Deep Drawing Steels

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    G. Ubertalli - 01/2011

    The tensile test

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    stress strain curve

    of a deep-drawing

    steel.

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    STRAIN HARDENING

    When a metallic material overcomes the yield strength and it enters

    in the plastic field, the lattice planes slip as a consequence of the

    dislocations movement. After a first ste of lanes sli , the number of

    the dislocations increase and they start to interfere each other (jog)

    inducing a pile up.

    In such a condition, the load necessary to continue to deform the

    material increases, as evidenced in the stress-strain curve.

    Therefore, when a metallic material is deformed, it manifests a

    higher strength.

    This phenomenon is called:

    STRAIN HARDENING

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    STRAIN HARDENING COEFFICIENT nThe behaviour in the plastic zone can be described in a simplified way from the

    Hollomon equation:

    = n

    The n coefficient ranges from 0 to 1.

    If it is 0, the equation is:

    = K

    So deformation without strain hardening (brittle crack).

    ,

    = K

    In this case there is a straight line with a rate equal to K (infinite toughness).

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    RELATIONSHIP BETWEEN AND nP = A

    At Pmax dP=0=dA + dA d/ = -dA/A (eq.1)

    V=AL= cost dV=0=dAL + AdL dA/A = -dL/L = -d (eq.2)

    Thus combinin e .1 and e .2 it can be obtained:

    d/d = In case of plastic strain the equation is:

    = Kn

    and substituting:

    n-1 = nAnd then:

    n = This mathematical relationship indicates that it is possible tohave a material with high strain , if such material has a high n.

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    ERIKSEN TEST

    a

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    THE COEFFICIENT OF ANISOTROPY r1

    3In the tensile test is normallydetected the

    1strain. If

    2and

    3

    are also measured , the ratio 2/

    3

    = = =

    .

    constant for every material and is

    indicated with the rletter; it is called

    COEFFICIENT OF ANISOTROPY

    0b

    b

    2

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    0a

    a

    Typical values of cold drawn steels

    STEEL Rp02(MPa)

    Rm

    (MPa)

    E (%) r

    avg.

    n

    avg.

    E.I. L.D.R.

    FeP01 220280 300410 2833 1.01.2 0.180.20 9.510 2.192.23

    FeP04 180210 270350 3842 1.51.9 0.200.22 10.511 2.232.31

    FeP06 160200 270340 4044 1.92.2 0.220.24 1112.2 2.312.44

    High 275500 400650 1530 0.91.1 0.150.19 79 1.82.2

    strength

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    DEEP DRAWING AND HIGH STRENGTH STEELS

    A deep drawing steel must have high toughness and ductility properties (toguarantee the deformability in the die) and good strength properties (to ensure

    high properties in use). Generally if there is an increase of strength properties a

    decrease in deformability is observed; instead in this case the increase or

    mechanical properties in directly connected to deforming process. These

    materials have therefore the double advantage to be particularly deformable

    during deep drawing process and increase their mechanical properties when are

    in use.

    Traditionally and for a long time were used for this purpose (and actually too) low

    carbon and Ti steel: the ferritic matrix of these steels can guarantee a good

    deformability, while the deep drawing can induce the strain hardening.

    In automotive company, the aim is the weight reduction to reduce fuel

    consumption. For this reason the market has imposed the use of different

    materials, which adopt alternative strengthening mechanism, maintaining good

    deformability. As a consequence, reduced depth can be used without reducing the

    in use affordability.

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    MILD STEEL. Traditional not alloyed steel with low carbon (C

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    INTERSTITIAL FREE. Traditional not alloyed steel with low carbon and Tihigher than 0,3%. The titanium has high attitude for carbide and nitride formation. The

    C and N content in solid reduction is therefore reduced, favouring the ferrite existence

    and the cold forming operations.

    The increase of mechanical properties in a consequence of the strain hardening.

    e

    X500 in orig. X3000 in orig

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    BAKE HARDENING. Not alloyed steel coil with low C percentage produced

    adopting parameters (chemical composition, roll ing temperature, annealing) toreduce carbides precipitation at room temperature and to increase it at the

    cataphoresis process temperature. High deformability in cold forming and an

    increase of mechanical properties during the cook of painting, induced from a fine

    carbide precipitation.

    Steel BH 220 after heat treatment at 180 C for 20 min.

    A fine presence of carbides in ferrite is detected.

    X500 in orig. X3000 in orig

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    MICROALLOYED or HSLA: Steel coil with low C percentage and Vand Nb (min. 0.015%) as alloying elements. These elements form fine

    precipitates at grain boundary (carbides and nitrides), induce fine grains

    formation and an enhancing of the strength.

    FeE355

    Steel FeE355 high amount of carbides (Nb) and a very fine grain size.

    X500 in orig. X3000 in orig.

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    DUAL PHASE: Steel with ferrite (good deformability) and almost 15% ofmartensite phase.

    Fe600DP

    Fig. 69 microstructure of a Dual Phase steel;

    coarse martensite area. In Fig. 70 the

    mar ens e s omogeneous y s r u e .

    The Fig. 71 is a magnification of Fig. 70.

    X500 in orig.Fig.69

    X500 in orig. X3000 in orig.Fig 70 Fig 71G. Ubertalli - 01/2011

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    TRIP: Coil steel with ferritic/bainitic/austenitic structure (it guarantee good cold

    forming). During deformation a percentage of energy is used to transform a certain

    amount of metastable austenite in martensite; this phase enhance the mechanical

    properties while the residual austenite acts as energy absorber in case of violent

    deformation (impact).

    Fe800 TRIP F

    In the microstructure it is difficult

    to distinguish the austenite from

    ferrite phase.G. Ubertalli - 01/2011

    MULTIPHASE: High strength steel with ferritic / bainitic /martensitic structure(high martensite content).

    Fe800MP

    MARTENSITIC: Steel characterized with very high martensite percentage.

    .

    Fe1300MS

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    SHEET METAL FORMING

    A schematic section of a typical stamping die. The sheet

    contacts only the punch or the die at any point. Membrane

    stresses stretch the sheet over the tools.

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    SHEET METAL FORMING

    A

    C C

    In order to analysed the deformability of the sheet of a

    metallic material, a network mesh is painted on

    undeformed surface. If a circle is painted, after

    deformation three possible conditions can be obtained:

    ,

    the plane of the foil. In this case the circle is deformed as in Fig. a.

    A schematic section of a typicalstamping die.

    A: Punch - B: Die

    C: Blank-Holder - D: Blank

    BDONE DIRECTION DEFOMATION, if the sheet is deformed in one

    direction only (Fig. b).

    DRAWING, if the sheet have a positive (in a direction) and a negative (in

    a perpendicular direction) deformation (Fig. c).

    e1>0 e1>0 e1>0a b c If d and d are res ectivel the diame-

    e2>0 e2=0 e20, while the

    sign of e2 depends on the deformationtype.

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    SHEET METAL FORMING

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    A schematic plot of the window of safestraining for simple paths the forming-

    limit diagram. With an isotropic material,

    the limits for 2>1 mirror those in the

    region where 1>2.

    Strain signatures along lines A to

    J and A to E in a rectangular pan.

    NAKAZIMA TEST

    The Nakazima test proposes to induce, on

    a metallic material to be deformed, all the

    possible types of deformations (from

    stretching to deep drawing). A punch with

    a spherical shape is adopted to deform

    a

    e1>0

    e2>0

    Original

    circle Deformed

    a

    samples of controlled geometry until the

    necking appearance or until the starting

    crack of material. The first sample has

    square geometry and the blank-holder on

    the four sides.

    The result is evidenced in image a. The

    other sample have one dimension that is

    progressively reduced, to increase the

    c

    bc r c e

    e1>0

    e2=0

    c

    deep drawing effect. The different samplesand results are reported in Figs. (a-e).

    The image e evidences a deep drawing

    effect of 100%. The circles evidence the

    deformation in the different samples.

    e

    de1>0

    e2

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    1,5

    2

    2,5

    e1

    CURVE LIMITE DI FORMABILITA'

    SAFE STRAINING CURVESample a

    Sample b

    Sample c

    Sample d

    Sample e

    SAFE STRAINING CURVE

    In figure are reported all the coupled

    values obtained in many samples afterthe Nakazima tests. (e1 VS e2 ).

    The line that connects the upper points is

    0

    0,5

    -0,5 -0,3 -0,1 0,1 0,3 0,5

    e2 EXPERIMENTAL POINTS

    TEST OF NAKAZIMA

    called SAFE STRAINING CURVE.

    The right side of the diagram is the

    stretching zone (e2 > 0), while the left

    side is the deep drawing zone (e2 < 0).

    The safe strainin curve SSC de end from the thickness are a,

    characteristic of every material and are well known or can be easily

    detected.

    They are very useful to designer to choose the more appropriate material

    for the different component, also from the point of view of the

    deformability.

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