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    Weld Design andWeld Design andSpecificationSpecification

    Jim Glancey, PEJim Glancey, PE

    Depts. of Depts. of BioresourcesBioresources EngineeringEngineering& Mechanical Engineering& Mechanical Engineering

    University of DelawareUniversity of Delaware [email protected] [email protected]

    http:// http:// udel.edu/~jglanceyudel.edu/~jglancey

    I cant explain everything . . .I cant explain everything . . .

    4 in

    6 in

    1000 ft

    Inside weld entire length

    1/4

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    Factors in Weld DesignFactors in Weld Design

    II Strength (static and/or fatigue)Strength (static and/or fatigue)II Material and the effects of heatingMaterial and the effects of heatingII CostCostII DistortionDistortionII Residual StressesResidual Stresses

    II Easy to WeldEasy to Weld

    Static StrengthStatic Strength

    I Stress - strain diagram

    Strain ( ) =

    Stress ( )

    =F

    A

    LL

    yield ultimate(tensile)

    F

    F

    A

    L

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    Shear StrengthShear Strength

    I In general, material fails in shear due todistortion (at a molecular level)

    I Criteria for failure: Ductile: Shear Strength ~ 0.5 Tensile Strength Brittle: Shear Strength ~ 0.75 Tensile Strength

    I Weld strength analysis is generally based on

    Shear Strength

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    Static Strength of WeldsStatic Strength of Welds

    F F Normal =

    Shear =

    Fw * h

    Fw * h

    2FF

    F

    1/8

    75 o3/8

    1/4 Max Normal =

    Max Shear =

    F0.618w * h

    F0.707w * h

    Butt

    Fillet

    h = throat size!

    Weld Size vs. Throat SizeWeld Size vs. Throat Size

    1/8

    75 o3/8

    h = plate thickness = weld size

    Butt

    h = 0.707 * plate thickness0.707 * weld size

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    Fillet

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    Fatigue StrengthFatigue Strength

    Cycles of Loading

    FatigueStrength

    1000 1,000,0001

    EnduranceLimit

    Static Tensile Strength

    LowCycle

    HighCycle Infinite

    Life

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    Endurance LimitEndurance Limit

    II For Steel:For Steel: Endurance Limit = 0.5 * Tensile StrengthEndurance Limit = 0.5 * Tensile Strength

    or 100or 100 kpsikpsi , which ever is lower., which ever is lower.

    II For Aluminum:For Aluminum: No endurance limit (cannot have an infinite No endurance limit (cannot have an infinite

    life)life)

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    Factors for Fatigue Stress AnalysisFactors for Fatigue Stress Analysis

    Type of Weld Stress Increase

    Butt Weld 1.2Transverse Fillet 1.5

    Parallel Fillet 2.7

    T-butt with corners 2.0

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    Strength ConsiderationsStrength Considerations

    I Try to minimize the stresses in welds; makethe parent materials carry highest stresses.

    I Butt welds are the most efficientI Avoid stress concentrationsI Intermittent weld length should be at least 4

    times the fillet sizeI Minimize weld size to reduce potential for

    fatigue failure

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    Effects of Welding on MetallurgyEffects of Welding on Metallurgy

    II Depends on the alloy and welding processDepends on the alloy and welding processII In general, cracking is promoted by:In general, cracking is promoted by:

    stress concentrationsstress concentrations

    brittle parent material after welding (lowbrittle parent material after welding (lowcarbon steels)carbon steels)

    hydrogen in the weld metalhydrogen in the weld metal

    impurities in the weld metalimpurities in the weld metal

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    Reducing DistortionReducing Distortion

    I Prevent overweldingI Intermittent weldingI Minimize number of passesI Place welds near the neutral axis of the partI Balance welds around the neutral axis

    I Anticipate shrinkage forcesI Residual stress relief

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    Neutral AxisNeutral Axis

    II The line (plane) where bending stresses areThe line (plane) where bending stresses arezero.zero.

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