, the instruction of primary air fan baffle opening, coal pulverizer is cold, hot air disperser opening degree instruction, condensate water pitch opening degree instruction, heater condensate pitch opening degree instruction, the major instruction signals such as condenser water replenishing pitch opening degree instruction.
In addition, be provided with Artificial switch, after switch drops into, realistic model no longer accepts the trunk instruction that emulation DCS sends, but transfer the instruction that acceptance test DCS sends to, the controling parameters that model calculates then is sent to test DCS and emulation DCS system simultaneously, and analog quantity loop simulation test macro is shown in schematic diagram 1.Like this after steering order changes in test DCS, can change through realistic model operation control parameter and be back to test DCS system, thus realizing the closed loop in Analog control loop, artificial debugging can be carried out to Analog control loop.
For hearth vacuum control loop, after dropping into Artificial switch, model starts the opening degree instruction of induced draft fan stator blade baffle plate in acceptance test DCS, and calculating combustion chamber draft through realistic model after aperture change can change, this parameter can pass test DCS system back, thus formation control closed loop.Other Analog control loops process in a similar way, thus effectively can carry out the artificial debugging of main analog amount control loop, comprise the control loops such as unit cooperative control, RB fast cutback.
Because emulation platform is based on 1000MW extra-supercritical unit, and the engineering unit of actual DCS system is 6000MW unit, therefore will carry out suitable range conversion when instruction and parameter transmit.In addition when carrying out emulation mode and switching, the switching also will carried out between test DCS system and emulation DCS system is followed the tracks of, and realizes no-harass switch, guarantees that test DCS and emulation platform normally work.
The above; be only the specific embodiment of the present invention; but protection scope of the present invention is not limited thereto; anyly be familiar with those skilled in the art in the technical scope that the present invention discloses; can expect amendment or the replacement of various equivalence easily, these amendments or replacement all should be encompassed within protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with the protection domain of claim.
Claims (7)
1. a fired power generating unit DCS system Analog control loop simulation test macro, it is characterized in that, comprise fired power generating unit Exciting-simulator system emulation platform and test DCS system, described fired power generating unit Exciting-simulator system emulation platform comprises interconnective emulation DCS system and realistic model, adopts trunk to link between described test DCS system and realistic model;
Trunk steering order is sent to realistic model by described test DCS system, by controling parameters to be sent back to after realistic model computing test DCS system and emulation DCS system simultaneously, realizes Control loop.
2. a kind of fired power generating unit DCS system Analog control loop simulation test macro according to claim 1, it is characterized in that, also comprise for testing the Artificial switch that switches between DCS system and emulation DCS system, this Artificial switch respectively with test DCS system, emulate DCS system and realistic model is connected;
After described Artificial switch is switched to test DCS system, described realistic model no longer receives the trunk steering order that emulation DCS system sends, transfer the trunk steering order receiving test DCS system and send to, the controling parameters that described realistic model calculates then is sent to test DCS system and emulation DCS system simultaneously.
3. a kind of fired power generating unit DCS system Analog control loop simulation test macro according to claim 1, is characterized in that, described test DCS system is the DCS system that range is identical or range is different with emulation DCS system.
4. a kind of fired power generating unit DCS system Analog control loop simulation test macro according to claim 3, it is characterized in that, when described test DCS system and emulation DCS system are the different DCS system of range, between described test DCS system and realistic model, be provided with range swithching unit.
5. a kind of fired power generating unit DCS system Analog control loop simulation test macro according to claim 1, it is characterized in that, the trunk steering order being sent to realistic model by test DCS system comprises load instruction, steam turbine pitch opening degree instruction, feeder rotary speed instruction, speed of feedwater instruction, the instruction of pressure fan baffle opening, the instruction of induced draft fan baffle opening, the instruction of primary air fan baffle opening, the hot and cold throttle opening instruction of coal pulverizer, condensate water pitch opening degree instruction, heater condensate pitch opening degree instruction and condenser water replenishing pitch opening degree instruction.
6. a kind of fired power generating unit DCS system Analog control loop simulation test macro according to claim 1, it is characterized in that, described test DCS system is with setting up outside trunk link between realistic model, other signals still maintain the link between original realistic model and emulation DCS system, and are run by realistic model by emulation DCS system.
7. implement the claims the fired power generating unit DCS system Analog control loop simulation method of testing described in 1, it is characterized in that, comprise the following steps:
1) set up test DCS system to link with the trunk of realistic model;
2) Dynamic simulation platform, makes realistic model be between the loading zone of setting;
3) trunk link signal is switched to test DCS system, described realistic model starts to receive the trunk steering order signal tested DCS system and send;
4) Obj State after realistic model computing and operational factor send test DCS system back to, formation control closed loop;
5) under Control loop, emulation testing is carried out to Analog control loop, find and eliminate Problems existing in steering logic, tentatively controling parameters is set, improving configuration work quality.
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| CN108536111A (en) * | 2018-07-12 | 2018-09-14 | 华能烟台发电有限公司 | Control unit in thermal control DCS is avoided to instruct the processing method of zero after restarting |
| CN110768871A (en) * | 2019-10-29 | 2020-02-07 | 北京广利核系统工程有限公司 | Test method and system for automatically counting data transmission correctness of DCS (distributed control system) |
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