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Al cu melting and aging

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    Casting and Heat Treatment of AL-4%Cu Alloy

    Abstract:

    Copper has been the most common alloying element almost since the

    beginning of the aluminum industry, and a variety of alloys in which copper

    is the major addition were developed.

    In the cast alloys the basic structure consists of cored dendrites of aluminum

    solid solution, with a variety of constituents at the grain boundaries or

    interdendritic spaces, forming a brittle, more or less continuous network of

    eutectics. Wrought products consist of a matrix of aluminum solid solution

    with the other soluble and insoluble constituents dispersed within it.

    Introduction:

    Use of aluminium castings in automobiles has increased from nonstructural

    demanding, as it is the case of cylinder heads and engine blocks, to

    structural parts, such as suspension struts due to the bene!cial e"ects that

    arise by combining light weight and mechanical properties. #he re$uirements

    for such structural parts are internal soundness, integrity, high strength and

    toughness, and, as result of this, %l&Cu cast alloys are considered to be ideal

    candidates. #he parameter that exerts the highest in'uence on the levels of

    strength and internal $uality re$uired is the solidi!cation rate( as the

    microstructure of the material is re!ned when solidi!cation proceeds at a

    higher rate. % further advantage of microstructural re!ning, when dealing

    with aluminium alloys susceptible for heat treating, is the enhancement in

    their mechanical properties( as particles formed during solidi!cation will be

    smaller and will re$uire less time to dissolve during heat treating )*+.

    Experimental rocedure:

    !" and mold was prepared of known specimen.#"#he weighed amount of %l - Cu were taken as per calculated

    theoretically.$" %l was melted in pit furnace.

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    4" %fter achieving %l in molten form, Cu was introduced in the form

    of Cu wire." Cu starts dissolving into the melt.&" olid degassing was done in order to remove all entrapped gases

    to get sound casting.'" lag was removed mechanically.(" %fter achieving a uniform melt of %l/Cu alloy , it was casted

    into sand mold.)" %fter solidi!cation di"erent samples were obtained and heat

    treated , there procedure is also discussed.

    *luxes and +egassers used in Al Casting:

    +i,culties in Al elting:#he main di0culties in %l melting are porosity, blow holes and gas

    absorption.

    +rossing: 1olten oxide product of metal is called dross.

    .as Absorption: olubility of gases in the molten metal is known as gas

    absorption.

    #he following reactions take place during the melting of aluminum(

    2%l 3 4526 7 %l2643 452

    8%l 3 4C627 2%l2643 %lC4

    9%l 3 4C6 7 %l2643 %lC4

    9%l 3 4627 %l2643 %l24

    :rossing will be more in case of pit furnace melting than induction melting.

    %s it is obvious from the above reactions that C6 - C62 is source for :ross

    formation and it will be available in ;it furnace due to burning of . :ross formation always must be kept minimum. #here is 8?>?/ %l in

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    dross that@s why dross comes on top surface otherwise sink. #hese kind of

    inclusions are detrimental to mechanical properties.

    52 gas is soluble in considerable amount in the molten %l. %s the

    temperature of molten metal increases the amount of 52 solubility alsoincreases. 6n solidi!cation 52 solubility decreases and result in the

    formation of pin holes and blow holes.

    Hydrogen /emo0al:

    :issolved hydrogen levels can be reduced by a number of methods, the most

    important of which is 'uxing with dry, chemically pure nitrogen, argon,

    chlorine, and freon. Compounds such as hexachloroethane are in common

    use( these compounds dissociate at molten metal temperatures to providethe generation of 'uxing gas.

    *lux:

    % chemical substance used to re!ne metals by combining with impurities to

    form a molten mixture that can be readily removed.

    +egasser:

    % chemical substance used to remove gas from li$uid metal.

    *luxing of Aluminum Alloys:

    Aluxes for melting aluminum are solid substances Bcommonly mixtures of

    chloride and 'uoride salts used in aluminum foundries in order to reduce the

    melt oxidation, minimiDe penetration of the atmospheric 5ydrogen, absorb

    nonmetallic inclusions suspended in the melt, keep the furnaceEladle wallclean from the built up oxides, decrease the content of aluminum entrapped

    in the dross, remove hydrogen dissolved in the melt, provide aluminum grain

    re!ning during olidi!cation, modify silicon inclusions in silicon containing

    alloys, oxidiDe excessive magnesium.

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    Common practice of 'ux introduction is manual application.

    1ost of the 'uxes are applied on the melt surface and stirred into the melt.

    ome of the 'uxes Bdegassing, grain re!ning are plunged to the bottom by a

    clean preheated perforated bell.

    Aluxes may also be introduced into the melt by injection in form of a powder

    in an inert gas B%rgon or

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    +rossing *luxes:

    :rossing 'uxes promote separation of molten aluminum entrapped in the

    dross Bsometimes up to 8?/. Gesides chlorides and 'uorides drossing 'uxes

    contain oxidiDing component BF

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    +egassing:

    Jemoval of dissolved gases from the li$uid metal is known as degasing.

    :egassing of molten %luminum alloys is a foundry operation aimed to

    remove 5ydrogen dissolved in the melt.

    5ydrogen in aluminum

    :egassing by 'uxes

    Jotary degasser

    In the case of diatomic gases such as 52, 62, or

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    Mi$uid aluminum actively dissolves hydrogen, which forms as a result of

    chemical reaction with water vaporK

    2%l 3 4526 N %l264 3 95

    olubility of gaseous hydrogen in li$uid aluminum at its melting point

    B*22?.=OAE99?.OC is ?.9* in4Elb B2.2 cm4 per *?? g.olubility of gaseous

    hydrogen falls sharply when aluminum solidi!esK solid aluminum at melting

    point contains only ?.?* in4Elb B?.? cm4 per *?? g.

    #herefore aluminium alloys release excessive amount of hydrogen during

    olidi!cation. #his results in porosity defects distributed throughout the solid

    metal. iDe of the hydrogen pores and their $uantity is determined by the

    initial content of hydrogen, the alloy composition and the solidi!cation

    conditions.

    5ources of ydrogen in molten aluminum:

    atmosphere humidity(

    wet metallic charge(

    wet furnace lining Bcrucible, transfer ladles(

    wet foundry instruments(

    wet 'uxes and other consumables(

    furnace fuel combustion products containing hydrogen.

    Heat Treatment 6f Al-4%Cu Alloy:

    Precipitation hardening, or age hardening, provides one of the most widely used mechanisms for

    the strengthening of metal alloys. The fundamental understanding and basis for this technique

    was established in early work at the U. S. Bureau of Standards on uralumin.

    The importance of theoretical suggestion for the development of new alloys is clear from the

    historical record. !t the end of the "#th century, cast iron was the only important commercial

    alloy not already known to western technology at the time of the $omans. %hen age hardening

    of aluminum was discovered accidentally by %ilm, during the years "#&' ("#"", it quickly

    became an important commercial alloy under the trade name uralumin.

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    The strength and hardness of some metal alloys may be enhanced by the formation of e)tremely

    small uniformly dispersed second(phase particles within the original phase matri) in a process

    known as precipitation or age hardening. The precipitate particles act as obstacles to dislocation

    movement and thereby strengthen the heat(treated alloys. *any aluminum based alloys, copper(

    tin, certain steels, nickel based super(alloys and titanium alloys can be strengthened by age

    hardening processes.

    +n order for an alloy system to be able to be precipitation(strengthened, there must be a terminal

    solid solution that has a decreasing solid solubility as the temperature decreases. The !l(u

    -uralumin is an aluminum alloy of /// group0 phase diagram shown in 1igure " shows this

    type of decrease along the solvus between the 2 and 234 regions. onsider a #5wt6!l 7 8wt

    6u alloy which is chosen since there is a large degrease in the solid solubility of solid solution

    2 in decreasing the temperature from 99&: to ;9:.

    Figure 1:The aluminum rich end of the !l(u phase diagram showing the three steps in the age(

    hardening heat treatment and the microstructures that are produced.

    +n an attempt to understand the dramatic strengthening of this alloy, Paul . *erica and his

    coworkers studied both the effect of various heat treatments on the hardness of the alloy and the

    influence of chemical composition on the hardness. !mong the most significant of their findings

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    was the observation that the solubility of u!l in aluminum increased with increasing

    temperature.

    !lthough the specific phases responsible for the hardening turned out to be too small to be

    observed directly, optical e)amination of the microstructures provided an identification ofseveral of the other phases that were present. The authors proceeded to develop an insightful

    e)planation for the hardening behavior of uralumin which rapidly became the model on which

    innumerable modern high(strength alloys have been developed.

    They summari

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    precipitated particles or go around them. By restricting dislocation movement during

    deformation, the alloy is strengthened.

    Age Hardening Precipitation.The strongest aluminum alloys -))), 5))) and ;)))0 are

    produced by age hardening. ! fine dispersion of precipitates can be formed by appropriate heat

    treatment.

    ! general model for decomposition is given, followed by details of the precipitation sequences in

    8 specific alloy systems= !l(u, !l(u(*g, !l(*g(Si and !l(?n(*g. The !l(u system is used

    as the main e)ample of decomposition, i.e.

    a& -SSSS0@ AP

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    "& nm diameter copper(rich plates on E"&&F!l planes. These develop into AP

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    Figure 2: Microstructure of Al-4%cu Alloy solution treated at 580oC

    for 2 hours, at 100 , etched in !"#A$ reagent

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    Figure : Microstructure of Al-4%cu Alloy solution treated at 580oC

    for 2 hours, at 200 , etched in !"#A$ reagent

    Figure 4: Microstructure of Al-4%cu Alloy solution treated at 580oC

    for 2 hours, at 400 , etched in !"#A$ reagent

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    Figure 5: Microstructure of Al-4%cu Alloy Arti&cial Aged at 180oC for

    1 hours, at 100 , etched in !"#A$ reagent

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    Figure ': Microstructure of Al-4%cu Alloy Arti&cially aged at 180oC

    for 1 hours, at 200 , etched in !"#A$ reagent

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    Figure (: Microstructure of Al-4%cu Alloy Arti&cially aged at 180oC

    for 1 hours, at 400 , etched in !"#A$ reagent

    /eferences

    *.CharacteriDation of an %l&Cu cast alloy ,1.%. #alamantesilvaa, %.

    JodrPgueDb, Q. #alamantesilvab, . Laltierrab, Jafael ColRsa, a Aacultad de

    IngenierPa 1ecRnica y SlTctrica, Universidad %utnoma de A, 99* an


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