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  • Study Committee B2Technical Advisory Group B2-AG-06

  • CIGR B2-AG-06 Seminar Bangkok

    TutorialTutorial

    Conductor FatigueConductor Fatigue

    Louis Cloutier ConvenorLouis Cloutier, ConvenorAndr Leblond, Secretary

    CIGR WG B2.30 "Engineering Guidelines Relating to Fatigue Endurance Capability of Conductor/Clamp Systems"

    F b 28 2011February 28, 2011 CIGR 2011

  • Outline of PresentationOutline of Presentation

    Introduction Examples of Conductor Fatiguep g Typical Conductor Configurations Some Characteristics of Suspension Clamps CIGRE Technical Brochures CIGRE Technical Brochures Prediction of Aeolian Vibration Amplitudes

    Conductor Profile During Aeolian Vibrations Field Measurements of Conductor Vibrations Analytical Representation of the Fatigue Phenomenon

    Laboratory Fatigue Tests Resonant Type Test Benches Fatigue Endurance Data

    Vibration Measurement Analysis Case Study Conductor and Clamp Types Lacking Fatigue Data

    Study Committee B2 - Technical Advisory Group B2-AG-06 32011-02-28

    Conclusion

  • Introduction (I)Introduction (I) Aeolian vibrations :

    Small vibration amplitudes exceeding rarely the conductor diameter; frequency range : 3 to 150 Hz; winds : 1 to 7 m/s May lead to fatigue failure of conductor strands at suspension clamps

    Such failures are caused by dynamic stresses resulting from reverse bendingfrom reverse bending

    Other wind-induced conductor motions such as wake-induced oscillations and galloping may also be responsible

    Study Committee B2 - Technical Advisory Group B2-AG-06 42011-02-28

    for fatigue conductor strand failures

  • Introduction (II)Introduction (II)

    Natural vibrations are not sinusoidal but show beatsbeats

    Examples :

    Study Committee B2 - Technical Advisory Group B2-AG-06 52011-02-28

  • Examples of Conductor Fatigue (I)Examples of Conductor Fatigue (I)

    Conductor fatigue occurs when wind-induced vibration is not controlled

    Fretting fatigue has long been recognized as being the cause of strand failures in outer as well as inner layers of the conductors

    Steel core can fail by overheating after aluminum layers are Steel core can fail by overheating after aluminum layers are separated

    Interstrand microslip amplitude increases, small cracks are t d d t t l t t d f il

    Study Committee B2 - Technical Advisory Group B2-AG-06 62011-02-28

    generated and some propagate up to complete strand failures

  • Examples of Conductor Fatigue (II) Strand failures occur mainly at

    suspension clamps where such

    Examples of Conductor Fatigue (II)

    p psingular conditions are created

    To a lesser extent, a similar phenomenon can occur at damper

    phenomenon can occur at damper, marker or spacer clamps

    Early detection of conductor failure i k f f il ( tt ti t

    or risk of failure (attentiveness to early warnings)

    Wear and failure of conductor strands due to spacer clamp loosening

    Fatigue usually takes many years

    Study Committee B2 - Technical Advisory Group B2-AG-06 72011-02-28

    Fatigue usually takes many years to become apparent

  • Typical Conductor Configurations (I) An important component of an overhead power line

    The conductor cost is up to about 40% of total capital investment

    Typical Conductor Configurations (I)

    The conductor cost is up to about 40% of total capital investment

    The conductor size is chosen to suit electrical and mechanical requirements

    The most common conductor type is ACSR (Aluminum Conductor Steel Reinforced)

    The ratio of steel to aluminum areas vary widely The ratio of steel to aluminum areas vary widely

    Study Committee B2 - Technical Advisory Group B2-AG-06 82011-02-28

  • Typical Conductor Configurations (II)Some Special Conductors

    Typical Conductor Configurations (II)

    Trapezoidal Z-shaped compact Self-damping Expanded

    Ri i d t River crossing conductor

    Study Committee B2 - Technical Advisory Group B2-AG-06 92011-02-28

  • Some Characteristics of Suspension Clamps (I)Some Characteristics of Suspension Clamps (I) Most of the conductor fatigue

    test results refer to those bt i d h th d tobtained when the conductor

    is supported in a short metallic clamp

    The ideal profile of the clamp The ideal profile of the clamp body follows the natural curvature of the conductor

    The ends of the clamp body The ends of the clamp body and the keeper must be rounded to avoid indenting the conductor

    The clamp should be able to rotate in a longitudinal vertical plane to accommodate

    t i l l d

    Study Committee B2 - Technical Advisory Group B2-AG-06 102011-02-28

    asymmetrical loads

  • Some Characteristics of Suspension Clamps (II)

    A i i

    Some Other Suspension ClampsSome Characteristics of Suspension Clamps (II)

    Armor grip suspension (AGS) Elastomeric bushing with

    cage of preformed rodscage of preformed rods Metal clamp with

    elastomeric insertSpecial river crossing clamp Special river crossing clamp Long saddle to reduce

    contact stress

    Study Committee B2 - Technical Advisory Group B2-AG-06 112011-02-28

  • CIGRE Technical Brochures (I)CIGRE Technical Brochures (I)

    This TB covers a state of the art review on the following aspects of the problem :the following aspects of the problem :

    Fretting behaviour in stranded conductor Determination of fatigue endurance Determination of fatigue endurance

    capability Inner conductor mechanics Assessment of vibration severity on actual

    lines Evaluation of conductor residual life

    This TB covers the determination of possible damage and ways to predict remaining life of conductors as well as new methods to t t d t / l t

    Study Committee B2 - Technical Advisory Group B2-AG-06 122011-02-28

    test conductor/clamp systems

  • CIGRE Technical Brochures (II)This TB is a complement to TB 332, which was a state of the art review :

    CIGRE Technical Brochures (II)

    Meant to be a reference for the practicing line engineer in the application of the latest technology

    Reviews the available design tools to achieve engineering solutions

    Identifies the inherent gaps in their li tiapplication

    Gives the engineer a better comprehension of the two related phenomena Fatigue of conductors Aeolian vibrations

    This TB includes a review of those design tools and gives the

    Study Committee B2 - Technical Advisory Group B2-AG-06 132011-02-28

    g gtransmission line engineer the limits to their application

  • Prediction of Aeolian Vibration AmplitudesPrediction of Aeolian Vibration Amplitudes

    Many utilities have their own design rules (for number of dampers) based on past experiencedampers) based on past experience

    Vibration severity can also be measured on existing lines A useful analytical approach is the "Energy Balance

    Principle" (EBP)Principle (EBP) The EBP leads to an estimate of conductor vibration

    amplitude based on equating the energy input from the wind with the energy absorption (damping) of thewind with the energy absorption (damping) of the conductor and dampers

    The EBP can also be used for the direct design of the damping system for a new linedamping system for a new line

    The estimate of the expected vibratory motion from EBP is considered an upper bound and is therefore a safe value Conditions can also be assessed through measurements on

    Study Committee B2 - Technical Advisory Group B2-AG-06 142011-02-28

    Conditions can also be assessed through measurements on existing lines

  • Conductor Profile During Aeolian VibrationsConductor Profile During Aeolian Vibrations

    Parameters describing conductor vibration include:

    Bending amplitude Yb, Free loop amplitude ymaxb maxBending angle , Wave length and Loop length

    This representation applies to metal clamps, not to

    Study Committee B2 - Technical Advisory Group B2-AG-06 152011-02-28

    elastomer lined clamps

  • Field Measurements of Conductor Vibrations (I)

    Several methods to measure the vibration intensity of a conductor

    Field Measurements of Conductor Vibrations (I)

    vibration intensity of a conductor have been employed

    The bending amplitude Yb method finally comes out as the most

    It measures the differential displacement of the conductor at 89 mm from the last point of contact with the clamp

    ypractical

    p p The reverse bending amplitude was presented as an alternative

    to permit the installation of the vibration recorder directly onto the conductor

    The bending amplitude method must be properly interpreted when cushioned clamps are used

    Recommended by IEEE in 1966 (also in the 2007 revision) and

    Study Committee B2 - Technical Advisory Group B2-AG-06 162011-02-28

    CIGRE SC22 WG04 1979 and SC22 WG11 TF02 1995

  • Field Measurements of Conductor Vibrations (II)Field Measurements of Conductor Vibrations (II)

    HILDAOntario Hydro RecorderTVM 90

    Pavica Ribe LVRVibrec 400

    Study Committee B2 - Technical Advisory Group B2-AG-06 172011-02-28

    Scolar III

  • Analytical Representation of the Fatigue Phenomenon (I)

    a YpdE2

    H

    a yt ca ep ese tat o o t e at gue e o e o ( )

    ( ) bpxaa Ypxe p+= 14 EIHp =An idealized bending stress in the top-most outer-layer strand (in the plane of the last point of contact) is calculated from the bending amplitude (Poffenberger-Swart formula)

    Ea: modulus of elasticity of outer wire material (N/mm2)

    d: diameter of outer layer wire (mm)

    ( )H: conductor tension at average temperature during test period (N)

    EI: sum of flexural rigidities of individual wires in the cable (Nmm2)

    x: distance from the point of measurement to the last point of contact between the

    Study Committee B2 - Technical Advisory Group B2-AG-06 182011-02-28

    x: distance from the point of measurement to the last point of contact between the clamp and the conductor

  • Analytical Representation of the Fatigue Phenomenon (II)

    fymEd =

    a yt ca ep ese tat o o t e at gue e o e o ( )

    maxaa fyEIEd

    The idealized bending stress can be derived from the free loop amplitude, ymax, which is the vibration parameter often measured in indoor test spans

    Ea: Youngs modulus for the outer-layer strand material (N/mm2)

    d: diameter of outer layer wire (mm)

    f: frequency of the motion (Hz)f: frequency of the motion (Hz)

    m: conductor mass per unit length (kg/m)

    EI: sum of flexural rigidities of individual wires in the cable (Nmm2)

    Study Committee B2 - Technical Advisory Group B2-AG-06 192011-02-28

    g ( )

  • Analytical Representation of the Fatigue Phenomenon (III)

    Fatigue of conductors is due to microslip movements of wires inducing fretting fatigue

    a yt ca ep ese tat o o t e at gue e o e o ( )

    fretting fatigue The phenomenon is complex and its exact

    modelling has yet to be completed Contact areas between round strands Contact areas between round strands

    are elliptical Fretting and microslip occur in these contact areas Fatigue cracks develop out of these contact areas The knowledge on fatigue performance of conductors mostly

    relies on results of laboratory tests made on conductors in fixed short metallic clampsshort metallic clamps It is not possible at the moment to determine the fatigue endurance of a

    conductor alone There is a wide diversity of design and geometry of conductors

    Study Committee B2 - Technical Advisory Group B2-AG-06 202011-02-28

    y g g yand supports

  • Laboratory Fatigue Tests Resonant Type Test BenchesLaboratory Fatigue Tests Resonant Type Test Benches

    Constant amplitude excitation Measurement of the bending Pneumatic tensioning systemDynamometer Suspension clamp g

    amplitude Yb and/or the free loop amplitude ymax

    Most tests done with conductors supported in short metallic clampsSlider

    DynamometerAmplitude measuring system

    Rubber dampers

    Wire break detectionVibrator

    End clamp

    Turnbuckle

    5.5 deg.supported in short metallic clamps

    Clamps usually held in a fixed position on the test bench

    Active length : 7 m2 m 2 m

    Study Committee B2 - Technical Advisory Group B2-AG-06 212011-02-28

  • Fatigue Endurance Data* (I)

    The results of fatigue tests ultimately lead to the presentation of a fatigue (S N) curve

    Fatigue Endurance Data (I)

    a fatigue (S-N) curve Note scatter in the data The endurance limit is determined

    at 500 megacyclesat 500 megacycles Idealized bending stress relative to

    Yb vs megacycles to failure Endurance limits Endurance limits

    22.5 MPa for single-layer ACSR 8.5 MPa for multi-layer ACSR

    *R f EPRI O B k

    Study Committee B2 - Technical Advisory Group B2-AG-06 222011-02-28

    *Ref.: EPRI Orange Book

  • Fatigue Endurance Data (II)Estimated bending amplitude endurance limits

    Fatigue Endurance Data (II)

    Study Committee B2 - Technical Advisory Group B2-AG-06 232011-02-28

  • Vibration Measurement Analysis (I)Vibration Measurement Analysis (I)

    Rule of Thumb Approach to Interpreting Fatigue Data (IEEE)

    Widely used set of empirical criteria (Guide for Aeolian Vibration Field Measurements of Overhead Conductors,

    1368 200 )IEEE P1368, 2007) The bending amplitude may exceed the endurance limit

    during no more than 5% of total cyclesduring no more than 5% of total cycles No more than 1% of total cycles may exceed 1.5 time

    the endurance limit No cycle may exceed 2 times the fatigue endurance limit

    Study Committee B2 - Technical Advisory Group B2-AG-06 242011-02-28

  • Vibration Measurement Analysis (II)Multi-Layer ACSR Fatigue Endurance Data

    Vibration Measurement Analysis (II)

    Statistical analysis S-N curves without wire

    f ilfailure Average 95% probability of survivalp y

    Study Committee B2 - Technical Advisory Group B2-AG-06 252011-02-28

  • Vibration Measurement Analysis (III)

    Based on Cumulative d th (Mi

    Vibration Measurement Analysis (III)

    damage theory (Miners rule)

    Total damage D at several stress levels i cumulates linearly:

    D = n /ND = ni/Ni Failure is predicted when

    D n /N 1D = ni/Ni =1 The accuracy of the resulting

    estimate of lifetime is between 50% d 200%

    Study Committee B2 - Technical Advisory Group B2-AG-06 262011-02-28

    50% and 200%

  • Case Study (I)Report evaluated on 02/05/2002

    Transmission line Circuit 3002

    Case Study (I)

    Voltage (kV)Conductor typeLocation of measurementTerrainSpan length (m)

    315ACSR PheasantTower 313 facing Tower 312Flat348 4Span length (m)

    Recorder (Type and No.)Remarks

    348.4PAVICA n 5P02Installation date : November 21, 2001 @ 0C

    First measurement atLast measurement atDuration of one measurement (s)Measurement cycle time (s)

    21/11/2001 18:0024/02/2002 18:0010900

    Total duration of measurement (s)Factor for extrapolation to one yearTotal number of measurements taken

    91200345.7899120

    Study Committee B2 - Technical Advisory Group B2-AG-06 272011-02-28

  • Case Study (II)Fatigue Endurance Limit Approach

    12

    PAVICA

    Case Study (II)

    10

    P

    a

    )

    PAVICAFatigue endurance limit

    6

    8

    l

    a

    t

    i

    v

    e

    t

    o

    Y

    b

    ,

    (

    M

    P

    4

    P

    S

    s

    t

    r

    e

    s

    s

    r

    e

    l

    0

    2

    Study Committee B2 - Technical Advisory Group B2-AG-06 282011-02-28

    0 10 20 30 40 50

    Frequency, (Hz)

  • Case Study (III)Cumulative Damage Approach

    12

    Case Study (III)

    10P

    a

    )

    5% S-N curve50% S-N curve95% S-N curveAccumulated stress curve per year

    6

    8

    a

    t

    i

    v

    e

    t

    o

    Y

    b

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    s

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    a

    0

    2

    Study Committee B2 - Technical Advisory Group B2-AG-06 292011-02-28

    0.01 0.1 1 10 100 1000 10000 100000 1000000

    N = Accumulated megacycles per year

  • Case Study (IV)

    Evaluation of remaining lif ti D 1

    1400

    Case Study (IV)

    lifetime, D=1 There is a 86%

    probability that the 1000

    1200

    e

    ,

    (

    y

    e

    a

    r

    s

    )

    remaining lifetime exceeds 20 years 600

    800

    i

    n

    i

    n

    g

    l

    i

    f

    e

    t

    i

    m

    e

    200

    400R

    e

    m

    a

    0 10 20 30 40 50 60 70 80 90 100

    Probability of survival, (%)

    0

    Study Committee B2 - Technical Advisory Group B2-AG-06 302011-02-28

  • Case Study (V)

    Assessment of the t d i

    55

    60

    65Case Study (V)

    most damaging frequencies

    Helpful for 4045

    50

    ) Helpful for choosing the right damping system

    25

    30

    35

    F

    r

    e

    q

    u

    e

    n

    c

    y

    ,

    (

    H

    z

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    10

    15

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    25

    0 4 8 12 16 20 24 28

    0

    5

    10

    Study Committee B2 - Technical Advisory Group B2-AG-06 312011-02-28

    0 4 8 12 16 20 24 28

    Damage share, (%)

  • Conductor and Clamp Types Lacking Fatigue Data

    The extrapolation of fatigue data available to other types of conductors or to different types of support is not recommended

    Conductor and Clamp Types Lacking Fatigue Data

    conductors or to different types of support is not recommended

    Bending amplitude method is valid only for armored or unarmored conductors fitted with solid metal-to-metal clamps

    Not valid for cushioned clamps (armored or unarmored) Little test data for conductors except ACSR and aluminum alloys Some data for ACSR conductors with armor rods There is a need for more published data on conductor fatigue

    Study Committee B2 - Technical Advisory Group B2-AG-06 322011-02-28

  • Some Important Recent Contributions

    Guide for Aeolian Vibration Field Measurements of Overhead Conductors, IEEE P1368, 2007 (a revision of

    Some Important Recent Contributions

    , 3 , (IEEE 1966 Report)

    Transmission Line Reference Book, Wind Induced Conductor Motion, Second Ed. EPRI 2007 (Chapter 3, , ( p ,Fatigue of Overhead Conductors), a revision of the 1979 Orange Book

    Fatigue Endurance Capability of Conductor/Clamp g p y pSystems Update of Present Knowledge, CIGRE TF B2.11.07, TB No. 332, October 2007

    Engineering Guidelines Relating to Fatigue Endurance g g g gCapability of Conductor/Clamp Systems, CIGRE WG B2.30, TB No. 429, October 2010

    Study Committee B2 - Technical Advisory Group B2-AG-06 332011-02-28

  • Conclusion

    Fatigue endurance capability of conductors is a very useful

    Conclusion

    parameter at the design stage as well as for a maintenance program Aeolian vibrations and conductor fatigue are both highly complex

    phenomena

    So far, design tools proposed are a good example of the engineering approach to solve a complex problemg g pp p p

    Adequate determination of the fatigue characteristics of a conductor/clamp system is very important in the design of a line Acceptable level of conductor vibrations Acceptable level of conductor vibrations Determination of safe design tensions

    Future work is needed to better understand the importance of many other parameters

    Study Committee B2 - Technical Advisory Group B2-AG-06 342011-02-28

    many other parameters

  • CIGRE WG B2 30

    Members : L Cloutier (Convenor) A Leblond (Secretary) U

    CIGRE WG B2.30

    Members : L. Cloutier (Convenor), A. Leblond (Secretary), U. Cosmai, P. Dulhunty, M. Ervik, D.G. Havard, D. Hearnshaw, H.J. Krispin, M. Landeira, P. Mouchard, K. Papailiou, D. Sunkle, B. WareingWareing

    Corresponding Members : J.A. Arajo, H. Argasinska, J.M. p g j , g ,Asselin, O. Cournil, G. Diana, K. Halsan, C.B. Rawlins, R. Stephen, P. Timbrell

    Associated Experts : T. Alderton, J. Duxbury, A. Goel, C. Hardy, A. Laneville, A. Manenti Diana, S. Pichot, T. Sepp, P. Van Dyke

    Study Committee B2 - Technical Advisory Group B2-AG-06 352011-02-28

  • Speaker's Contact InformationSpeaker s Contact Information

    Andr Leblond, Ph.D., Eng.

    Tel: 1-514-879-4100 ext. 5734Tel: 1 514 879 4100 ext. 5734Fax: 1-514-879-4855E-Mail: [email protected]

    Address :85, rue Ste-Catherine Ouest, 2nd floorMontreal QuebecMontreal, QuebecH2X 3P4CANADA

    Study Committee B2 - Technical Advisory Group B2-AG-06 362011-02-28

  • Thank you !Thank you !

    QUESTIONSQUESTIONS

    Study Committee B2 - Technical Advisory Group B2-AG-06 372011-02-28