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aluminium in commercial vehicles - European Aluminium Association

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EUROPEAN ALUMINIUM ASSOCIATION ALUMINIUM IN COMMERCIAL VEHICLES CHAPTER VI 59<br />

4. Alum<strong>in</strong>ium versus Steel<br />

Both steel and <strong>alum<strong>in</strong>ium</strong> are<br />

metals with relatively high<br />

strength. Both materials are<br />

<strong>in</strong>combustible and will not contribute<br />

to a fire. For structural<br />

purposes the ma<strong>in</strong> differences<br />

are:<br />

Elasticity: The modulus of elasticity<br />

(E-modulus) of <strong>alum<strong>in</strong>ium</strong> is<br />

1/3 of that of steel. This means<br />

that an <strong>alum<strong>in</strong>ium</strong> beam with<br />

the same cross-section and the<br />

same loads as a steel beam will<br />

have a deflection 3 times that of<br />

the steel beam.<br />

Weight: The density of <strong>alum<strong>in</strong>ium</strong><br />

is 1/3 of that of steel. This<br />

means that a steel beam will<br />

weigh 3 times more than an <strong>alum<strong>in</strong>ium</strong><br />

beam with the same<br />

cross-section.<br />

Weld<strong>in</strong>g: When weld<strong>in</strong>g a hardened<br />

<strong>alum<strong>in</strong>ium</strong> alloy some of<br />

the harden<strong>in</strong>g effects will be lost.<br />

The strength <strong>in</strong> the heat affected<br />

zone (HAZ) will be reduced. This<br />

reduction depends on the alloy,<br />

temper, type of product and<br />

weld<strong>in</strong>g procedure. Ord<strong>in</strong>ary<br />

steel has no strength reduction<br />

after weld<strong>in</strong>g.<br />

Thermal elongation: The coefficient<br />

of thermal elongation of<br />

<strong>alum<strong>in</strong>ium</strong> is twice that of steel.<br />

This means that an <strong>alum<strong>in</strong>ium</strong><br />

member will get twice the thermal<br />

elongation as a similar steel<br />

member with the same temperature<br />

difference. S<strong>in</strong>ce the elastic<br />

modulus of <strong>alum<strong>in</strong>ium</strong> is 1/3 of<br />

steel, the stresses <strong>in</strong> an <strong>alum<strong>in</strong>ium</strong><br />

member with fixation are 2/3 of<br />

that <strong>in</strong> a similar steel member.<br />

Most of the structural <strong>alum<strong>in</strong>ium</strong><br />

alloys have relatively high<br />

“strength-to-E modulus” ratio.<br />

This effect is especially clear<br />

when the <strong>alum<strong>in</strong>ium</strong> alloy is<br />

stra<strong>in</strong>-hardened or heat-treated.<br />

Structural <strong>alum<strong>in</strong>ium</strong> alloys have<br />

roughly twice the “strength-to-E<br />

modulus” ratio than standard steel.<br />

However, when compared with<br />

high strength steels, structural<br />

<strong>alum<strong>in</strong>ium</strong> alloys have about the<br />

same “strength-to-E modulus”<br />

ratio. It should also be noted that<br />

the elastic modulus of an alloy<br />

ma<strong>in</strong>ly depends on its parent<br />

metal. In other words, all <strong>alum<strong>in</strong>ium</strong><br />

alloys have very similar Emodulus,<br />

but this is also valid for<br />

steel alloys. Consequently, the so<br />

called “high strength steels”<br />

don’t have better elastic properties<br />

than mild steel.<br />

Steel designers often use the<br />

strength of the material as govern<strong>in</strong>g<br />

criteria when desig n<strong>in</strong>g a<br />

steel struc ture and check afterwards<br />

whether the deflection is<br />

with<strong>in</strong> the requirement.<br />

When design<strong>in</strong>g an <strong>alum<strong>in</strong>ium</strong><br />

structure, it will often be the<br />

deflection criterion that will be<br />

govern<strong>in</strong>g. For that reason, the<br />

design procedure will start with<br />

the deflection criterion and it will<br />

be checked afterwards if the<br />

stress or the resistance of the<br />

structure is with<strong>in</strong> the limits.<br />

The deflection of members under<br />

bend<strong>in</strong>g load depends on the<br />

modulus of elasticity (E) and on<br />

the moment of <strong>in</strong>ertia (I) together<br />

with the load and the span.<br />

With the same span and load, it<br />

will be the product E x I that will<br />

determ<strong>in</strong>e the deflection.<br />

To get the same deflection of<br />

steel and <strong>alum<strong>in</strong>ium</strong> beams <strong>in</strong><br />

bend<strong>in</strong>g, the moment of <strong>in</strong>ertia<br />

of the <strong>alum<strong>in</strong>ium</strong> beam must be<br />

three times that of steel. If the<br />

<strong>in</strong>crease <strong>in</strong> the moment of <strong>in</strong>ertia<br />

is to be done only by <strong>in</strong>creas<strong>in</strong>g<br />

the thickness of the web and<br />

flanges, the <strong>alum<strong>in</strong>ium</strong> beam will<br />

have the same weight as the<br />

steel beam.

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