fatigue of bolted connections

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    Fatigue Failure of Bolted Connections

    by: Chris Meisl

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    Presentation Outline

    The Fatigue Process Sequence of Fatigue Failure

    Behavior of Fatigue Loading

    S-N Curves

    Factors Affecting Fatigue

    Bolted Connections in Tension Location of Failure

    Preloading and Contact Area

    Prying Action

    Bolted Connections in Shear

    Preloading

    Stress Concentration and FailureLocations

    Anchor Bolts

    Design Codes

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    What is Fatigue?

    Caused by the repeated application

    of loads that are not large enough to

    cause failure in a single application.

    Generally caused by repeated

    cycles of tensile loading.

    Failure occurs suddenly.

    Fracture surface of a paper clipbroken by ~6 cycles of repeated

    bending (80 X)

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    Stages of Fatigue Failure

    Failure will only occur if the

    following essential conditions are

    present:

    Cyclic tensile loads

    Stress levels above a threshold

    value Flaw in the material

    Stages of fatigue failure:

    1. Crack initiation

    2. Crack growth

    3. Crack propagation

    4. Final rupture

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    Behaviour of Fatigue Loading

    The fatigue life = the number of

    repeated cycles of loading (N) that

    a material will undergo before it

    fails.

    Higher the fatigue stress level, the

    fewer number of loading cyclesrequired to cause failure.

    Major factors that effect fatigue

    life:

    1. Shape of the connection

    2. Magnitude of stress variations

    3. Mean stress level

    4. Choice of materialS-N Curve for varying magnitude

    of altering stress

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    Bolted Connections in Tension Failure Locations

    Crack is initiated at areas of high stress concentrations.

    Potential failure sites:

    a. Head-shank transition

    b. Run-out of thread

    c. Thread at nut

    Failure is most likely to occur at the first engagement of the threads ofthe bolt and nut.

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    Bolted Connections in Tension Influences

    The magnitude of the load on the

    bolt depends on:

    1. The magnitude of the externaltension load.

    2. The bolt-to-joint stiffness ratio(K

    B

    /KJ

    ).

    3. Whether or not the externaltension load exceeds the critical

    load required to separate the joint

    (depends on initial preloading).

    4. Location of the contact area.

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    Bolted Connections in Tension Non Preloaded Bolts

    Flange connection with non-preloaded bolts

    The external tensile force Ft applied on the connection will be transferred

    directly to the bolts, Fb.

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    Bolted Connections in Tension Preloaded Bolts

    Flange connection with preloaded bolts

    Preload decreases the load variation in the bolt, until the contact forces

    Fc are exceeded.

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    Bolted Connections in Tension Contact Area

    If the flange thickness is to

    thin bending may occur,

    leading to contact areas.

    Contact area at the centre:

    KJ > KB

    Low variation of load on boltuntil preload is exceeded.

    Contact area at edges:

    KJ < KB

    High variation of load on

    bolt.

    Contact areas located atedges are more susceptible

    to fatigue.

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    Bolted Connections in Tension Contact Area

    Contact force in centre Contact forces located at flange edges

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    Bolted Connections in Shear

    Non-Preloading

    Load transferred

    via bearing of

    bolt shank.

    Can not be used

    in variable load

    conditions.

    Preloaded:

    Load transferred

    by friction

    between plates.

    Use HSFG

    bolts.

    Can be used in

    variable load

    conditions.

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    Bolted Connections in Shear

    Non-Preloading

    Stress

    concentration at

    hole.

    Fatigue cracks

    near hole, or

    shearing of bolt.

    Preloaded:

    Low stress

    concentration

    near hole.

    Fatigue cracksat gross section

    of plate.

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    Anchor Bolts

    Behave in the same way as normal

    bolts.

    Bolt diameter and thread size has

    little effect.

    Method of forming thread influences

    fatigue strength Rolled threads better than cut due to

    residual compressive stress.

    Double nut increases fatigue

    resistance.

    Must consider prying effects.

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    Code Requirements CAN/CSA-S16.1-94

    Based on detail categories,

    number of load cycles, and the

    corresponding S-N curve.

    Considers fatigue failure to occur

    in the connecting material.

    Parameters:g = fatigue life constant [Table 4(a)]

    n = number of stress range cycles

    [Table 4(b)]

    N = number of passages of the

    moving load

    Fsrt = constant amplitude thresholdrange

    Fsrg

    nN

    1

    3

    Fsrt

    2

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    Code Requirements AISC LRFD 1999

    Based on detail categories, numberof load cycles, and the correspondingS-N curve.

    Considers fatigue failure to occur inthe connecting material and bolt.

    Parameters:

    Fsr= design stress rangeCf= constant [Table A-K3.1]

    N = number of stress range fluctuations

    Fth = threshold fatigue stress range[Table A-K3.1]

    At = net tensile area

    P = pitchdb = nominal diameter

    Shear

    Fsr Cf 327

    N

    1

    3

    Ft

    Tension

    Category E Cf= 3.9E8

    Fth = 48MPa

    Include prying effects

    At

    4db 0.9382P( )

    2

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    Design Tool Formatted Spreadsheet

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    Design Tool Formatted Spreadsheet

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    Conclusions

    Fatigue is an important

    consideration in applications

    involving repeated loading.

    Codes offer little guidance for

    fatigue of bolted connections.

    Avoid fatigue susceptible details.

    Firth of Forth Rail Bridge