Autofrettage in Pressure Vessels

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    Autofrettage in pressure

    vessels

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    Residual stress analysis of Autofrettaged thick-walledspherical pressure vessel

    Results are obtained by developing an extension of variable materialproperties (VMP) method ( Find out the Autofrettaged stress and strains byusing the formula).

    • By performing a parametri study! the optimum autofrettage pressure andorresponding autofrettage per ent for reating desirable residual stress

    state are introdu ed and determined.•

    "he modi# ation ma$es VMP method appli able for analyses of spheri alvessels based on a tual material behavior both in loading and unloadingand onsidering variable Baus hinger e%e t.

    • &n addition! the optimum pressure for autofrettage of the spheri al pressurevessels made of A' and *B' steels is dis ussed here.

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    Residual stress analysis of Autofrettaged thick-walledspherical pressure vessel

    Boundary conditions:

    The maximum applied working pressure for A723 steel. the maximum internal pressure without causingyielding! is

    The yield strength of A723 steels are considered ""3#$%a.

    +,- MPa

    outer radius/inner radius+

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    Residual stress analysis of Autofrettaged thick-walledspherical pressure vessel

    • &y using the 'ame(s e)uations for calculating the hoop stress* radial stress* along thethickness of the cylinder* when the ends of the cylinder are open and unconstrained so that thecylinder is in a condition of plane stress.

    • "he radial displa ement is

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    Residual stress analysis of Autofrettaged thick-walledspherical pressure vessel

    Calculation of autofrettage pressure (Pa):0et 1n2 be denoted as the ratio of operating pressure to yield stress.

    0et 1m2 be the ratio of Autofrettaged radius to inner radius

    3in e! the value of autofrettaged radius 4as not found! an e5uation

    4hi h gives a relation bet4een 1n2 and 1m2 4as used to found thevalue of 1m2 based on von Misses riterion.

    + .,-

    -.,-

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    Residual stress analysis of Autofrettaged thick-walledspherical pressure vessel

    +67 MPa

    Determination of autofrettaged radius (ρ)

    Calculation of maximum von-Mises stress (σvon-max)

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    F8M A9A0:3&3

    ;A< Model and F8 model=

    Slno

    Speci cations value

    -

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    Bi and Multi linear stress strainurve=

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    Boundary ondition

    Pressure is applied ,- MPaA : axis free! Both !C axis #xedB axis free! Both :!C axis #xed

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    linear isotropi Results=•

    Pressure is applied for - y le.

    • 85uivalent stress=

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    axial stress*oop stress

    Radial stress

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    Bilinear isotropi Results=•

    Pressure is applied for - y le.

    • 85uivalent stress=

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    *oop stressAxial stress

    Radial stress

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    Bilinear isotropi Results=•

    Pressure is applied for ' y le.

    • 85uivalent stress=

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    *oop stressAxial stress

    Radial stress

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    Bilinear isotropi Results=•

    Pressure is applied for ' y le 4ithD extra.

    • 85uivalent stress=

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    *oop stressAxial stress

    Radial stress

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    Bilinear isotropi Results=•

    Pressure is applied for ' y le 4ith?D extra.

    • 85uivalent stress=

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    *oop stressAxial stress

    Radial stress

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    Multi linear isotropiResults=

    Pressure is applied for - y le.

    • 85uivalent stress=

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    Axial stress*oop stress

    Radial stress

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    Multi linear isotropiResults=

    • Pressure is applied for ' y le 4ithautofrettage .

    • 85uivalent stress=

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    Axial stress*oop stress

    Radial stress

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    Multi linear isotropiResults=

    • Pressure is applied for ' y le 4ith Dautofrettage .

    • 85uivalent stress=

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    Axial stress*oop stress

    Radial stress

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    Multi linear isotropiResults=

    • Pressure is applied for ' y le 4ith ? Dautofrettage .

    • 85uivalent stress=

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    Axial stress*oop stress

    Radial stress

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    ;on lusion• "he residual stress distribution indu ed in autofrettaged spheri al

    pressure vessels made of A' steels! based on their a tual

    behavior in loading and unloading 4as evaluated by numeri almethod (Bilinear and multilinear analysis).• &t 4as investigated that usage of isotropi hardening model in

    analysis leads to signi# ant overestimation in residual hoop stress.• "he autofrettage per ent by 4hi h high ompressive and relatively

    lo4 tensional hoop residual stress are simultaneously attainablenear the inner and outer radii of the vessel 4as introdu ed as theoptimum per entage of autofrettage.

    • &t 4as observed that in the ase of A' spheri al vessel 4ithradius ratio of ! by in reasing autofrettage per ent up to ? D!the inner ompressive hoop residual stress de reases and the

    outer hoop tensional stress gradually in reases (Both in bilinearand multilinear analysis.