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4140 Steel

Apr 05, 2018

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    Nisha Cyr i l and Al i Fa t em i , Un iversi t y o f Toledo

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    Effec t o f Sul fur on t he Durabi l i t y o fSAE4140 St eel Forgings

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    Motivation and Objectives

    Experimental Program

    Experimental Observations

    Correlations and Predictions

    Conclusions

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    A common inclusion in steels is sulfides, such as MnS.

    Up to a certain low level, MnS inclusions are desirable

    as they improve the machinability.

    Metal working processes such as rolling and forging

    result in anisotropic microstructure.

    Fatigue failures are the most common type of failures

    governed by crack nucleation and growth.

    Understanding the effects of S and S inclusions on

    fatigue behavior is of considerable interest.

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    To evaluate the effects of sulfur content and sulfideinclusions on tensile properties, impact toughness, andfatigue resistance.

    To compare the effects of sulfur content and sulfideinclusions between the longitudinal and transverse

    loading directions.

    To develop a predictive model as a function of S to

    represent fatigue behavior for loading in the transversedirection.

    OBJECTIVES

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    SAE 4140 steel at 3 Sulfur Levels

    Continuously Cast into 150 mm Square Billets

    Transverse Tests

    Cast Billets Hot Forged into 64 mm Square Bars,Normalized, and Quenched & Tempered to 43 HRC and52 HRC

    Longitudinal Tests

    Cast Billets Hot Rolled into 29.8 mm Round bars,Normalized, and Quench & Tempered to 42 HRC

    MATERIALS

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    SAE 4140 steel

    Three S levels:

    High (0.077% S)

    Low (0.012% S)

    Ultra Low (0.004% S)

    Each at two hardness levels:

    43 HRC

    52 HRC

    MATERIALS

    0.004 % S

    0.012 % S

    0.077 % S

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    MATERIALS

    Inclusions were

    primarily sulfides

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    MATERIALS

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    SPECIMENS

    EXPERIMENTS

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    Testing Program Included: Tensile tests

    Strain-controlled fatigue tests

    CVN impact tests

    Procedures and practices as

    outlined by ASTM

    Specimens cut-out from the

    transverse direction

    Some longitudinal test results

    also available

    Closed-loop servo-hydraulic

    axial load frame

    EXPERIMENTS

    TENSILE TEST

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    R TENSILE TESTRESULTS

    CVN IMPACT

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    R CVN IMPACTTEST RESULTS

    Test

    results

    at RT

    FATIGUE TEST

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    R FATIGUE TESTRESULTS AT 40 HRC

    0.10%

    1.00%

    10.00%

    1E+1 1E+2 1E+3 1E+4 1E+5 1E+6 1E+7 1E+8

    Reversals to Failure, 2Nf

    TrueStrainA

    mplitude,/2(%)

    99 Trans U Lo S 40 HRC

    80 Trans Lo S 40 HRC

    81 Trans Hi S 40 HRC

    96 Long Lo S 40 HRC

    97 Long Hi S 40 HRC

    (SS) (SS)

    FATIGUE TEST

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    R FATIGUE TESTRESULTS AT 50 HRC

    0.10%

    1.00%

    10.00%

    1E+1 1E+2 1E+3 1E+4 1E+5 1E+6 1E+7 1E+8

    Reversals to Failure, 2Nf

    TrueStrainA

    mplitude,/2(%)

    98 Trans U Lo S 50 HRC

    76 Trans Lo S 50 HRC

    77 Trans Hi S 50 HRC

    (SS) (SS)

    (SS)

    (SS)

    FATIGUE LIMIT &

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    RFATIGUE LIMIT &

    CYCLIC YIELD STRENGTH

    0

    200

    400

    600

    800

    1000

    1200

    1400

    1600

    1800

    2000

    Fatigue limit

    (40 HRC)

    Fatigue limit

    (50 HRC)

    MPa

    Hi S Trans

    Lo S Trans

    U Lo S Trans

    Hi S LongLo S Long

    Cyclic yield

    strength

    (40 HRC)

    Cyclic yield

    strength

    (40 HRC)

    FATIGUE FRACTURE

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    R FATIGUE FRACTURESURFACES

    Fish-eye on fracture surface for low S

    material at 52 HRC at long life.

    Elongated inclusions at and around the

    fracture origin for high S material at 52

    HRC at short life.

    FATIGUE FRACTURE

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    R FATIGUE FRACTURESURFACES

    Flat and rough fracture surface for high S

    material at 43 HRC at long life, resulting

    from initiation & growth of several cracks.

    Fracture surface for surface initiated failure

    of low S material at 52 HRC at long life

    showing initiation site & shear lips.

    FATIGUE CURVE

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    R FATIGUE CURVEESTIMATION

    Roessle-Fatemi Strain-Life Equation:

    For longitudinal loading condition

    Based on hardness

    Reference:

    Roessle, M. L. and Fatemi, A., Strain-controlled fatigue properties ofsteels and some simple approximations,International Journal of

    Fatigue, Vol. 22, 20002000, pp. 495-511.

    ESTIMATION CURVE

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    R ESTIMATION CURVEMODIFICATION

    Roessle-Fatemi Strain-Life Equation Modification:

    For transverse loading condition

    Based on hardness and sulfur (S) content

    Reference:N. Cyril and A. Fatemi, Experimental Evaluation and Modeling of

    Sulfur Content and Anisotropy of Sulfide Inclusions on Fatigue

    Behavior of Steels ,International Journal of Fatigue (to appear).

    ]65.0)(22.1[2

    ]09.0)(3.0[

    )2)]((25.71[191000)(487)(32.0

    )2(

    225)(25.4

    2

    +

    +

    +

    =

    S

    f

    S

    f

    NS

    E

    HBHB

    NE

    HB

    PREDICTED VS

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    R PREDICTED VSEXPERIMENTAL LIFE

    1E+1

    1E+2

    1E+3

    1E+4

    1E+5

    1E+6

    1E+7

    1E+8

    1E+1 1E+2 1E+3 1E+4 1E+5 1E+6 1E+7 1E+8

    Reversals to Failure from Experimental Data

    PredictedR

    eversalstoFa

    ilure

    77 Trans Hi S 53 HRC

    76 Trans Lo S 53 HRC

    98 Trans U Lo S 51 HRC

    81 Trans Hi S 45 HRC

    80 Trans Hi S 44 HRC

    99 Trans Hi S 42 HRC

    Life factor of 2

    Life factor of 5

    R

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    The inclusions were predominantly sulfides and for thetransverse samples the percent of sulfide area fractions werevery close to the percent sulfur weight.

    The maximum inclusion size was about the same for the lowsulfur and the ultra low sulfur materials, although the ultra low

    sulfur material had a sparser distribution of sulfides.

    Ductility and toughness reduced considerably by the increase

    in sulfur content for the transverse samples. However, thedifferences in either the yield strength or the ultimate tensilestrength for the different sulfur level materials at a givenhardness level were not significant.

    CONCLUSIONS

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    CONCLUSIONS

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    Strain-life curve at 50 HRC for the ultra low S material showedconsiderable improvement over the low S material at very shortlife, as a consequence of better ductility, while in the long liferegime the two curves were close to each other.

    At 50 HRC, there was about a factor of 30 difference in fatiguelife in LCF regime and about two orders of magnitude differencein HCF regime between the high and the ultra low S materials.

    At 40 HRC, there was about a factor of 40 difference in life inLCF and about one order of magnitude difference in HCF

    between the high sulfur and the ultra low sulfur materials.

    At 40 HRC, the strain-life curves for the ultra low and low sulfurmaterials in the transverse direction were close to each other and

    to the curves for the longitudinally loaded samples.

    CONCLUSIONS

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    CONCLUSIONS

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    The increase in hardness from 40 HRC to 50 HRC did not resultin improved HCF behavior of the high sulfur material in thetransverse direction, due to a more pronounced effect ofinclusions at higher hardness and at long life.

    The three sulfur level materials at 50 HRC exhibited sub-surfaceas well as surface failure modes at long lives, resulting inconsiderable scatter of fatigue life.

    The fracture surfaces of the high sulfur transverse material werevery rough, caused by several cracks originating from inclusions,

    propagating and merging.

    A modified model to predict strain-life curves for transverseloading based on Roessle-Fatemi equation showed good

    predictions for most of the data.

    CONCLUSIONS

    R REFERENCE

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    N. Cyril, A. Fatemi and B. Cryderman, Effects of

    Sulfur Level and Anisotropy of Sulfide Inclusions on

    Tensile, Impact, and Fatigue Properties of SAE 4140Steel, SAE Technical Paper, SAE World Congress,

    Detroit, Michigan, April 2008.

    N. Cyril and A. Fatemi, Experimental Evaluation

    and Modeling of Sulfur Content and Anisotropy ofSulfide Inclusions on Fatigue Behavior of Steels ,

    International Journal of Fatigue (to appear).

    REFERENCEPUBLICATIONS

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    Financial Support:AISI(David Anderson)

    Bar Fatigue Committee: Chaired by Tom Oakwood

    Heat Treatment: Chrysler (Peter Bauerle)

    Residual Stresses: Cummins Engine (Steve Ferdon)

    ACKNOWLEDGEMENT

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    w w w . a u t o s t e e l . o r g

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    Great Designs in Steel is Sponsored by:

    AK Steel Corporation, ArcelorMittal, Nucor Corporation,

    Severstal North America Inc. and United States Steel Corporation