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Research ArticleEffect Mechanism of Penstock on Stability and RegulationQuality of Turbine Regulating System
Wencheng Guo, Jiandong Yang, Jieping Chen, and Yi Teng
State Key Laboratory of Water Resources and Hydropower Engineering Science, Wuhan University, Wuhan 430072, China
Correspondence should be addressed to Wencheng Guo; [email protected]
Received 17 July 2014; Accepted 20 October 2014; Published 19 November 2014
Academic Editor: Hongbin Zhang
Copyright 2014 Wencheng Guo et al.This is an open access article distributed under the Creative Commons Attribution License,which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
This paper studies the effect mechanism of water inertia and head loss of penstock on stability and regulation quality of turbineregulating system with surge tank or not and proposes the construction method of equivalent model of regulating system. Firstly,the complete linear mathematical model of regulating system is established. Then, the free oscillation equation and time responseof the frequency that describe stability and regulation quality, respectively, are obtained. Finally, the effects of penstock are analysedby using stability region and response curves. The results indicate that the stability and regulation quality of system without surgetank are determined by time response of frequency which only depends on water hammer wave in penstock, while, for system withsurge tank, the time response of frequency depending on water hammer wave in penstock and water-level fluctuation in surge tankjointly determines the stability and regulation quality. Water inertia of penstock mainly affects the stability and time response offrequency of system without surge tank as well as the stability and head wave of time response of frequency with surge tank. Headloss of penstock mainly affects the stability and tail wave of time response of frequency with surge tank.
1. Introduction
Turbine regulating system is the core component of load fre-quency control (LFC) of hydropower system. When hydro-electric power plant (HPP) operates under isolated modeor becomes isolated from the grid, the regulating systemshould maintain adequate stability margins as well as certainregulation quality. Stability and regulation quality are twosides which are the unity of opposites of regulating systemand are influenced by hydraulic, mechanical, and electricalfactors [1]. Pipeline network is the foundation of hydraulicfactors. As a key link of pipeline network, penstock hassignificant and unique effects on stability and regulationquality. Hence, a thorough and detailed understanding ofeffects of penstock is necessary for proper control of stabilityand regulation quality of turbine regulating system.
For the subject of stability and regulation quality, previousresearch centres upon governor. Many authors studied theworking performance of temporary droop type governor [25] and proportional-integral-derivative (PID) type governor[610]. The adjustment of governor parameters was also
researched [11]. As for penstock of HPP without surge tank,Ruud [12] investigated the instability of a hydraulic turbinewith a very long penstock;Murty andHariharan [13] analysedthe influence of water column elasticity on the stabilitylimits of hydroturbine generating unit with long penstockand proposed a modified water column compensator toenhance the stability regions and dynamic performance;Souza and Barbieri [14] discussed hydraulic transients inhydropower plants based on the nonlinearmodel of penstockand hydraulic turbine model; Sanathanan [15] proposed amethod for obtaining accurate low order model for hydraulicturbine penstock; Krivehenko et al. [16] studied some specialconditions of unit operation in hydropower plant with longpenstocks. If a HPP has surge tank, its penstock is usuallyneglected to simplify the mathematical model of turbineregulating system [17, 18].
It can be found from the above summary that the previousresearch on the effects of penstock on stability and regulationquality forms two major limitations. Firstly, the researchobject is mainly the HPP which has long penstock and doesnot have surge tank. However, the most important factors
Hindawi Publishing CorporationMathematical Problems in EngineeringVolume 2014, Article ID 349086, 13 pageshttp://dx.doi.org/10.1155/2014/349086
http://dx.doi.org/10.1155/2014/349086
2 Mathematical Problems in Engineering
Penstock
Draft tube
Generating unitReservoir
Qt Lt ft ht0 Twt
(a) Pipeline and power generating system (withoutsurge tank)
Z
Penstock
Headrace tunnel
Draft tube
Generating unitReservoir
Qt Lt ft ht0 Twt
Qy Ly fy hy0 Twy
Surge tank TF
(b) Pipeline and power generating system (with surge tank)
Headrace tunnelSurge tank Turbinegenerator
Gridload
Feedback element
Measurement element
Point elementAmplification elementCorrection element
Actuator
Turbine control system
+
Controlled system
Penstock
(c) Turbine regulating system
Figure 1: Turbine regulating system of isolated HPP with surge tank or not.
of penstock are water inertia and head loss. The effects ofthese two factors are not investigated and compared deeply.Secondly, there is only little research onHPPwith surge tank.It is well recognized that surge tank is indeed an importantmeasure of pressure reduction. Since the influence of water-level fluctuation in surge tank, the dynamic response ofregulating system with surge tank is significantly differentfrom the case without surge tank.
This paper aims to overcome the above two limitationsand thoroughly study the effect mechanism of water inertiaand head loss of penstock on stability and regulation qualityof turbine regulating system with surge tank or not. It isassumed that the system operates on an isolated load andthe water column is rigid. This paper is organized as follows.In Section 2, the complete linear mathematical model ofturbine regulating system that includes all subsystems (i.e.,headrace tunnel, surge tank, penstock, turbine, generator, andgovernor) is established, and the overall transfer functionsof systems without surge tank and with surge tank arederived from the complete mathematical model under stepload disturbance. In Sections 3 and 4, based on the freeoscillation equation and time response of the frequency ofsystem derived from overall transfer function, the effectsof water inertia and head loss of penstock on stability andregulation quality are analysed by using stability regionand response curves. In Section 5, the effect mechanism ofpenstock is epurated and summarized. Then according tothis effect mechanism, the improvement methods of stabilityand regulation quality and constructionmethod of equivalentmodel of regulating system are proposed.
2. Mathematical Model
Theturbine regulating systemof isolatedHPPwith surge tankor not is illustrated in Figure 1.
2.1. Basic Equations. The HPP without surge tank can beregarded as a special case of HPP with surge tank when thelength of headrace tunnel and the sectional area of surge tankare both 0. Hence, in this section, the complete mathematicalmodel of turbine regulating systemof isolatedHPPwith surgetank is first established, and then the model of that withoutsurge tank can be obtained as a special case.
2.1.1. Turbine Regulating System of Isolated HPP withSurge Tank
(1) Controlled System [19, 20]. Momentum equation of head-race tunnel:
=
+
20
0
. (1)
Continuity equation of surge tank:
=
. (2)
Momentum equation of penstock:
=
20
0
. (3)
Mathematical Problems in Engineering 3
1++
++
+
+
++
+
Kp
Ki/s
eqx
eqy
eqh
ey
Gs(s)
ex
eh
Mg(s)
eg
X(s)1/Tas
(a) Overall block diagram of turbine regulating system
+
++
Twts
2ht0/H0
Twys
2hy0/H0
TFs
Qt(s) H(s)
(b) Block diagram of pipeline system (with surgetank)
2ht0/H0
Qt(s)Twts
H(s)
(c) Block diagram of pipeline sys-tem (without surge tank)
Figure 2: Block diagram of turbine regulating system.
Moment equation and discharge equation of turbine:
=
+
+
,
=
+
+
.
(4)
First derivative differential equation of generator:
= (
+
) . (5)
(2) Turbine Control System [19, 20]. Equation of governor:
=
. (6)
The nomenclatures in (1)(6) are presented inAppendix A.
2.1.2. Turbine Regulating System of Isolated HPPwithout SurgeTank. Delete (1) and (2) and reformulate (3) to the followingform:
=
20
0
. (7)
Then (7), (4)(6) are the complete mathematical model ofturbine regulating system of isolatedHPPwithout surge tank.Note that this model (see (7), (4)(6)) can as well be obtainedfrom (1)(6) in the conditions of
= 0,
0= 0, and
= 0.
2.2. Overall Transfer Function. For the situation of loaddisturbance, the block diagram of turbine regulating system
is determined by the basic equations in Section 2.1 and shownin Figure 2, where
() = ()/
() is the transfer function
of pipeline system and can be derived from the Laplacetransforms of (1)(3) forHPPwith surge tank and (7) forHPPwithout surge tank. is complex variable.
According to Figures 2(a) and 2(b) and the Laplacetransforms of (1)(6), the following overall transfer functionof turbine regulating system of isolated HPP with surge tankis obtained:
() =
()
()
=
(03
+ 12
+ 2 +
3) /
05+
14+
23+
32+
4 +
5
,
(8)
where () and () are the Laplace transforms of load
disturbance
and time response of the frequency x,respectively, and the former is input signal and the lateris output signal. The expressions of coefficients in (8) arepresented in Appendix B.
By proceeding in a similar manner, the overall transferfunction of turbine regulating systemof isolatedHPPwithoutsurge tank is derived from Figures 2(a) and 2(c) and theLaplace transforms of (7), (4)(6) are as follows:
() =
()
()
=
(2 +
3) /
23+
32+
4 +
5
. (9)
Note that (9) can also be obtained from (8) by letting
= 0, 0
= 0, and = 0. The expressions of coefficients
in (9) are the special cases of those in (8) when ,
0, and
are both 0.
4 Mathematical Problems in Engineering
Instability region
Stability region
Stability boundary
Z
X
YKp/K
i(s
)
1/Kp
(a) Stability region in the plane of 1/and
/
x
X
Y
Z
t (s)
(b) Types of free oscillations corresponding to different regions
Figure 3: Stability region of turbine regulating system.
3. Effect of Penstock on Stability
Stability reflects the performance of free oscillation ofdynamic system that restores to a new equilibrium state afterinput disturbance vanishes. The free oscillation is dividedinto three types: damped oscillation, persistent oscillation,and divergent oscillation (shown in Figure 3(b)). On the basisof the definition of Lyapunov on stability [21], the first twotypes of oscillation are stable and the third one is unstable.However, the stable oscillation is only restricted to dampedoscillation in practical projects. This paper uses the latterdefinition.
3.1. Free Oscillation Equation and Stability Criterion. The sta-bility of regulating system is described by free oscillationequation and discriminated by stability criterion.
3.1.1. Free Oscillation Equation. The following third orderand fifth order linear homogeneous differential equationsobtained from (9) and (8) are the free oscillation equations ofturbine regulating system without surge tank and with surgetank, respectively:
2
3
3+
3
2
2+
4
+ 5= 0, (10)
0
5
5+
1
4
4+
2
3
3+
3
2
2+
4
+ 5= 0. (11)
3.1.2. Stability Criterion. By applying Routh-Hurwitz crite-rion [21], the stability criterions of turbine regulating systemrepresented by (10) and (11) are listed in Table 1.
When the coefficients in (10) satisfy the discriminants
1> 0 and
2> 0 simultaneously, the system without surge
tank is stable. Similarly, the system with surge tank is stablein the conditions of
1> 0,
2> 0, and
4> 0.
3.2. Stability Analysis. The stability region is the region thatsatisfies stability criterion of regulating system. In this paper,
Table 1: Stability Criterion.
System without surge tank(10) System with surge tank (11)
1=
> 0 ( = 2, 3, 4, 5)
1=
> 0 ( = 0, 1, 2, 3, 4, 5)
2=
34
25> 0
2=
12
03> 0
4= (
12
03)(
34
25)
(14
05)2
> 0
the abscissa and ordinate of coordinate plane are selected as1/
and
/
, respectively, and the stability region is illus-
trated in Figure 3(a).The corresponding relation between theregions in coordinate plane and the types of free oscillationsis shown in Figure 3(b).
This paper takes HPP A as example (basic informationis shown in Table 3 of Appendix C) to analyse the effectmechanism of water inertia and head loss of penstock onstability of turbine regulating system with surge tank ornot. In order to make sure that the results have universalsignificance and can be applied to any hydroelectric system,the variation ranges of
and
0are selected as 04 s (4 s is
the limit value of) and 010%
, respectively. In addition,
the sensitivity analysis of net head is carried out under largeamplitude of variation (0.67
1.33
) so that the effects of
different operating conditions can be revealed.Aiming at two cases ofHPPA (with surge tank of real case
and without surge tank of assumed case), the investigationof the effects of
,
0, and
0on stability is proceeded
by controlling variable method. The default values of ,
0, and
0are 2.0s, 4.0m (4.4%
), and 90m (1.00
),
respectively. The values of other parameters are as follows:= 1.5,
= 1,
= 1,
= 0.5,
= 0,
= 1,
=
8.34 s, = 0, and = 0.9, in which = /
is amplification
coefficient of sectional area of surge tank, and is critical
stable sectional area.
Mathematical Problems in Engineering 5
0.0 0.2 0.4 0.6 0.8 1.00
5
10
15
20
25
30
0.0 0.2 0.4 0.6 0.8 1.00
5
10
15
20
25
30
0.25 0.30 0.353
4
5
0.0 0.2 0.4 0.6 0.8 1.00
5
10
15
20
25
30
0.25 0.30 0.353
4
5
Kp/K
i(s
)Kp/K
i(s
)Kp/K
i(s
)
1/Kp
1/Kp
1/Kp
Twt = 1.0 sTwt = 2.0 s
Twt = 3.0 sTwt = 4.0 s
ht0 = 0.0 mht0 = 2.0 mht0 = 4.0 m
ht0 = 6.0 mht0 = 8.0 m
H0 = 60 mH0 = 90 mH0 = 120 m
(a1) Twt
(a2) ht0
(a3) H0
(a) System without surge tank
30
0.0 0.2 0.4 0.6 0.8 1.00
5
10
15
20
25
0.0 0.2 0.4 0.6 0.8 1.00
5
10
15
20
25
30
S
0.0 0.2 0.4 0.6 0.8 1.00
5
10
15
20
25
30
Kp/K
i(s
)Kp/K
i(s
)Kp/K
i(s
)
1/Kp
1/Kp
1/Kp
Twt = 0.0 sTwt = 1.0 sTwt = 2.0 s
Twt = 3.0 sTwt = 4.0 s
ht0 = 0.0 mht0 = 2.0 mht0 = 4.0 m
ht0 = 6.0 mht0 = 8.0 m
H0 = 60 mH0 = 90 mH0 = 120 m
(b1) Twt
(b2) ht0
(b3) H0
(b) System with surge tank
Figure 4: Effects of penstock and net head on stability regions.
6 Mathematical Problems in Engineering
The stability regions of turbine regulating system withsurge tank or not are shown in Figure 4.
Figure 4 shows the following.
(1) For the turbine regulating system without surge tank,
has significant effect on stability while the effectsof
0and
0are relatively small. When
increases
from 1 s to 4 s, the stability region reduces obviously;that is, the stability of system notably worsens. Withthe rise of
0from 0.0m to 8.0m (8.9%
), the
stability region enlarges slightly. On the contrary, thestability region diminishes slightly if
0increases
from 60m (0.67) to 120m (1.33
).
(2) For the turbine regulating system with surge tank,,
0, and
0all have bigger effects on stability,
especially, 0. The stability region enlarges with
the decrease of
and increase of 0. When
0
decreases from 8.0m (8.9%) to 2.0m (2.2%
), the
stability region enlarges dramatically. It is importantto note that there is an intersection point between thestability boundary curves of
0= 0.0m and
0=
2.0m (Point in Figure 4(b2)). In the right sideof Point the stability region diminishes with theincrease of
0while the change law is just opposite
to the left side of Point .(3) By comparing the turbine regulating system without
surge tank and that with surge tank, the followingresults can be obtained. The effect laws of
on
the stability of these two systems are consistent andthe difference is that the influence on system withoutsurge tank is more sensitive than that with surgetank, while the effect laws of
0as well as
0on
these two systems are contrary and the influence onsystem with surge tank is far more sensitive than thatwithout surge tank. When
,
0, and
0change,
the variation amplitude of stability boundary curvesin the domain of small 1/
is much greater than that
of big 1/for system without surge tank; however,
the variation amplitudes of stability boundary curvesin these two domains are close for system with surgetank.
4. Effect of Penstock on Regulation Quality
Regulation quality reflects the rapidity and stationarity ofdynamic response of regulating system. The common useddynamic performance indexes that evaluate regulation qual-ity are peak time, settling time, overshoot, and number ofoscillation. Regulation quality depends on its own oscilla-tion characteristic of dynamic response [22]. The dynamicresponse of turbine regulating system is represented by thetime response of the frequency of hydroelectric generatingunit. Hence, the regulation quality is determined by oscilla-tion characteristic of time response of the frequency in timedomain.
4.1. Time Response of the Frequency. The input signal for astep load disturbance can be computed from
() =
0/,
in which0
is relative value of the load step. Substitution of
() =
0/ into (9) and (8) yields the following output
signals of time response of the frequency for system withoutsurge tank and system with surge tank, respectively:
() =
3
=23
5
=25
0
, (12)
() =
3
=03
5
=05
0
. (13)
4.2. Regulation Quality Analysis. By proceeding in a similarmanner with stability analysis in Section 3.2, HPP A is alsotaken as an example to analyse the effect mechanism of waterinertia and head loss of penstock on regulation quality ofturbine regulating system with surge tank or not. For the caseof 10% load step reduction when the unit operates at ratedpower output, that is,
0= 0.1, the time responses of the
frequency of the two turbine regulating systems are shown inFigure 5, in which
and
are 2.0 and 0.1 s1, respectively,
and other parameters are the same as those in Section 3.2.Note that the formula of the period of water-level fluctu-
ation in surge tank in frictional headrace tunnel, surge tanksystem is shown in Appendix D.
Figure 5 and Table 2 show the following.
(1) Under step change in load, there are obvious differ-ences of time responses of the frequency betweensystem without surge tank and that with surge tank.The time response of the frequency of system withoutsurge tank is a single property oscillation which iscaused by water hammer wave in penstock, and thisresponse has the characteristics of short period, largeamplitude, and fast attenuation. The time response ofthe frequency of systemwith surge tank is superposedby twooscillations of different properties. In these twooscillations, the one in the beginning time intervalof time response of the frequency is called headwave and the other in the follow-up time interval iscalled tail wave (shown in Figure 5(b1)), of which theformer has the same property with the oscillation ofsystem without surge tank and the latter belongs tolow frequency forced oscillation caused bywater-levelfluctuation in surge tank. The period of tail wave isconsistent with that of water-level fluctuation in surgetank. Tail wave has the characteristics of long period,small amplitude, and slow attenuation, and it is themain body of time response of the frequency andthe principal factor that determines the regulationquality.
(2) For the turbine regulating system without surge tank,like the effects on stability,
has significant effect
on time response of the frequency while the effectsof
0and
0are relatively small. When
rises,
the maximum amplitude, overshoot, and numberof oscillation enlarge dramatically and regulationquality worsen obviously. The maximum amplitudeand overshoot increase with the rising of
0and
Mathematical Problems in Engineering 7
Table 2: Characteristic parameters for time responses of the frequency of turbine regulating system with surge tank or not under0= 0.1.
Types of fluctuationSystem without surge tank System with surge tank Water-level fluctuation
in surge tankHead wave Tail waveMaximum Maximum Amplitude Attenuation rate Period (s) Period (s)
(s)0 / 0.0318 0.0140 0.0007 323.87 313.911 0.0337 0.0344 0.0141 0.0007 322.21 313.912 0.0416 0.0419 0.0142 0.0007 322.21 313.913 0.0529 0.0534 0.0145 0.0006 322.21 313.914 0.0666 0.0670 0.0145 0.0006 322.21 313.91
0(m)0 0.0395 0.0398 0.0122 0.0010 317.33 310.722 0.0404 0.0409 0.0132 0.0008 318.94 312.214 0.0416 0.0419 0.0142 0.0007 322.21 313.916 0.0427 0.0429 0.0156 0.0006 325.55 315.878 0.0439 0.0443 0.0172 0.0004 328.96 318.15
0(m)60 0.0427 0.0426 0.0227 0.0005 356.99 342.1190 0.0416 0.0419 0.0142 0.0007 322.21 313.91120 0.0410 0.0415 0.0105 0.0013 286.90 305.00
Table 3: Basic information of actual examples of HPP.
HPP Rated power output(MW) Rated head
(m) Rated discharge
(m3/s)
(s)
(s)
0(m)
0(m)
A 51.28 90.00 62.70 17.75 2.33 7.57 5.53B 118.56 177.00 72.50 39.73 1.82 20.53 5.12C 610.00 288.00 228.60 23.84 1.26 12.92 2.91
regulation quality worsens as a consequence. If 0
increases, the maximum amplitude and overshootdecrease and then regulation quality is improved.
(3) For the turbine regulating systemwith surge tank, theeffect laws of
,
0, and
0on head wave are the
samewith those on the time response of the frequencyof system without surge tank;
has almost no
influence on tail wave while the influences of 0and
0are significant.With the increase of
, the period
of tail wave reduces and the maximum amplitudeand attenuation rate of tail wave enlarge. As a result,regulation quality will get better or worse. When
0
rises, regulation quality notably worsens because ofthe increase of period and maximum amplitude andthe decrease of attenuation rate. In contrast with
0,
the period and the maximum amplitude reduce andattenuation rate enlarges with the rising of
0, and the
regulation quality notably gets better.In the high head HPP, pressure fluctuation in penstock
and limited speed of guide vane movement are importantfor the stable and secure operation at the changes of poweror frequency, especially at load rejections and emergencyshut-down functions. Figure 6 gives the time responses of theguide vane opening and net head of turbine regulating
system with surge tank or not under0
= 0.1 correspond-ing to time response of the frequency .
Figure 6 shows the following.
(1) The change laws of guide vane opening response andnet head response of system without surge tank arethe same with those of system with surge tank. Whenthe frequency increases (or decreases), the guide vaneopening decreases (or increases) to reduce (or rise)the discharge and output power, and then the net headincreases (or decreases) because of the reduction (orrising) of discharge.
(2) The amplitude of variation of guide vane openingresponse is larger than that of net head response,and they are larger than that of time response of thefrequency, especially in the system with surge tank.This result indicates that guide vane opening responseand net head response are more sensitive than timeresponse of the frequency to load disturbance.
(3) The stability of these three responses is the same,while their regulation qualities are of significant dif-ferences.
8 Mathematical Problems in Engineering
0 30 60 90 120 1500.02
0.00
0.02
0.04
0.06
0.08
x
0 30 60 90 120 1500.02
0.00
0.02
0.04
0.06
0.08
x
0 30 60 90 120 1500.02
0.00
0.02
0.04
0.06
0.08
x
t (s)
t (s)
t (s)
Twt = 1.0 sTwt = 2.0 s
Twt = 3.0 sTwt = 4.0 s
(a1) Twt
(a2) ht0
(a3) H0
ht0 = 0.0 mht0 = 2.0 mht0 = 4.0 m
ht0 = 6.0 mht0 = 8.0 m
H0 = 60 mH0 = 90 mH0 = 120 m
(a) System without surge tank
0 200 400 600 800 10000.02
0.00
0.02
0.04
0.06
0.08
x 0 20 40 60 80 1000.000.020.040.060.08
Tail wave
Head wave
0 200 400 600 800 10000.02
0.00
0.02
0.04
0.06
0.08
x 0 20 40 60 801000.000.020.040.06
0 200 400 600 800 10000.02
0.00
0.02
0.04
0.06
0.08
x 0 20 40 60 80 1000.000.020.040.06
t (s)
t (s)
t (s)
Twt = 0.0 sTwt = 1.0 sTwt = 2.0 s
Twt = 3.0 sTwt = 4.0 s
(b1) Twt
(b2) ht0
(b3) H0
ht0 = 0.0 mht0 = 2.0 mht0 = 4.0 m
ht0 = 6.0 mht0 = 8.0 m
H0 = 60 mH0 = 90 mH0 = 120 m
(b) System with surge tank
Figure 5: Effects of penstock and net head on time responses of the frequency.
5. Effect Mechanism of Water Inertia andHead Loss of Penstock and Its Applications
5.1. Effect Mechanism of Water Inertia and Head Loss ofPenstock. Based on the analyses in Sections 3 and 4, theeffect mechanism of penstock is epurated and summarized asfollows.The stability and regulation quality of systemwithoutsurge tank are determined by the dynamic response (e.g.,time response of the frequency) which only depends onwater
hammer wave in penstock. However, for system with surgetank, the dynamic response depending on water hammerwave in penstock and water-level fluctuation in surge tankjointly determines the stability and regulation quality. Specificto the effects of water inertia and head loss of penstock.
Water inertia of penstock is the principal aspect thatinfluences water hammer wave. Hence, the stability and timeresponse of the frequency of system without surge tank, aswell as the stability and head wave of system with surge
Mathematical Problems in Engineering 9
0 10 20 30 40 50
0.3
0.2
0.1
0.0
0.1
0.2Re
spon
ses
t (s)
Frequency xGuide vane opening yNet head h
(a) System without surge tank
0 200 400 600 800 1000
0.3
0.2
0.1
0.0
0.1
0.2
Resp
onse
s
Frequency xGuide vane opening yNet head h
(b) System with surge tank
Figure 6: Time responses of the guide vane opening and net head.
tank, are significantly impacted by thewater inertia.However,water hammer wave which is low frequency fluctuationhas little influence on water-level fluctuation in surge tank.Therefore, there is almost no effect of the water inertia on thetail wave of system with surge tank.
Head loss of penstock is the damping of turbine regulatingsystem and influences the water-level fluctuation charac-teristic in surge tank mainly by impacting the water flowmovement and energy consumption of surge tank-penstocksubsystem. Hence, the head loss almost has no effect onthe stability and time response of the frequency of systemwithout surge tank, while the stability and tail wave of systemwith surge tank are notably affected. In addition, in themathematicalmodel of turbine regulating system (Section 2),0is represented in the form of
0/
0which indicates that
the effect of 0is actualized by serving as the amplification
coefficient of 0(i.e., 1/
0). This result reveals the internal
cause of the opposite effects of 0and
0.
5.2. Application I: Improvements of Stability and RegulationQuality. According to the effect mechanism of water inertiaand head loss of penstock, the stability and regulation qualitycan be improved specifically. The methods of improvementare the results in Sections 3 and 4. Reversely, in the design ofHPP, the effect mechanism can provide theoretical founda-tion and guidance for reasonable selections of
,
0,
0,
, and
to guarantee preferable stability and regulation
quality.
5.3. Application II: Construction of Equivalent Model. Byneglecting secondary factors in the complete mathematicalmodel of turbine regulating system based on the effectmechanism of penstock, some equivalent simplified modelscan be constructed.
5.3.1. Equivalent Model for Stability of System without SurgeTank. For stability of system without surge tank, the waterinertia and head loss of penstock are the principal factor andsecondary factor, respectively. Hence, if the head loss item
Twts
Qt(s) H(s)
Figure 7: Block diagramof pipeline systemwithout surge tankwhenhead loss of penstock is neglected.
is neglected, the original block diagram of pipeline systemwithout surge tank shown in Figure 2(c) is simplified to theblock diagram shown in Figure 7. Then the equivalent freeoscillation equation of (10) can be obtained by letting
0be 0.
This equivalent equation is also third order. HPP B and HPPC (shown in Table 3 of Appendix C, assumed cases withoutheadrace tunnel and surge tank) are taken as examples toverify the stability of this equivalent third order model andoriginal third ordermodel (i.e., see (10)).The stability regionsof these twomodels are shown in Figure 8. It can be seen thatthe stability regions of equivalent model and original modelare nearly overlapped.
5.3.2. Equivalent Model for Regulation Quality of System withSurge Tank. For regulation quality of system with surge tank,the head loss and water inertia of penstock are the principalfactor and secondary factor, respectively. Proceeding simi-larly as Section 5.3.1, Figure 9 and (14) obtained by neglectingthe water inertia item are the equivalent simplified blockdiagram of pipeline systemwith surge tank of Figure 2(b) andtime response of the frequency of (13), respectively:
() =
3
=13
5
=15
0
. (14)
Equation (14) is a fourth order response model and itscoefficients are the special cases of those in original fifth orderresponse model (see (13)) when
is 0. According to Galois
theory [23], original fifth order model has no extract rootsformulas. Therefore, it is not only impossible to solve thefluctuation equation of time response of the frequency (i.e., = ()) from original fifth order model directly, but alsodifficult to carry out theoretical analysis. This paper realizes
10 Mathematical Problems in Engineering
0.0 0.2 0.4 0.6 0.8 1.00
5
10
15
20
25
30
Original third order modelEquivalent third order model
Kp/K
i(s
)
1/Kp
(a) HPP B
0.0 0.2 0.4 0.6 0.8 1.00
5
10
15
20
25
30
Original third order modelEquivalent third order model
Kp/K
i(s
)
1/Kp
(b) HPP C
Figure 8: Comparison of stability regions between equivalent third order model and original third order model.
+
+
+
2ht0/H0
Twys
2hy0/H0
TFs
Qt(s) H(s)
Figure 9: Block diagram of pipeline system with surge tank whenwater inertia of penstock is neglected.
order reduction by using the effect mechanism of penstockand obtains an equivalent fourth order responsemodel whichcan be theoretically solved.Themethod and result have greatapplication values.
Figure 10 compares the time responses of the frequencybetween equivalent fourth order model and original fifthorder model using HPP B and HPP C. There is a satisfactoryagreement between the time responses of the frequency ofthese two models. This result indicates that the equivalentfourth order model can represent and replace the originalfifth order model.
6. Conclusions
Aiming at the turbine regulating system of isolated HPPwithout surge tank and that with surge tank, this paperstudies the effect mechanism of water inertia and headloss of penstock on stability and regulation quality underload disturbance based on the free oscillation equation andtime response of the frequency of system. The constructionmethods of equivalent models for stability and regulation
quality are proposed according to the effect mechanism. Themajor conclusions are summarized as follows.
(1) The stability and regulation quality of system withoutsurge tank are determined by time response of the fre-quency which only depends on water hammer wavein penstock, while for system with surge tank, thetime response of the frequency depending on waterhammer wave in penstock and water-level fluctuationin surge tank jointly determines the stability andregulation quality.
(2) Water inertia of penstock mainly affects the stabilityand time response of the frequency of system withoutsurge tank as well as the stability and head waveof time response of the frequency with surge tank.However, it has almost no effect on the tail wave oftime response of the frequency with surge tank.
(3) Head loss of penstock mainly affects the stability andtail wave of time response of the frequency with surgetank rather than the stability and time response ofthe frequency without surge tank and head wave.Theeffect of
0on stability and regulation quality which
is opposite to that of 0is actualized by serving as the
amplification coefficient of 0(i.e. 1/
0).
(4) The effect mechanism of penstock can be appliedas theoretical foundation and guidance to improvestability and regulation quality.
(5) For stability of system without surge tank, the thirdorder free oscillation equation obtained by neglectingthe head loss item of penstock is the equivalentmodel of original third order free oscillation equation.For regulation quality of system with surge tank,the fourth order response obtained by neglecting
Mathematical Problems in Engineering 11
0 400 800 1200 1600 2000
0.02
0.01
0.00
0.01
0.02
0.03
0.04
x
Original fifth order response modelEquivalent fourth order response model
t (s)
(a) HPP B
0 400 800 1200 1600 2000
0.02
0.01
0.00
0.01
0.02
0.03
0.04
x
Original fifth order response modelEquivalent fourth order response model
t (s)
(b) HPP C
Figure 10: Comparison of time responses of the frequency between equivalent fourth order model and original fifth order model.
the water inertia item of penstock is the equivalentmodel of original fifth order response.
Appendices
A. Definitions of Parameters
See Nomenclature Section.Note the following.
(1) = /0, = (
0)/
0,
= (
0)/
0,
= (
0)/
0, = (
0)/
0, = (
0)/
0,
= (
0)/
0, and
= (
0)/
0are
the relative deviations of corresponding variables.Thesubscript 0 refers to the initial value:
0=
0=
0,
=
0/
0.
(2) The six transfer coefficients are defined as follows:=
/,
=
/,
=
/,
=
/
,
= /, and
=
/.
(3) is actually equal to the relative deviation of load in
the isolated operation. Hence, is regarded as the
load disturbance.
B. Expressions of Coefficients
The expressions of coefficients in overall transfer function(see (8)) are as follows:
0=
19,
1=
110+
29+
512,
2=
111+
210+
39+
513+
612,
3=
211+
310+
49+
613+
712,
4=
311+
410+
713+
812,
5=
411+
813,
0=
1,
1=
2,
2=
3,
3=
4,
1=
,
2=
[
(1 +
20
0
) +
20
0
] ,
3=
(
+
) +
20
0
(1 +
20
0
) ,
4= 1 +
2 (0
+ 0)
0
,
5=
,
6=
(
20
0
+
20
0
) ,
7=
+
+
20
0
20
0
,
8=
2 (0
+ 0)
0
,
9=
,
10
=
(
)
+
,
11
= ,
12
=
,
13
= .
(B.1)
12 Mathematical Problems in Engineering
C. Basic Information of ActualExamples of HPP
See Table 3.
D. Period of Water-Level Fluctuation inSurge Tank in FrictionalHeadrace Tunnel-Surge Tank System
Based on reference [1], the free oscillation equation of water-level fluctuation in surge tank in frictional headrace tunnel-surge tank system is derived as follows:
2
2+ 2
+ 2
= 0, (D.1)
where = (V0/2)[2/
/(
0 2
0)], = (
/
)(1 (2
0/(
0 2
0))), =
0/V2
0, and V
0is flow
velocity in headrace tunnel.The period of water-level fluctuation in surge tank is
obtained according to (D.1):
= 2/2
2. If the fric-tion is neglected, the formula of period is simplified to
=
2/
.
Nomenclature
: Change of surge tank water level (positivedirection is downward)
: Headrace tunnel discharge
: Unit frequency
: Kinetic moment
: Length of headrace tunnel
: Sectional area of headrace tunnel
0: Head loss of headrace tunnel
: Water inertia time constant of headrace
tunnel: Sectional area of surge tank,
,
: Moment transfer coefficients of turbine
: Unit inertia time constant
: Proportional gain
: Net head
: Penstock discharge
: Guide vane opening
: Resisting moment
: Length of penstock
: Sectional area of penstock
0: Head loss of penstock
: Water inertia time constant of penstock
: Time constant of surge tank
,
,
: Discharge transfer coefficients of turbine
: Load self-regulation coefficient
: Integral gain.
Conflict of Interests
The authors declare that there is no conflict of interestsregarding the publication of this paper.
Acknowledgment
This work was supported by the National Natural ScienceFoundation of China (Projects nos. 51379158 and 51039005).
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