presentacion del aluminio

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    Aerospace Materials

    Fundamentals of the Structure of Metals

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    Behaviour and Manufacturing Properties

    of Material

    Behaviour and Manufacturing Properties of Material

    Structure of the

    material

    Mechanical

    Properties

    Physical and Chemical

    Properties

    Property

    Modification

    Atomic Bonding

    Crystalline

    Amorphous

    PartiallyCrystalline

    Polymer Chain

    Strength

    Ductility

    Elasticity

    Hardness

    Fatigue

    Creep

    Toughness

    Fracture

    Density

    Melting Point

    Specific Heat

    Thermal and ElectricalConductivity

    Magnetic Properties

    Oxidation

    Corrosion

    Heat Treatment

    Precipitation Hardening

    Annealing

    Tempering

    Surface treatment

    Alloying

    Reinforcements

    Composites

    Laminates

    Fillers

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    Atomic Structure and Interatomic

    Bonding

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    Periodic Table

    Why is so important to understand the periodictable?

    It classifies the elements according to their electron

    configuration.

    Each column or group have similar valence electronstructures, as well as chemical and physical properties.

    The elements situated on the right-hand side of the

    table are electronegative. They accept electrons to

    form negatively charged ions, or sometimes they shareelectrons with other atoms

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    Chemical Bonding

    An understanding of many of the physical properties

    of materials is predicated on a knowledge of the

    interatomic forces that bind the atoms together.

    Three different types of primary or chemical bondare found in solids: IONIC, COVALENT, ANDMETALLIC

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    Chemical Bonding

    Ionic BondAtoms of a metallic

    element easily give up their

    valence electrons to thenonmetallic atoms

    Covalent BondStable electron configurations

    are assumed by the sharing of

    electrons between adjacentatoms

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    Chemical Bonding Metallic bondingis found in metals and

    their alloys. Metallic materials haveone, two, or at

    most, three valence electrons.

    These valence electrons are not bound

    to any particular atom in the solid and are

    more or less free to driftthroughout theentire metal.

    They may be thought of as belonging to

    the metal as a whole, or forming a sea

    of electronsor an electron cloud.

    The remaining nonvalence electrons and

    atomic nuclei form what are calledion

    cores,which possess a net positive

    charge equal in magnitude to the total

    valence electron charge per atom.

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    Crystal Structures

    Atoms situated in repeating or periodic array

    All metals, many ceramics and certain

    polymers form crystal structures

    Hard sphere model, unit cells. For metals,

    three simple crystal structures:

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    BCC

    Metallic Crystal Structures

    Body-centered cubicChromium, iron,

    tungsten, as well as

    several other metals.

    Face-centeredcubiccopper, aluminum,silver, and gold

    FCC

    Hexagonal close-packed

    The HCP metals includecadmium, magnesium,titanium, and zinc.

    HCP

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    Bravais

    Lattices

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    Lattice Parameter Relationships

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    Lattice Parameter Relationships

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    Assignment 2

    Define and give some examples of these differentstructures:

    Amorphous

    Partially Crystalline

    Polymer Chain Define and explain the different tests needed to

    obtained the materials mechanical properties.

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    Solidification of Polycrystalline Material

    Diagram of the various

    stages in the solidificationof a polycrystalline material

    (square grids depict unit

    cells):

    a) Small crystallite nuclei.

    b) Growth of thecrystallites.

    c) Upon completion of

    solidification, grains

    having irregular shapes

    have formed.d) The grain structure as it

    would appear under the

    microscope.

    a) b)

    c) d)

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    Solidification of Polycrystalline Material

    Single crystals have periodic, repeated atomic

    arrangement and this can be also produced

    artificially under controlled conditions.

    More common is polycrystalline structures,composed of small crystals or grains.

    Generally, rapid cooling produces smaller

    grains and slow cooling larger grains.

    At room temperature, large grains generally

    low strength, hardness and ductility.

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    Microstructure of Common Materials

    Cartridge brass

    - grain boundaries

    - annealing twinsStructure in 1045 steel: Ferrite (light) +

    pearlite (lamellar)

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    Anisotropy

    The physical properties of single crystals of somesubstances depend on the crystallographic directionin which measurements are taken.

    For example, the elastic modulus, the electrical

    conductivity, and the index of refraction may havedifferent values in the [100] and [111] directions.This directionality of properties is termedanisotropy.

    Substances in which measured properties areindependent of the direction of measurement areisotropic.

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    Anisotropy

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    a) Interstitial impurity atom, b) Edge dislocation, c) Self interstitial atom,

    d) Vacancy, e) Precipitate of impurity atoms, f) Vacancy type dislocation

    loop, g) Interstitial type dislocation loop, h) Substitutional impurity atom

    Crystal Defects

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    Point Defects (lattice irregularities)

    Impede dislocation motion Vacancies form during solidification, and as

    a result of atomic vibrations. Equilibriumnumber of vacancies increases exponentiallywith temperature.

    Self interstitial is atom crowded intointerstitial void . In metals this induces large

    distortions due to high packing factors, and isnot highly probable (will exist in lowconcentrations).

    Impurities always exist. Alloys have higher"impurities"

    Solvent is host element, solute iselement in minor concentration.

    Solid solution if random, uniformdispersal of impurities.

    Substitution

    Interstitial atoms must be much smallerthan host atoms (carbon .071nm isinterstitial when added to iron .124nm,with max. concentration ~2%).

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    Line Defects (Dislocations) Dislocations motion allows sl ip(plastic deformation

    wherein interatomic bonds are ruptured and reformed). Edge dislocations allow slip at a much lower stress

    than in a perfect crystal

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    Line Defects (Dislocations)

    Dislocation motion is analogous to the movement of a

    caterpillar

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    Line Defects (Dislocations)

    Dislocation motion is analogous to the movement of a

    caterpillar

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    Line Defects (Dislocations)

    Another type of dislocation, called a screw dislocation.

    The screw dislocation derives its name from the spiral or

    helical path or ramp that is traced around the dislocation

    line by the atomic planes of atoms.

    Most dislocations found in crystalline materials areprobably neither pure edge nor pure screw, but exhibit

    components of both types; these are termed mixed

    dislocations.

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    Motion of Dislocations

    Edge Dislocation:

    Dislocation moves in

    direction of applied shear

    stress

    Screw Dislocation:Dislocation motion is

    perpendicular to applied

    shear stress

    Direction of motion of

    mixed dislocations is

    somewhere between

    parallel and perpendicular

    to the applied stress.

    Formation of a step on the surface of a crystal due to:

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    Slip

    Slip is dominant mechanism fordeformation.

    Slip occurs due to dislocation motion, and

    the slip plane is the preferred plane for

    dislocation motion.

    Slip bands are collection of parallel slip

    planes.

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    Slip lines on the surface of a

    polycrystalline specimen of

    copper which was polished and

    subsequently deformed.

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    Slip Planes

    Slip planes are those with most dense atomicpacking Metals with FCC or BCC structures have relatively large

    number of slip systems, and thus are quite ductile (plasticdeformation possible along slip systems)

    Slip systems >5 indicate ductile material

    HCP metals tend to be brittle due to few slip planes

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    Slip Planes

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    Plastic Deformation of Polycrystalline

    Materials More complicated than single crystals because direction of slip

    varies by grain.

    Strength generally increased due to tangled dislocations.

    Anisotropic behaviour (preferred orientations).

    Alteration of grain

    structure by plastic

    deformation:

    a) before: equiaxed

    grainsb) after: elongated grains

    Hot working would not

    produce elongated

    grains

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    Plastic Deformation of Polycrystalline

    Materials

    Plastic deformation of grains in

    compression (e.g. rolling, forging) Alignment along horizontal

    preferred direction

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    Slip planes

    In single crystals there are preferred planes wheredislocations move (slip planes). There they do notmove in any direction, but in preferredcrystallographic directions (slip direction).

    The set of slip planes and directions constituteslip systems.

    The slip planes are those ofhighest packingdensity.

    How do we explain this? Since the distance between atoms is shorter than the

    average, the distance perpendicular to the plane has to belonger than average. Being relatively far apart, the atomscan move more easily with respect to the atoms of theadjacent plane.

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    Slip planes

    BCC and FCC crystals have more slip systems, that is

    more ways for dislocation to propagate. Thus, those

    crystals are more ductile than HCP crystals (HCP

    crystals are more brittle).

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    Strengthening

    Size of grains influences the mechanical properties

    Generally, rapid cooling produces smaller grains and

    slow cooling larger grains

    At room temp., large grains generally low strength,

    hardness and ductility

    The ability to plastically deform depends on the

    ability ofdislocations to move, so to increase

    strength one must impede dislocation motion:

    by alloying -- introducing point defects and more grains

    by "tangling" dislocations through "working"

    by making smaller grains when cooling the melt

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    Strengthening by Grain Size Reduction

    Grain boundaries (planar

    defects) generally impededislocation motion

    more grains produce higher

    strength

    High Temperature: grains can slide against one

    another under load (creep)

    some alloying elements &

    impurities can cause

    embrittlement

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    Strengthening by Grain Size Reduction

    Grain boundaries (planardefects) generally impede

    dislocation motion

    more grains produce

    higher strength Grain boundary barrier to

    dislocation motion

    slip planes discontinuous

    slip planes have different

    orientations

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    Strengthening by Grain Size Reduction

    At High Temperature:

    grains can slide against one

    another under load (creep)

    some alloying elements &

    impurities can causeembrittlement

    Figure shows the influence of

    grain size on yield strength of

    70% Cu - 30% Zn brass alloy.

    grain diameter increases right

    to left

    scale not linear

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    Solid Solution Hardening

    Another technique to strengthen and harden metals is

    alloying with impurity atoms that go into eithersubstitutional or interstitial solid solution.

    This is called solid-solution strengthening.

    High-purity metals are almost always softer and weakerthan alloys composed of the same base metal.

    Increasing the concentration of the impurity results in anattendant increase in tensile and yield strengths, asindicated in Figures a and b for nickel in copper; thedependence of ductility on nickel concentration ispresented in Figure c.

    Dislocation movement is restricted due to lattice strainfield interactions between dislocations and these impurityatoms

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    Strain hardening

    Strain hardening is the phenomenon whereby a ductile

    metal becomes harder and stronger as it is plastically

    deformed.

    It is also called wo rk hardening, or, because the

    temperature at which deformation takes place is coldrelative to the absolute melting temperature of the metal,

    cold working.

    Most metals strain harden at room temperature.

    The price for this enhancement of hardness andstrength is in the ductility of the metal.

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    Strain hardening

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    Recovery, Recrystallization and Grain

    Growth Some of the energy from the deformation process is

    stored within the structure as STRAIN ENERGY around

    dislocations and shear zones.

    Properties such as strength, ductility, conductivity etc.

    are all affected by cold work.

    The properties may be returned to the pre-cold work

    values through the processes ofRECOVERY AND

    RECRYSTALLIZATION. This can be followed by GRAIN

    GROWTH.

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    Recovery: Internal stresses are relieved and subgrain boundaries formed

    (polygonization) in highly worked regions -- with no appreciable changein mechanical properties

    Recrystallization:

    New, strain-free grains are formed between 0.3 Tm and 0.5 Tm Depends on prior cold work (lower temp. reqd. due to stored

    energy)

    Grain Growth: Big grains are soft and low in strength (no tangled dislocations)

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    Recovery,

    Recrystallization

    andGrainGrowth

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    Recrystallization and grain growth of brass

    Cold-worked (33%CW) grain structure

    Initial stage of recrystallization after heating

    3s at 580CPartial replacement of cold-worked grains

    by recrystallized ones (4 s at 580C)Complete recrystallization (8 s at 580C)

    Grain growth after 15 min at 580C

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    Numerical Simulation of the Grain

    Growth The grain grows form small

    nuclei (shown in the 50s and

    100s in grey)

    Each color represents

    different crystallographic

    orientation.