An AHP Approach for Determining the Weightage of Reaction Turbine Parameters Influencing its Performance

DOI : 10.17577/IJERTV3IS090613

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An AHP Approach for Determining the Weightage of Reaction Turbine Parameters Influencing its Performance

Rajib Das Ankuran Saha

    1. ech 2nd year Hydro Informatics Department; Assistant Professor National Institute Of Technology; Agartala Department of Mechanical Engineering:

      NIT Agartala

      Abstract Cavitation and its negative consequences have a significant effect on the overall performance of a hydro power plant. Various causes which provoke the formation of different types of cavitations have a significant effect on the performance of a hydro power plant. In this present paper an attempt has been made to find the most significant cause and the relative weightage of the causes which influences the performance of a hydropower plant.A Fuzzy scale has been introduced to rate different parameters. The rating has been done on the basis of information provided in different literatures and published research papers. The weightage of different parameters is obtained with AHP method.The waterfall model of AHP has generated the weightage of the causes which significantly affects the performance of a hydro power plant. A Francis Turbine has been considered for study.

      Key words: Cavitation; AHP; FUZZY; Francis turbine

      1. INTRODUCTION

        Cavitation is formation of vapor bubbles in the liquid flowing through any Hydraulic Turbine.Cavitation occurs when the static pressure of the liquid falls below its vapor pressure. In turbines cavitation occurs mainly near the fast moving blades and in the exit region [1]. Knapp et al. [2]defined cavitation as the phenomenon which takes place at constant temperaturewhen a liquid reaches a state at which vapor cavities are formed and grow due to dynamic- pressure reductions to the vapor pressure of the liquid. Theemission of large amplitude shock-wavesare generatedin a very short time of about several nanoseconds due to the violentprocess of cavity collapse takes place and as demonstrated by Avellan and Farhat [3].Travelling bubbles, attached cavities or cavitating vortices are the different forms of cavities which can form in a flowing liquid described by Hammit [4] and Arndt [5].

        Cavitation is defined as the formation of the vapor phase in a liquid. The initial formation of bubbles (inception) to large-scale, attached cavities (supercavitation)impliesthe term cavitation. The formation of individual bubbles and subsequent development of attached cavities, bubble clouds, etc., is directly related to reductions in pressure to some critical value, which in turn

        is associated with dynamical effects, in a flowing liquid [6].

        Cavitation causes hazardous effects on hydraulic turbines such as erosion, vibration, machine efficiency loss and noise depending on the various causes of occurrence such as higher or lower head then the machine design, partial or high load, velocity component of flow discharge and the plant cavitation number. This is why it is necessary to know what brings about the creation of steam bubbles in the liquid flow of hydraulic turbines and the ways to avoid harmful cavitationalconditions.The paper presents the cavitation types and the most important causes and effects on the performance of reaction turbine based on their weightage using fuzzy scale and AHP method.

        The earliest studies on the theory of a cavitating flow with free boundaries and supercavitation were published in the book [7] followed by [8] .A large number of exact solutions of plane problemsderivations can be easy obtained with the help of these books as it includes well- developed theory of conformal mappings of functions of a complex variable. Another venue combining the existing exact solutions with approximated and heuristic models was explored in the work [9] that refined the applied calculation techniques based on the principle of cavity expansion independence, theory of pulsations and stability of elongated axisymmetric cavities, etc [10], [11].

        APPENDIX NOMENCLATURE

        PB bubble pressure (Pa)

        RB bubble radius (m).

        Ro bubble maximum radius (m) Pv vapor pressure (Pa)

        P infinite domain pressure (Pa)

        Surface tension (N/m)

        viscosity (m2/s)

        density (Kg/m3)

        Rayleigh time (s)

        p Thoma coefficient

        GM geometric mean

        CI consistency index

        RI random index

        LE Leading Edge

        TB Travelling Bubble

        IB Inter Blade Vortex

        DT Draft Tube Swirl

        H Head

        L Load

        V Velocity Component FlowDischarge C Plant Cavitation Number

        1.1. Effects Of Cavitation In Turbine

        Cavitation can affect the performance of turbomachinery resulting in decreased efficiency of hydro turbines [12], [13], [14]. Noise and vibration occur in many applications. In addition to the deleterious effects of reduced performance, noise and vibration, there is the possibility of cavitation damage [6],[12],[13],[15], [16].

        cavitation occurs in turbomachinery it can induce abnormal dynamic behavior and cause serious erosion [19].

        2.3 Travelling Bubble

        In low pressure regions of the flow bubbles usually appear around a body from micron-sized nuclei. They implode when they find an adverse pressure gradient whiletravelling with the flow.Air content of the liquidinfluenced these bubbles strongly. Nevertheless, their erosive power is considered to be relatively weak [19].Based on the assumption that remains spherical in an infinite liquid an isolated bubble can be modeled [21]. In this case, the generalized RayleighPlesset equation is a valid approximation of the bubble growth and it can be solved to find the radius of the bubble, RB (t) provided that the bubble pressure, PB(t); and the infinite domain pressure, P (t); are known:

        They cause the erosion noise, mechanical vibrations,

        P t P t

        d²R

        1. dR 2

          4 dR 2

          and modification of flow field of the hydraulic machine

          = R dt² + 2 dt

          + R dt + R

          [16].According to the fact that cavitation is connected with efficiency change,increase of noise level and increase of vibrations, the numerous researches arefocusedon various experimental methods which indirectly via the above mentionedeffects estimate the cavitational phenomena in water turbines [17],[18].

          .

      2. DIFFERENT FORMS OF CAVITIES IN LIQUID

        FLOW

        1. Vortex Cavitation

          At low pressures,flow regions with concentrated vortices can develop cavitation in their central cores. The solid surface becomes potentially erosive if the tips of thevapor filled vortices are in contact with it since the final collapse of the whole cavity takes place on them. If Von Karman vortex-shedding occurs at the trailing edge of a hydrofoil this type of cavitation can developwhen pressure is low enough. As a result, lift fluctuations are provoked synchronized with the shedding frequency[19].

          2.2 Attached Cavities

          In the flowmacro-cavities aredeveloped on a solid wallthattakes the form of cavitation. Cavitation grows from the leading edge on the suction side of a hydrofoil with a positive angle of incidence. This is a very common and complex type of cavitation that can present different regimes depending on the hydrodynamic conditions. Sheet cavitation is one of the regimes, whichcharacterized by thin stable cavities with smooth and transparent interfaces. At their rear part, the cavity closure presents a slight and weak pulsation due to the shedding of small cavitation vortices so that it represents a low risk of erosion [19].

          Cloud cavitationis another regime,shows a strong unsteadiness and a pulsating behavior that provokes signficant oscillations of the cavity length. The cavity interface is wavy and turbulent. Large U-shaped transient cavities and clouds of cavities are shed awaydownstream of the cavity closure that collapse violently on the solid surface [20]. Consequently, this is a very aggressive form of cavitation with a high erosive power. When this type of

          Assuming that the bubble reaches a maximum radius, R0; from which the implosion orcollapsing process starts, the Rayleigh time or collapse time ; until RB = 0 is reached is given by

          = 0:915R0

          PP

            1. Leading Edge Cavitation

              On the suction side of the runner blades or on the pressure side[14]it takes the form of an attached cavity in (fig 1) due to operation at a higher head than the machine design head when the incidence angle of the inlet flow is positive and largely deviated from the design value or at a lower head than the machine design head when the incidence angle is negative [19]. This type of cavitation is a very aggressive and deeply erodes the blades also provoke pressure fluctuations [1] when it becomes unstable. This type of cavitation is not very sensitive to the value of the Thoma number and it can lead to a severe erosion of the blades [14].

              Fig1.Shows Leading edge cavitation Picture courtesy of Saini [22]

            2. Travelling bubble cavitation

              It is attached to the blade suction sidenear the mid- chord next to the trailing edgewhich takes the form of separated bubbles(fig 2). When the machine operates in overload condition with the highest flow ratethese travelling bubbles appear due to a low plant cavitation number and they grow with load reaching their maximum [19]. This type of cavitation is a severe and noisy type which significantlyreduces the machine efficiency and ifthe bubbles collapse on the blade it that provoke erosion[1]. This type of cavitation is very sensitive to the content of cavitation nuclei and to the value of the Thoma number [14], [23].

              Fig2.Shows travelling bubble cavitation Picture courtesy of Grindoz [24]

            3. Draft tube swirl

              It is a cavitation vortex-core flow that it formed just below the runner cone in the centre of the draft tube fig 3. Its volume depends on and it appears at partial load and at overload due to the residual circumferential velocity component of the flow discharged from the runner [19]. This type of cavitation provokes large bursts of pressure pulses in the draft tube causing strong vibrations on the turbine and even on the powerhouse [1].

              Fig 3.Shows draft tube swirl Picture courtesy of Saini [22]

            4. Inter-blade vortex cavitation

          This is formed by secondary vortices located in the channels betweenblades that arise due to the flow separation provoked by the incidence variation from the hub tothe band (fig 4). These vortices appear at partial load operation and yield a high broadband noise level. They can also appear and cavitate at extremely high-head operation ranges because the is relatively low [19]. It cause strong vibrations if becomes unstable and if their tip is in touch with the runner surface they can result in erosion.

          Fig4.Shows Inter-blade vortex cavitation Picture courtesy of Avellan [20]

      3. FUZZY LOGIC

        Fuzzy logicconcepthas been introduced by Lotfi Zadeh. It is relatively young theory;the areas of applications are process control, management and decision making, operations research, economies. The major advantage of this theory is that linguistics terms are used in description of problems, rather thanin terms of relationships between precise numerical values is.

        A linguistic variable are not expressed in numbers but words or sentences in a natural or artificial language, i.e., in terms of linguistic (Zadeh, 1975) [25]. The concept of a linguistic variable is very useful in dealing with situations, which are too complex or not well defined to be reasonably described in conventional quantitative expressions (Zimmermann, 1991)[26]. For example, weight is a linguistic variable whose values are very low, low,

        medium, high, very high, etc. Fuzzy numbers can also represent these linguistic values.

        Fuzzy logic aims to model human thinking and reasoning.The key advantage of the fuzzy methods is how they reflect the human mind in its remarkable ability to store and process information that is imprecise, uncertain and resistant to classification [27].

        Fuzzy logic theoryis a uniquely useful tool due to its capability of handling theinherent fuzziness or imprecision of real-world informationin ascientific fashion[28] andbecomes even more powerful when applied in conjunctionwith analytical modeling and stochastic simulation.

        In the decision-making process fuzzy logic has been with analytic hierarchy process to form a model for risk assessment. Those risk assessment models are widely applied to multiple fields such as floor water invasion in coal mines [29], oil and gas offshore wells [30], electronic

        engineering [31], [32], information technology projects [33],green initiatives in the fashion industry [34], food supply chains [35].

        The linguistic fuzzy scale used in this paper is given below:

          1. Analytic Hierarchy Process

            Multi Criteria decision making method, Analytic Hierarchy Process (AHP) was developed by Saaty [36], [37], [38] uses a process of pair wise comparison to determine the relative importance of alternatives in decision making.It converts individual preferences into ratio scale weights that can be combined into a linear additive weight for each alternative.

            The steps of fuzzy AHP decision making are given as follows

            1. Find out the relative importance of different criteria with respect to the objective. For this a pair-wise comparison matrix using a scale of relative importance has to construct. Using the fundamental scale of the AHP the judgments are entered. An attribute compared with it is always assigned the value 1 so the main diagonal entries of the pair-wise comparison matrix are all 1. The numbers 6, 7, 9, and 11 correspond to the verbal judgments slightly more effective, effective, more effective, and extremely more effective (with 1, 2, 3, and 4 for compromise between the previous

        the attributes because of its simplicity and easiness to find out the maximum Eigen value and to reduce the inconsistency in judgments.

        1. Calculate matrix A3 and A4 such that A3 = A1 x A2 and A4 = A3 / A2, where A2 = [W1, W2, ,WM]T. Each element of A4 is obtained by dividing each element of A3 by the corresponding element of A2.

          Extre mely more effect ive

          Mor e effe ctive

          Effe ctive

          Slig htly mor e effe

          ctive

          Equal weig htage

          Slig htly less effe ctive

          Less effe ctive

          Ver y less effe ctive

          Extre mely less effect ive

          11

          9

          7

          6

          5

          4

          3

          2

          1

        2. Find out the maximum eigen value max (i.e. the average of matrix A4).

        3. Calculate the consistency index CI = (max M) / (M 1). The smaller the value of CI, the smaller is the deviation from the consistency.

        4. Obtain the random index (RI) for the number of at- tributes used in decision making [39].

        5. Calculate the consistency ratio CR = CI/RI. Usually, a CR of 0.1 or less is considered as acceptable and it reflects an informed judgment that could be attributed to the knowledge of the analyst about the problem under study.

      4. FORMULATIONS OF COMPARISON MATRIX AND WEIGHTED MATRIX

    1. Pair wise comparisons of negative effects on the basis of turbine performance

      Vibration Erosion Efficiency Noise

      values). Assuming Mcrteria, the pair-wise comparison of attribute i with attribute j yields a square matrix A1 where rij denotes the

      /

      / /

      comparative importance of attribute i with respect to attribute j. In the matrix, rij= 1 when

      i = j and rji= 1 / rij

      1 2 3 M Criteria

      11 12 13 1 1

      / / /

      Table1. Shows the pair-wise comparisons determine the weightage of

      effects on turbine performance

      Weightage of Effects on the basis of turbine performance

      Vibration

      Erosion

      Efficiency

      Noise

      0 .2343

      0.1679

      0.5404

      0.0574

      21 22 23

      2

      2

      31 32 33 3

      3

      Table2.Shows theweightage of negative effects w.r.t turbine

      AI =

      (1)

      1 2 3

      performance

    2. Weightage of cavitation types depending on their negative effects on performance of turbine

      b) Find the relative normalized weight (Wj) of each at-tribute by i) calculating the geometric mean of ith row and ii) normalizing the geometric means of

      In terms oferosion, pair-wise comparisons determine the weightage of different types of cavitation

      LE TB IB DT

      rows in the comparison matrix. This can be represented as

      1

      j=1

      GMi = M

      rij M

      (2)

      Wj = GM GM

      (3)

      =1

      The geometric mean method of AHP is used in the present work to find out the relative normalized weights of

      Table3. Shows the pair-wise comparisons determine the weightage of different types of cavitation in terms of Erosion.

      Weightage of cavitation type depending on erosion effect

      Leading edge

      Travelling bubble

      Inter blade vortex

      Draft tube swirl

      0.36906

      0.21031

      0.26094

      0.15969

      Table4. Shows the weightage of different types of cavitation w.r.t

      erosion

      In terms of vibration, pair-wise comparisons determine the weightage of different types of cavitation:

      LE TB IB DT

      Weightage of cavitation type depending on noise

      Leading edge

      Travelling bubble

      Inter blade vortex

      Draft tube swirl

      0.16251

      0.33695

      0.25421

      0.24532

      Table10. Shows the weightage of different types of cavitation w.r.t

      noise

    3. Weightage of the causes of cavitation in different types of turbine

In terms ofleading edge cavitation, pair-wise comparisons determine the weightage of causes:

H L V C

Table5.Shows the pair-wise comparisons determine the weightage of

different types of cavitation in terms of Vibration.

Weightage of cavitation type depending on vibration effect

Leading edge

Travelling bubble

Inter blade vortex

Draft tube swirl

0.16105

0.17824

0.33729

0.32405

Table6.Shows the weightage of different types of cavitation w.r.t

vibration

In terms ofefficiency, pair-wise comparisons determine the weightage of different types of cavitation:

LE TB IB DT

Table11. Shows the pair-wise comparisons determine the weightage of

causes in terms of LE

Weightage of causes of Leading edge cavitation are

Head

Load

Velocity component of flow discharge

Plant cavitation number

0.34645

0.18732

0.18675

0.27947

Table12. Shows the weightage of cause w.r.t LE

In terms of travelling bubble cavitation, pair-wise

comparisons determine the weightage of causes:

H L V C

Table7.Shows the pair-wise comparisons determine the weightage of

different types of cavitation in terms of Efficiency.

Weightage of cavitation type depending on efficiency reduction

Leading edge

Travelling

bubble

Inter blade

vortex

Draft tube

swirl

0.21203

0.38341

0.22359

0.18097

Table8. Shows the weightage of different types of cavitation w.r.t

efficiency

In terms of noise, pair-wise comparisons determine the weightage of different types of cavitation:

LE TB IB DT

Table13.Shows the pair-wise comparisons determine the weightage of

causes in terms of TB

Weightage of causes of travelling bubble cavitation are

Head

Load

Velocity component of

flow discharge

Plant cavitation number

0.16511

0.28595

0.19713

0.35181

Table14.Shows the weightage of cause w.r.t TB

In terms of inter blade vortex cavitation,pair-wise comparisons determine the weightage of causes:

H L V C

Table9. Shows the pair-wise comparisons determine the weightage of different types of cavitation in terms of Noise.

Table15. Shows the pair-wise comparisons determine the weightage of

causes in terms of IB

Weightage of causes of inter blade vortex cavitation are

.

Head

Load

Velocity component of

flow discharge

Plant cavitation number

0.36115

0.29193

0.18411

0.16281

.

.

.

Table16.Shows the weightage of cause w.r.t IB

In terms of draft tube swirl cavitation, pair-wise comparisons determine the weightage of causes:

H L V C

Table22. Shows the weightage of the final result matrix of causes

6. CONCLUSIONS

From literatures different negative consequences of cavitation which are dominant for the declined performance of a hydro power plant are identified and rated on the fuzzy scale to build the AHP model. The AHP model has given

Table17. Shows the pair-wise comparisons determine the weightage of

causes in terms of DT

Weightage of causes of draft tube swirl cavitation are

Head

Load

Velocity component of

flow discharge

Plant cavitation number

0.16595

0.32905

0.31423

0.19077

Table18.Shows the weightage of cause w.r.t DT

5. RESULTS

Now for the final weightage of cavitaton types from the effects

Vibration erosion efficiency noise

the weightage of the negative effects of cavitation which are predominant on the overall performance of a hydro power plant. In the next stage the weightage of different types of cavitation is determined on the basis of their contribution towards causing a particular type of negative effect. Finally the weightage of different causes of cavitation are determined separately for each type of cavitation. These different weightage matrices have given the weightage of the causes of cavitation on the basis of their ultimate effect on hydro power plant performance. It has been seen that Load and Headare two most significant causes affecting the overall performance of a hydro power plant. The weightage of different causes may help in taking strategic decision for the establishment of a hydro power plant and at the same time at dynamic scenario during the operation of the turbine it may help in regulating the operational parameters for maximizing the performance of the plant and turbine.

. . . .

. . . .

.

.

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. . . . .

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