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1/115Metallurgical Science and TechnologyVol. 29-1 - Ed. 2011

Mechanical characterization of aluminium alloysfor high temperature applications

Part1: Al-Si-Cu alloys

R. Molina, P. Amalberto - Teksid Aluminum

M. Rosso - Politecnico di Torino (Italy)

ABSTRACT

N e w c h a l l e n g e s f o r t h e A l u m i n i u m a l l o y s

u s e d f o r t h e p r o d u c t i o n o f c a s t i n g s f o r

a u t o m o t i v e e n g i n e c o m p o n e n t s a r e c o m i n g

f r o m t h e e v o l u t i o n t r e n d o f I n t e r n a l

c o m b u s t i o n e n g i n e s t o w a r d s h i g h e r s p e c i f i cp o w e r o u t p u t . C y l i n d e r h e a d s , i n p a r t i c u l a r ,h a v e t o w i t h s t a n d h i g h e r o p e r a t i n gt e m p e r a t u r e s a n d s t r e s s le v e ls . T h e p r e s e n ts t u d y i s a i m e d t o e v a l u a t e t h e m e c h a n i c a lp r o p e r t i e s a t h i g h t e m p e r a t u r e o f A l - S i - C u

a l u m i n i u m a l l o y s t r a d i t i o n a l l y u s e d f o r t h e

p r o d u c t i o n o f c y l i n d e r h e a d c a s t i n g s . T h e

o b t a i n e d r e s u l t s a r e v e r y p r o m i s i n g ,

e s p e c i a l ly f o r w h a t c o n c e r n s t h e m o d i f i e d

a l l o y s . I n f a c t , t h e r e s i s t a n c e o f b a s e A l - S i - C u

a l l o y i s f a i r l y g o o d u p t o 1 5 0 C , b u t d r o p s a t

2 5 0 C , w h i l e s o m e i n t e r e s t i n g i m p r o v e m e n t sh a v e b e e n a c h i e v e d b y m o d i f y i n g t h ec o m p o s i t i o n o f t h e b a s e a l l o y w i t h t h ea d d i t i o n o f M n a n d N i , r e s u l t i n g i n a ni n c r e a s e o f s t r e n g t h a n d d u c t i l i t y a t b o t h r o o ma n d h i g h t e m p e r a t u r e s . F u r t h e r s t u d i e s r e l a t e d

t o H i g h C y c l e F a t i g u e a n d c r e e p r e s i s t a n c e a t

h i g h t e m p e r a t u r e a r e u n d e r w a y . M o r e o v e r ,

t h e r e s e a r c h w i l l b e c o n t i n u e d a l s o

c o n s i d e r i n g o t h e r a l l o y s f a m i l i e s , l i k e A l - M g

a n d A l - C u a n d t h e r e s u l t s w i l l b e d i s c u s s e d i n

a s e c o n d p a r t o f t h e a r t i c l e .

RIASSUNTO

Con la crescente evoluzione dei motoriendotermici e il relativo aumento dellepotenze specifiche, le leghe di alluminioutilizzate per la produzione di componentiper propulsori automobilistici sono chiamatea supportare nuove sfide. In particolare leteste cilindri sono componenti che devonoresistere ad alte temperature operative elivelli di sollecitazione sempre pi elevati.Questo studio ha lo scopo di valutare lepropriet meccaniche alle alte temperaturedelle leghe di alluminio Al-Si-Cutradizionalmente utilizzate per laproduzione di teste cilindri e i risultatiottenuti sono molto promettenti, in particolarmodo per le leghe modificate mediante

appropriate aggiunte di particolarielementi. Il livello di resistenza della lega dibase Al-Si-Cu risulta soddisfacente fino a150C, ma decresce a 250C, mentreinteressanti miglioramenti sono statiriscontrati modificando la composizionechimica della lega di base con laggiunta diMn e Ni con un conseguente aumento dellepropriet di resistenza meccanica e ditenacit sia a temperatura ambiente che allealte temperature. Nellintento diraggiungere sempre pi alti livelli diresistenza sono tuttoggi in corso le

caratterizzazioni alle prove di Faticatermica ad alto numero di cicli e resistenzaallo scorrimento viscoso (creep) sempre allealte temperature. Inoltre la ricerca sarportata avanti considerando altre famigliedi leghe come Al-Mg e Al-Cu con lapubblicazione dei relativi risultati nellaseconda parte dellarticolo.

KEYWORDS

C y l i n d e r h e a d ; A l - S i - C u a l l o y s ; M e c h a n i c a l

p

r o p e r t i e s ; H i g h t e m p e r a t u r e ; M i c r o s t r u c t u r a l

e v a l u a t i o n .

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INTRODUCTION

Aluminium castings are widely used in theautomotive industry for several componentssuch as engine blocks and cylinder heads,produced in high volumes, thanks to theirfavourable combination of low weight,easy machinability, recyclability and low

cost.In the last years the evolution of internalcombustion engines has been driven mainlyby the need to meet new stringentemissions standards (like Euro 5 or futureEuro 6 in Europe) and to improve fueleconomy of the vehicles aiming to reducethe amount of CO2, which is considered a

greenhouse gas with potential effect onglobal warming, released to the ambient.The concept of Engine Downsizing, inwhich large displacement engines arereplaced by smaller, lighter more efficientunits with higher specific ratings, i.e. morepower output for unit displacement, hasbeen widely applied, for the developmentof new engine families.The increase of specific output, achievedmainly by the application of super orturbocharging and of direct fuel injectionconcepts also to spark ignited engines, hasled to a general increase of mechanicaland thermal loads on engine components.In addition, in the last ten years, alsocomponents for light and medium duty

diesel engines, which continue to gainmarket shares in Europe, have started to becast in aluminium alloys even where, due tothe high requirements on strength anddurability, cast iron was traditionally used.Consequently, also requirements for thematerials used to produce enginecomponents have grown in terms ofmechanical and fatigue resistance atoperating temperatures, ductility andresistance to the creep at elevatedtemperatures.

Developments in aluminium alloys andoptimization of casting techniques havelead to improved material properties andfunctional integration which enablealuminium castings to satisfy the newmarket requirements and have allowed toreplace, in many cases, engine componentsmade with heavy cast iron alloys.Nevertheless requirements for newproducts are becoming more and morechallenging for conventional aluminiumalloys and their further improvement or theintroduction of new alloys are under

evaluation.

Cylinder heads are, in particular, theengine components in which stress andoperating temperature levels haveincreased most in new downsized engines.The stresses on the cylinders heads inoperating conditions are mainly related tothe forces indicated in figure 1:1. Loads due to the pressure peaks in the

combustion chamber, that can reachvalues around 200 bar in dieselengines, resulting in fatigue loading ofthe structure, in particular on the water

jacket side of the flame deck.2. Dynamic loads from the valve train

system, acting mainly on the upper sideof the structure, in particular on thesupports of the camshaft.

3. Cylinder head bolts loads, generatedby the screws connecting the head tothe cylinder block. Tightening torque isusually very high in order to ensureproper cylinder head gasket sealingunder firing conditions.

4. Thermal loads due to the uneventemperature distribution in thecomponent and thus to non-uniformthermal expansion of the material.

A typical temperature distribution in thecylinder head of a high specific power

engine in operating conditions is shown inFig. 2.Maximum temperatures can locally exceed250C in the flame deck, combustion side(typically between exhaust valves), and

Fig. 1: Forces acting on a cylinder head.

Fig. 2: Temperature distribution in a cylinder head.

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reach values around 140C at the interfacewith the cooling water jacket.A typical stress distribution on the waterjacket side of a cylinder head, resulting bythe combination of the a.m. effects isreported in Fig. 3, showing that areas ofhigh stress concentration are found at theroot of the ports, where they intersect the

flame deck.

DESCRIPTION OF WORK

The present work summarizes the result ofan internal activity, carried out at TeksidAluminum, in which the mechanicalbehaviour at elevated temperature of anAl-Si-Cu alloy (A354 family), typically usedtoday for diesel cylinder heads cast inGravity Semi-Permanent Mould (GSPM),has been evaluated and the possibility of a

further development of this alloy to improveits resistance to high temperatures has beenstudied.The following properties have beenconsidered for the comparison:

tensile strength properties at roomtemperature (RT);

tensile strength properties at 150C(Typical condition found at the coolingfluid interface);

tensile strength properties at 250C(Typical condition found in the

combustion chamber); Hardness data for each test condition.

Test specimens have been taken both fromthe flame deck of actual cylinder headcastings (see Fig. 4), poured in the alloyunder evaluation, and, in some cases, fromseparately cast samples, poured using aspecific steel mould (Fig. 5), reproducingthe typical cooling conditions found in thebottom part of a cylinder head castingclose to the drag of the mould, so that asimilar microstructure can be reproduced.

Mechanical tests have been performed ona Zwick Z100/TL3S tensile testing machine,equipped with data acquisition system forthe recording of stress-strain curves.For the High Temperature (HT) tests atubular furnace positioned around thespecimen under test has been used; inorder to ensure temperature settingconsistency and to avoid temperaturegradient along the test bar, the controlsystem of the furnace uses threethermocouples positioned in the middleand at the ends of the test bar.

Fig. 3: Stress distribution in a cylinder head.

Fig. 4: Test specimen extracted from casting. Fig. 5: Mould for separately cast samples.

Fig. 6: RT Tensile test set-up. Fig. 7: HT Tensile test set-up.

Specially designed extensometer in stainless steel connected to optical position measuringsystem has been used to measure elongation during the HT tests. RT and HT test set-upsare shown in Fig. 6 and 7.

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CHOICE OF THE ALLOY SYSTEMS TO BE STUDIED

The following primary alloys, characterized by low content of impurities, Fe in particular,and whose composition is summarized in Table 1, have been used for the study:

Table 1. Alloys Composition

Chemical composition Adding elements Grain Eutectic(%) (%) refined modification

Alloys Si Mg Cu Fe Mn Ni TiB2 AlSr

AlSi9Cu1 9.40 0.40 1.05 0.25 < 0.10 0.00 0.05 0.05

AlSi9Cu1Mn 9.40 0.40 1.05 0.25 0.40 0.00 0.05 0.05

AlSi9Cu1NiMn 9.40 0.40 1.05 0.25 0.20 1.00 0.05 0.05

AlSi9Cu1

Baseline alloy, typically used at Teksid Aluminum for diesel cylinder heads. As pointed outin the Al-Si phase diagram, the 9% of silicon provides a good fluidity allowing good fillingof complex shapes with relatively low wall thickness, due to the low Liquidus temperature(start of solidification).

In Fig. 8 the binary Al-Si phase diagram is compared to a thermal analysis curve of thealloy. It is evident that respect to thermal analysis this alloy presents a quite shortsolidification interval, moreover, its considerable high silicon content (9%) allows for anhigher amount of eutectic phase solidification compared to a lower silicon alloy like acommon AlSi7/A356 with 7% Si.The content of approx. 1% of copper provides good mechanical properties at hightemperature, without affecting significantly elongation at RT.The cooling curve pointed out shows three transformation phase at three differenttemperatures during solidification.

Phase : f irst germination of alpha-Aluminium nucleus (Aluminum ) T.Liquidus =585C;

Phase : principal Eutectic solidif ication of Silicon compounds (Al+Si+Al5FeSi)T.Eutectic= 565/568C;

Phase (Al2Cu): first precipitation of Copper compounds (Al+Al2Cu+Si+Al5FeSi) T. =557/522C;

Phase (Al2Cu): complex Eutectic solidification of Copper compounds(Al+Al2Cu+Si+Al5Mg8Cu2Si6).

Solidification is completed at approx. 500C.

With the aim to search for improvement ofmechanical properties, at hightemperatures especially, the addition ofsome alloying has been considered andtwo modification of this alloy have beenincluded in the study:

AlSi9Cu1 (Mn) with addition of0.4% of Mn, aimed to reduce the

negative effect of acicular phasescontaining Fe impurities bytransforming them in Fe-Mnintermetallics with more complexshape (Chinese scripts).

AlSi9Cu1 (Ni-Mn) with 0.2% Mnand 1% Ni. Where the addition of Nishould provide improved resistance athigh temperature.

HEAT TREATMENT ANDCONDITIONING

All the cylinder head castings and theseparately poured samples have been heattreated before the tests in order tomaximize the aluminium alloys properties.T6 treatments were selected depending onthe type of alloy.

T6 HEAT TREATMENT

Solution phase at 510C for 6 hours.

Quenching in hot water (80C), at the

end of the solution phase in order tofreeze the state of solution in alloyelements.

Precipitation hardening at 225 for 6hours according to the type of alloy.

Fig. 8: Al-Si Phase Diagram & Thermal analysis of AlSi9Cu1.

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Before the tensile testing at HT (150 250C) all the test samples have been pre-conditioned at the test temperature for 500hours, in order to reproduce the inservice conditions of the over-agedmaterial and the microstructuraldamages caused by long exposure tohigh temperatures.

MECHANICAL TESTS RESULTS

A summary of the test conditions analyzedfor the various alloys is reported in table 2,while the results obtained in the tensiletests, as well as on Brinell hardness, at

Fig. 9: Tensile test results at RT.

Table 2. Summary of test conditions.

Alloy Heat treatment Over-Aging Characterization condition

Tensile test (20C)AlSi9Cu1 T6 500 h x 150C Tensile test (150C)

500 h x 250C Tensile test (250C)

Tensile test (20C)AlSi9Cu1 Mn T6 500 h x 150C Tensile test (150C)

500 h x 250C Tensile test (250C)

Tensile test (20C)AlSi9Cu1 NiMn T6 500 h x 250C Tensile test (250C)

Tensile test at room temperature

UTS (MPa) YTS (MPa) E% HB (5 mm-250Kg)

AlSi9Cu1 270 235 1,0 94AlSi9Cu1 + Mn 305 245 3,0 105

AlSi9Cu1 + Ni + Mn 310 270 1,3 106

room temperature and at 150 and 250C are reported in the Figs. 9, 10 and 11.Figures reported in the tables and histograms are the average values measured for eachset of tested specimen, while the stress-strain curves show the results of a single specimenrepresentative of the typical behaviour of the alloy.

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The following considerations can be drawn by the analysis of results obtained at RT (figure 9):

The behaviour of base alloy AlSi9Cu1 can be improved by the addition of Mn or Mn+Ni: in the first case UTS and elongationincrease significantly (reaching respectively 300 MPa and 3%), in the second both UTS (310 MPa) and YTS (270 MPa) grow, whileelongation remains stable.

According to the increase of the strength, the hardness is also improved.

Fig. 10: Tensile test results at 150C.

Tensile test at 150C (conditioning)


AlSi9Cu1 210 178 2,2 94

AlSi9Cu1 + Mn 233 211 4,8 100

At 150C, Fig. 10, all the alloys show a reduction of tensile properties compared to RT conditions. UTS decreases approximately 20%in average, even if the AlSi9Cu1 (Ni-Mn) modified alloy has not been tested at this temperature, it is confirmed that AlSi9Cu1(Mn)maintains better elongation and UTS compared to the base alloy.At 250C, Fig. 11, we can notice a further significant decrease of strength for all the alloys, with dramatic increase of elongation values.From the data in Fig. 11 it is evident that UTS of all the tested alloys drops well below 100 MPa, however the variant with Mn-Ni additionhas a slightly better behaviour than the others.

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Fig. 11: Tensile test results at 250C.

Tensile test at 250C (conditioning)


AlSi9Cu1 70 54 14,0 51

AlSi9Cu1 + Mn 75 58 21,0 53

AlSi9Cu1 + Ni + Mn 92 66 16,5 62

MICROSTRUCTURALEVALUATION

In order to get a deeper understanding ofthe behaviour of the different alloys, amicrostructural evaluation was performedon the specimen after the tensile test and asuitable surface preparation of transversesection of samples.

AlSi9Cu1

This type of alloy is characterized by dendritestructure with a homogeneous distribution ofeutectic silicon shown in Fig. 12.

By the addition of appropriate elementssuch as strontium in the liquid metal, it ispossible to modify silicon morphologicalstructure from lamellar to globular duringthe solidification. This modificationtreatment improves the mechanicalproperties of the AlSi alloy by reducing thenotching effect of needle shaped naturaleutectic silicon (Fig. 13).Another important practice to improve themechanical properties and castingcharacteristics is to introduce inoculatingcompound like titanium and boron. Thistreatment of grain refinement allows to

have a fine distribution of first dendritesgermination, due to nucleation of Al3TiB2particles during the melt cooling.The strengthening effect of Cu in this alloyis linked to precipitation of secondaryeutectic phases of CuAl2 intermetallics,shown in Fig. 14. The heat treatment causesthe disappearance/solubilisation of CuAl2while the last solidified phaseAl5Mg8Cu2Si6 is partly solubilised.Silicon particles are rounded and moreagglomerated, whilst the iron compounddoesnt show any shape modification.

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Fig. 12: Typical dendrite structure of AlSi alloys. Fig. 13: AlSi9Cu1 Globular distribution ofeutectic silicon.

Fig. 14: AlSi9Cu1- Eutectic Cu2 Mg8 Si6 Al5compound.

Fig. 15: AlSi9Cu1 Acicular morphology of Fe impurities

Element Weight% Atomic%

Al K 69.77 74.34

Si K 19.87 20.34Mn K 0.80 0.42

Fe K 9.28 4.78

Cu K 0.27 0.12

AlSi9Cu1 (Mn)

The presence of iron based precipitates on the AlSi9Cu1 base alloy is evident in Fig. 15, their morphology is of the acicular type and,as it is well known, this type of morphology is quite deleterious, especially for what concerns mechanical characteristics and ductility, in

particular the fracture appearance shows the presence of some clivages.

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With the addition of Mn the morphology of Fe compound changes from acicular type to complex shape, typical of Fe-Mn intermetallics(Chinese script, Fig. 16), improving the elongation properties of the alloy, due to the reduction of notching effect of Fe needles, thefracture surface now shows the consistent presence of dimples to state higher toughness properties. Because negative effects are notemphasized, it is possible to state that the modification of the base alloy with 0.5 % of manganese is beneficial.

Fig. 16: AlSi9Cu1 Mn - Morphology of Fe-Mn intermetallics


Al K 75.70 81.70Si K 10.83 11.22

Mn K 9.50 5.03

Fe K 3.43 1.79

Cu K 0.55 0.25


CK 8.93 24.14

Al K 35.37 42.58

Si K 1.03 1.19

Mn K 38.73 22.90

Fe K 14.88 8.6

Cu K 1.06 0.54

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AlSi9Cu1 (NiMn)

The second studied modification of the base alloy includes smaller Mn amount (0.2%), with the addition of 1% Ni. Also in this case, withrespect the basic alloy, the most relevant structure differences are always related to the modification of the morphology of the Fecontaining phases, that change from acicular ferrous compound type to complex shape, typical of Fe-Mn intermetallics and the acicularstructures are no longer observed. Moreover, the considerable percentage of nickel (1%), with reference to SEM analysis shown in Fig.17, contributes to the formation of solid solutions and mainly rounded eutectic components. In particular, it seems that nickel ties withcopper compound (CuAl2) improving the copper effect on resistance at high temperature.

Fig. 17: AlSi9Cu1 NiMn- Morphology of Fe-Mn intermetallics


Al K 82.89 84.03

Si K 12.77 15.35

Ni K 1.8 0.51

Cu K 2.25 0.41


Al K 92.61 96.62

Mn K 0.66 0.34

Ni K 1.53 0.73

Cu K 5.20 2.30

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SUMMARY ANDCONCLUSIONS

The mechanical behaviour of Aluminumalloys, measured by means of tensile testand Brinell hardness, is strongly influencedby the test temperature and by theexposure time at high temperatures.

The resistance of base Al-Si-Cu alloy isfairly good up to 150C (temperature atwhich the material actually works in the

most stressed areas at the bottom of thewater jacket of a cylinder head), but dropsat 250C.Some interesting improvements have beenachieved by modifying the composition ofthe base alloy with the addition of Mn andNi, resulting in an increase of strength andductility at both room and high

temperature.Based on the results achieved in the presentstudy it was decided to continue the

evaluation of the considered alloys also interms of High Cycle Fatigue and creepresistance at high temperature. This activityis at present on-going.Moreover the study will be continuedconsidering other binary alloys, mainlybased on Al-Mg and Al-Cu series, toevaluate their real potentiality towards this

kind of application. The obtained resultswill be presented and discussed in a secondpart of the paper

ACKNOWLEDGMENTS

The authors wish to thank the personnel at Teksid Aluminum R&D and testing Labs and Dario Pezzini of Materials Laboratory ofPolitecnico di Torino, Alessandria branch (Italy), for their precious contribution to the work.

Cylinder Heads Cast of Aluminum SAETechnical Paper Series SAE Technical PaperSeries 940153 (1994);

L. Arnberg, G.Heiberg, K.Nogita,M.Raanes, A.L.Dons.: Effect of magnesium,iron and copper on eutectic solidification ofhypoeutectic aluminium-silicon alloys AFSAmerican Foundry Society Transactions 02-088 (2002);

Blanda Lenczowsky, Hubert Koch, KlausEigenfelde, Burkhard Plege: New

developments of resistant alloys fromfoundry of aluminum to the hightemperatures Sonderdruck aus Gieberei 91(08/2004);

J. Royset and N. Ryum: Scandium inaluminium alloys Published by Maney forthe institute And ASM (2005)

BIBLIOGRAPHY

Pres. Kent R. Van Horn: AluminumProperties Physical Metallurgy and PhaseDiagrams, ASM American Society forMetals, (1967);

Di Russo: Metallographic atlas of aluminumalloys from foundry, Brescia EditionEDIMET (1993);

Paul H. Mikkola, John A.Redemske:Optimizing Proprerties of Automotive

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