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    Chapter 6 and 7

    Metals and heat treatment

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    Adapted from Fig. 10.28, Callister &

    Rethwisch 3e.(Fig. 10.28 adapted

    from Binary Alloy Phase Diagrams,

    2nd ed., Vol. 1, T.B. Massalski (Ed.-in-Chief), ASM International, Materials

    Park, OH, 1990.)

    Adapted from Fig.

    13.1, Callister &

    Rethwisch 3e.

    Classification of Metal AlloysMetal Alloys

    Steels

    Ferrous Nonferrous

    Cast Irons

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    Ferrous alloy: Those which iron is the primeconstituent

    Low carbon steel:

    Properties: Carbon content less than 0.25 wt%, Soft

    and ductile

    Applications: Automobile body, Pipe line, Building,Bridge

    Medium carbon steel: Properties: Carbon content 0.25 wt% to 0.60 wt%,

    Low hardenabilities

    Applications: Railway wheels and tracks, Gears

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    High carbon steel:

    Properties: Carbon content 0.6 wt% to 1.4 wt%, Hardest,strongest, less ductile among the carbon steel

    Applications: Knives, Razors, Hacksaw blades

    Stainless steel: Properties: At least 11 wt% Cr. May be other elements (Ni,

    Mo) can be added for high corrosion resistance

    Applications: Automobile exhaust components, Chemical and

    food processing equipment.

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    Types of Cast Iron (cont.)White iron

    < 1 wt% Si

    pearlite + cementite

    very hard and brittle

    Malleable iron

    heat treat white iron at 800-900C

    graphite in rosettes reasonably strong and ductile

    Adapted from Fig.

    13.3(c) & (d),

    Callister &

    Rethwisch 3e.

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    Types of Cast Iron (cont.)Compacted graphite iron

    relatively high thermal conductivity

    good resistance to thermal shock

    lower oxidation at elevated

    temperatures

    Adapted from Fig. 13.3(e),

    Callister & Rethwisch 3e.

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    Limitations of Ferrous Alloys

    1) Relatively high densities

    2) Relatively low electrical conductivities

    3) Generally poor corrosion resistance

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    9Based on discussion and data provided in Section 13.3, Callister & Rethwisch 3e.

    Nonferrous Alloys

    NonFerrousAlloys

    Al Alloys

    -low r: 2.7 g/cm3

    -Cu, Mg, Si, Mn, Zn additions-solid sol. or precip.

    strengthened (struct.aircraft parts

    & packaging) Mg Alloys

    -very low r: 1.7g/cm3

    -ignites easily-aircraft, missiles

    Refractory metals-high melting Ts-Nb, Mo, W, Ta Noble metals

    -Ag, Au, Pt-oxid./corr. resistant

    Ti Alloys

    -relativelylowr:4.5g/cm3

    vs 7.9 for steel-reactiveathighTs-space applic.

    Cu Alloys

    Brass:

    Zn is subst. impurity(costume jewelry, coins,corrosion resistant)Bronze: Sn, Al, Si, Ni aresubst. impurities(Dental equipment,

    landing gear

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    10

    Metal Fabrication

    How do we fabricate metals?

    Blacksmith - hammer (forged)

    Cast molten metal into mold

    Forming Operations

    Rough stock formed to final shape

    Hot working vs. Cold workingDeformation temperature

    high enough for

    recrystallization

    Large deformations

    Deformation belowrecrystallization

    temperature

    Strain hardening occurs

    Small deformations

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    FORMING

    roll

    Ao

    Adroll

    Rolling (Hot or Cold Rolling)

    (I-beams, rails, sheet & plate)

    Ao Ad

    force

    die

    blank

    force

    Forging (Hammering; Stamping)

    (wrenches, crankshafts)

    often at

    elev. T

    Adapted from

    Fig. 14.2,

    Callister &

    Rethwisch 3e.

    Metal Fabrication Methods (i)

    ram billet

    container

    container

    forcedie holder

    die

    Ao

    Adextrusion

    Extrusion

    (rods, tubing)

    ductile metals, e.g. Cu, Al (hot)

    tensileforce

    Ao

    Addie

    die

    Drawing

    (rods, wire, tubing)

    die must be well lubricated & clean

    CASTING MISCELLANEOUS

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    FORMING CASTING

    Metal Fabrication Methods (ii)

    Casting- mold is filled with molten metal

    metal melted in furnace, perhaps alloying elements added, then

    castin a mold common and inexpensive

    gives good production of shapes

    weaker products, internal defects

    good option for brittle materials

    MISCELLANEOUS

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    Sand Casting

    (large parts, e.g.,

    auto engine blocks)

    Metal Fabrication Methods (iii)

    What material will withstand T>1600Cand is inexpensive and easy to mold?

    Answer: sand!!!

    To create mold, pack sand around form(pattern) of desired shape

    Sand Sand

    molten metal

    FORMING CASTING MISCELLANEOUS

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    Stage IMold formed by pouringplaster of paris around wax pattern.

    Plaster allowed to harden.

    Stage IIWax is melted and then

    poured from moldhollow moldcavity remains.

    Stage IIIMolten metal is poured

    into mold and allowed to solidify.

    Metal Fabrication Methods (iv)

    FORMING CASTING MISCELLANEOUS

    Investment Casting

    (low volume, complex shapes

    e.g., jewelry, turbine blades)

    wax I

    II

    III

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    Metal Fabrication Methods (v)

    Continuous Casting

    -- simple shapes

    (e.g., rectangular slabs,

    cylinders)

    molten

    solidified

    FORMING CASTING MISCELLANEOUS

    Die Casting

    -- high volume

    -- for alloys having low melting

    temperatures

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    MISCELLANEOUSCASTING

    Metal Fabrication Methods (vi)

    Powder Metallurgy

    (metals w/low ductilities)

    pressure

    heat

    point contactat low T

    densificationby diffusion athigher T

    area

    contact

    densify

    Welding

    (when fabrication of one large

    part is impractical)

    Heat-affected zone:

    (region in which the

    microstructure has been

    changed).

    Adapted from Fig.

    14.3, Callister &

    Rethwisch 3e.

    (Fig. 14.3 from Iron

    Castings

    Handbook, C.F.

    Walton and T.J.

    Opar (Ed.), 1981.)

    piece 1 piece 2

    fused base metal

    filler metal (melted)base metal (melted)

    unaffectedunaffectedheat-affected zone

    FORMING

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    Summary of Possible TransformationsAdapted from

    Fig. 11.37,

    Callister &Rethwisch 3e.

    Austenite (g)

    Pearlite(a+ Fe3C layers + a

    proeutectoid phase)

    slowcool

    Bainite(a+ elong. Fe3C particles)

    moderatecool

    Martensite(BCT phase

    diffusionlesstransformation)

    rapidquench

    TemperedMartensite(a+ very fine

    Fe3C particles)

    reheat

    Strength

    Ductility

    MartensiteT Martensite

    bainitefine pearlite

    coarse pearlitespheroidite

    General Trends

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    Annealing: Heat to Tanneal, then cool slowly.

    Based on discussion in Section 14.5, Callister & Rethwisch 3e.

    Thermal Processing of Metals

    Types of

    Annealing

    Process Anneal:

    Negate effects ofcold working by(recovery/

    recrystallization)

    Stress Relief: Reducestresses resulting from:

    - plastic deformation- nonuniform cooling- phase transform.

    Normalize (steels): Deformsteel with large grains. Then heattreat to allow recrystallizationand formation of smaller grains.

    Full Anneal (steels):Make soft steels forgood forming. Heatto get g, then furnace-cool

    to obtain coarse pearlite.

    Spheroidize (steels):Make very soft steels forgood machining. Heat just

    below Teutectoid& hold for

    15-25h.

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    a) Full Annealing

    b) Quenching

    Heat Treatment Temperature-Time Paths

    c)

    c) Tempering(Tempered

    Martensite)

    P

    B

    A

    A

    a)b)

    Fig. 11.26,

    Callister &

    Rethwisch 3e.

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    Hardenability -- Steels Hardenability measure of the ability to form martensite

    Jominy end quench test used to measure hardenability.

    Plot hardness versus distance from the quenched end.

    Adapted from Fig. 14.5,

    Callister & Rethwisch 3e.

    (Fig. 14.5 adapted from

    A.G. Guy, Essentials of

    Materials Science,

    McGraw-Hill Book

    Company, New York,1978.)

    Adapted from Fig. 14.6,

    Callister & Rethwisch 3e.

    24C water

    specimen(heated to g

    phase field)

    flat ground

    Rockwell Chardness tests

    Hardness,

    HR

    C

    Distance from quenched end

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    The cooling rate decreases with distance from quenched end.

    Adapted from Fig. 14.7, Callister &

    Rethwisch 3e. (Fig. 14.7 adapted from H.

    Boyer (Ed.)Atlas of Isothermal

    Transformation and Cooling

    Transformation Diagrams, American

    Society for Metals, 1977, p. 376.)

    Reason Why Hardness Changes with Distance

    distance from quenched end (in)Hardness,

    HRC

    20

    40

    60

    0 1 2 3

    600

    400

    200A M

    0.1 1 10 100 1000

    T(C)

    M(start)

    Time (s)

    0

    0%

    100%

    M(finish)

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    Hardenability vs Alloy Composition Hardenability curves for

    five alloys each with,

    C= 0.4 wt% C

    "Alloy Steels"

    (4140, 4340, 5140, 8640)

    -- contain Ni, Cr, Mo

    (0.2 to 2 wt%)-- these elements shift

    the "nose" to longer times

    (from A to B)

    -- martensite is easier

    to form

    Adapted from Fig. 14.8, Callister &

    Rethwisch 3e. (Fig. 14.8 adapted from

    figure furnished courtesy Republic SteelCorporation.)

    Cooling rate (C/s)

    Hardness,

    HR

    C

    20

    40

    60

    100 20 30 40 50Distance from quenched end (mm)

    210100 3

    4140

    8640

    5140

    50

    80

    100

    %M4340

    T(C)

    10-1

    10 103

    1050

    200

    400

    600

    800

    Time (s)

    M(start)

    M(90%)

    BA

    TE

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    Effect of quenching medium:

    Medium

    air

    oil

    water

    Severity of Quench

    low

    moderate

    high

    Hardness

    low

    moderate

    high

    Effect of specimen geometry:

    When surface area-to-volume ratio increases:

    -- cooling rate throughout interior increases

    -- hardness throughout interior increases

    Positioncenter

    surface

    Cooling ratelow

    high

    Hardnesslow

    high

    Influences of Quenching Medium & Specimen

    Geometry