Turbulent Natural Convection and Thermal Behaviour of Cylindrical Gas-Insulated Transmission Lines (GIL)

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  • 8/11/2019 Turbulent Natural Convection and Thermal Behaviour of Cylindrical Gas-Insulated Transmission Lines (GIL)

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    Turbulent Natural Convection and Thermal

    Behaviour of Cylindrical Gas-Insulated

    Transmission Lines (GIL)

    Abdellah Chakir and Hermann

    Koch

    ,41rstmct - This paper presents a numerical study of the natural

    convection of gases in a horizontal armulus of gas-umdated

    transmission lines (GIL). It consist of thermal analysis of high

    voltage power gas insulated transmission lines,

    In different case

    studies the inner cylinder is heated of a constant heat or kept at a

    constant temperature, the outer cylinder is mamtained at constant

    temperature.

    The

    cylinders are

    long ancl the flow is assumed to have

    axially independent properties. The two dimensional analyses of the

    heat transfer and fluid motion are performed for Rayleigh number

    ranging from 10S to 100, the radius ratio is at 2,5. Comparisons are

    made with experimental test set up and measurements.

    Index Terms - Gas-Insulated Transmission Line, natural convection,

    thermal behavimrr, numerical study, amnrli, experimental test set-up,

    measurement

    I. INTRODUCTION

    Flows due to the natural convection between two horizontal

    isothermal cylinders has been widely studied by many

    authors. The study of this type of problem is usually

    encountered in many fields specially in solar concentrators,

    thermal storage plants, pressurised water reactors and

    electrical Gas insulated transmission lines.

    Many

    experimental and numerical works are carried out for laminar

    case or turbulent flow with low Rayleigh number (till 10) and

    for isothermal cylinders as boundary conditions. Only a few

    papers studied the convection with non isothermal boundary

    conditions and for a Rayleigh over than 107. The results of

    these experimental and theoretical-numerical studies show the

    dependence of the flow patterns on the Rayleigh number, the

    Prandtl number and radius ratio. Investigations of the problem

    experimental] y and numerically determined the temperature

    distribution and the local heat transfer coefficients in air and

    in water. The use of two fluid showed the Prandtl number

    affect the transition characteristics. In another experimental

    study it was shown, that the heat flow is substantially altered

    on both cylinders due to the influence of the eccentricity of

    the inner cylinder.

    Good agreement for the temperatures profiles and the flow

    pattern was found and the Graschoff transition number was

    determined indirectly. It was shown, that the stream fimction

    remain negative, i.e., no secondary counter-rotating cells

    generation. The flow regions of convection a three

    dimensional spiral flow divided into 5 regions: an inner

    boundary layer near the inner cylinder, an outer boundary

    layer near the outer cylinder, a vertical plume region above

    the inner cylinder, a stagnant region below the inner cylinder,

    and a core region surrounded by the four regions.

    This study consists of thermal analysis of high voltage power

    gas insulated transmission lines (GIL) based on the above

    mentioned basic knowledge. Two coaxial cylinders of a

    metallic sheath, an inner conductor and outer enclosure are

    separated by a dielectric medium, mixture of gas SF6 and Nz.

    The GIL is designed to be laid in underground or laid in

    Tunnel with a cooling air flow. The cylinders are very larger

    than the gap between the inner and outer cylinder, then the

    two dimensional is applicable.

    The results of the calculations and the experimental

    measurements show that for the GIL a ve~ good heat transfer

    from the conductor, which is represented by the inner pipe, to

    the outer enclosure is given. The temperature drop between

    conductor and enclosure is below 10 K. For the practical

    application of the GIL this means that for a directly buried

    GIL, or a GIL in a tunnel the thermal heat produced by the

    current through the conductor is transported fast to the

    surrounding of the GIL the soil or the ambient air, and leaves

    low maximum temperatures at the conductor.

    Compared to a solid insulated cable the maximum

    temperatures are much lower at the transition point between

    the outer cable or GIL surface and the soil or air around.

    Specially in cases of high transmission power ratings of 1500

    to 2000 MVA at 420 kV or 550 kV transmission voltage

    levels the better heat transmission of the GIL is an important

    advantage.

    A. Chakir and H. Koch are with Siemens AG, Power Transmission and

    Distribu tion, P. (). Box 3220, 91050 Erlangen, Germany

    (e-mad: abdelIah,chakw@ev. slemens.de, hermann.koch@ev. siemens.de)

    0-7803-7031-7/01/ 10.00 (C) 2001 IEEE

    0-7803-7173-9/01/ 10.00 2001 IEEE 162

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    o ~~

    o 20 40

    en 80 IIXJ

    120 140 160

    180

    Alw@ (degreas)

    Fig. 2. Nusselt number distribution of the inner cylinder calculated with

    different wall function in comparison to e~perimental data presented by

    Temperatures for the Angles 60, 70, 60

    1

    ~

    0

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    Fig. 5b. Measur ing points

    TABLE 2 EXPERIMENTAL RESULTS FOR CASE 2 AND 3

    E : ~

    Ra=2,1 10 Ra=l,7 10

    case 2

    case 3

    Positio inner cylinder outer cylinder

    inner cylinder outer cylinder

    n of the T(K) T(K) T(K)

    T(K)

    sensor

    o

    325.56 (point 309,16 (point 3 ;3.46 (point 335.96 (point

    90 1)

    2) 1) 2)

    180 325.06 (point 311.96 (point

    3: 2.86 (point 339.96 (point

    3) 4) 3) 4)

    325.46 (point 313.36 (point 353.36 (point 341.86 (point

    5 6 5)

    5

    Heat

    flux 101.8

    110.5

    (Wlm2

    TABLE 3 COMPARISON OF NUMERICAL AND EXPERIMENTAL

    (

    &sa

    Angle r) experiment Equilibrium

    The calculations are made for a constant heat flux

    101.8 W/m, 110.5 W/m applied at the inner cylinder obtained

    from the experiments and with a temperature constant at outer

    cylinder, which is the average value of the three values above

    (311 .5K, 339.3 K). The numerical results are presented in

    the Tab. 2. The calculation was carried out with radiation be-

    tween the two cylinders.

    The same numerical results are obtained with the Van Drist

    and Spalding model [3]. They arc slightly over the value

    obtained with the Equilibrium model. The calculated

    temperature clifference between top and the middle is over

    than 5,

    however the experimental difference is not

    significant. One can explain the constant value of temperature

    at the inner cylinder in the experiment by the more important

    conduction heat phenomena in the wall of inner cylinder than

    the convection phenomena at the boundary layer.

    This is shown by the Biot number resistance in the wall

    (Bi= a

    =0.02), i.e., the conduction heat is

    JCY,inde, I

    Lo

    much smaller than the convection heat resistance. The Nusselt

    number at the inner and outer cylinder for the three wall

    function are presented in fig. 5 for case 2. The inner cylinder

    is at a constant heat flux. In the outer cylinder the Nusselt

    number increase sharply from the bottom till the horizontal

    plan (90 )where remain constant until the region near the top.

    For the inner cylinder the temperature decrease slowly from

    angle 0 till angle 160 at which an inversion increase the

    Nusseh value to the one at OO. The equilibrium model

    presents an increased Nusselt-number, while the Spalding and

    Van Drist [4] models presents a decrease (fig. 5). This

    phenomena of Nusselt-number decrease for Spalding and Van

    Drist models appear only for high Ra number (see fig. 1: Ra =

    2,5 10). Both wall function Spalding and Van Drist seem not

    good for high turbulence. The numerical results obtained with

    the equilibrium model presents the best agreements with the

    experiment values (Tab 3). So the calculation for the second

    experiment are made only with this model and results of

    temperatures for inner cylinder are presented in Tab. 4

    TABLE 4 COMPARISON OF NUMERICAL AND EXPERIMENTAL

    RESULTS (CASE 3)

    (Case 3) Ra=l,7 10 inner cylinder

    k

    ngle ()

    o

    90

    180

    7 -

    experiment I Equilibrium model

    T(K) T(K)

    353.3

    361.4

    352.7

    354.6

    353.2 I 360.8

    OUTER CYUNDER

    .

    l

    Eqlb

    60

    +

    S@ldlm

    -c-

    Van Dnst

    m-

    =40-

    zsc-

    20-

    o ~~

    o 20 40 60 S6 100

    120 140

    160

    180

    Angle (degrees)

    Fig. 5 . Nusselt number distribution of the outer cylinder calculated with

    different wa ll function for a h igh Rayle igh number (case 2)

    Three different studies were made to examine mainly the

    effects of a Rayleigh number variation on the convection heat

    transfer at the inner and outer cylinder (fig. 6, 7). The

    temperature was constant at both cylinders. The radiation

    was not considered. The Rayleigh number reach from 2,5e6

    to 4,2e9, the other parameter are nearly constant at R+=2,5

    and PI=0,7 (case 1,4,5).

    0-7803-7031-7/01/ 10.00 (C) 2001 IEEE

    0-7803-7173-9/01/ 10.00 2001 IEEE 165

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    V. CONCLUS1ON

    An investigation of turbulent natural convection in a

    horizontal concentric annulus wa:s carried out for high

    Rayleigh numbers up to Ra=l O1. T he results were presented

    in form of temperatures and Nusselt numbers at the inner and

    outer cylinder. The numerical results were compared with

    experimental data. Three different wall functions were used

    to find an accarate model. There were no effects noticeable

    for a low tttrlbulent flow. The differences to the achieved

    Nusselt results of Goldstein were small. The maximum

    temperature deviation was 15Yo.

    The equilibrium model shows the best results compared to the

    carried out experiment. The temperatures of the middle inner

    cylinder were nearly equal. However, high differences

    appeared at the top/bottom of the cylinder. This were the

    results of the much smaller heat resistance in the wall than the

    convective resistance. The calculated temperatures at the

    inner cylinder had a uniform trend except the top and bottom,

    where they were rising to the highest values at 0 and 180

    The Nusselt number as a function of Rayleigh showed the

    high dependency. The increasing heat convection for high

    Rayleigh numbers occurred especially in the middle part of

    the cylinders and in the top of the outer one.

    The temperatures in the center of the annulus became

    constant for higher turbulence. The temperature gradient at

    the wall boundary layers was rising. The trend for high

    turbulence is going to small thermal boundary layer at the

    inner and outer cylinder with uniform temperatures at the

    annulus center.

    [1]

    [2]

    [3]

    [4]

    [5]

    VI. REFERENCES

    T.H. Kuebn und R.J. Goldstein, An experimental and theoretical

    study of nataral convection in the annulus between horizontal

    concentric cyl inders, J Fhrid Mech. 74, 695-719(1976).

    T. H. Kuehn, R. J. Goldstein, An experimental study of natural

    convection heat transfer in concentric and eccentric horizontal

    cylindrical annu li, ASME J. Heat Transfer 100,635-640 (1978).

    B. E. Launder, D. B. Spalding, The numerical computation of

    torbulent flows, Computer methods in applied mechanics and

    engineering Vol. 3,269-289 (1974).

    E. R. van Drist, On Turbulent Flow Near a Wall, Journal of the

    Aeronautical Sc iences, vol. 23, 1956, p. 1007

    Fluid flow, Ansys Theory Reference release 5.4, chap.7, pp 7.1 - pp

    7-39 (1996)

    VII. BIOGRAPHIES

    Institute was f in ished with

    Dr.-hrg. Hermann Koch was born in

    November 1954 in Hauswarz, Germany.

    From 1976-1979 he studied Electrical

    Engineering at the Fachhochschtde Riissels-

    heim, where he graduated with the d ip loma of

    eng ineering (D ipl.-lng.). From 1980-1981 he

    studied on a Ftdbright Scholarship at New

    Jersey Institute of Techno logy, Newark, New

    Jersey, USA. From 1981-1986 he studied

    Electrica l Engineering at the Technical Uni-

    versity of Darrnstadt, where he graduated with

    the diploma of engineering (Dipl.-Ing.). His

    continued research work at the High Voltage

    his doctoral work about Partial Discharges in

    Low Voltage Equipment and the degree of Dr.-hrg. Since 1990 he is

    working with Siemens High Voltage Division where he ia head of Gas

    Insulated Lines Department. He is committee member of the IEEE Power

    Engineering Society in the Gas Insulated Substat ion Committee. In the IEC

    he is Secretary of Technical Subcommittee SC I 7C and in CENELEC he is

    Secretary of the Technical Commi ttee TC 17.

    in research and development

    Insulated Substations.

    Dr.-lng. Abdellah Chakir was born 1965

    in Casablanca, Morocco. He received his

    Dipl. Ing. und M. SC. degrees in

    mechanical and aeronautical engineering in

    1990 from ENSMA (Ecole Nationale

    Superieure de

    M4canique et

    dA&otechnique de Poitiers, France) and

    received the Ph. D. degree in Mechanics in

    1993 from Poitiers University, France.

    From 1993-1996 he was Auxiliar Professor

    in mechanical engineering at the

    Polytechnic Institute and ISACE of

    Guarda, Portugal . S ince 1996 he is working

    with Siemens High Voltage Division, Gas-

    0-7803-7173-9/01/ 10.00 2001 IEEE 167