Skip to main content

Chapter 9 · 3 hours

Non-ferrous Alloys

Practice questions

Practice questions and answers

3 exam-style questions on this chapter, written for this site from the official syllabus. We haven’t found past IOE papers for this subject yet; if you have some, share them in the community.

  • Practice · 6 marks

Write short notes on the classification of aluminium alloys. State the properties of pure aluminium that make it important, and give the composition and uses of duralumin and Y-alloy.

Answer

Properties of aluminium

  • Low density (2.7 g/cm3^3, one third of steel), FCC structure (ductile at all temperatures).
  • Good electrical and thermal conductivity, high reflectivity.
  • Natural Al2_2O3_3 film gives good corrosion resistance.
  • Pure Al is weak (tensile strength about 90 MPa), so it is alloyed (Cu, Mg, Si, Zn, Mn) and strengthened by cold work or precipitation hardening.

Classification

Aluminium alloys
 |-- Wrought (rolled, extruded, forged)
 |     |-- Non-heat-treatable : 1xxx, 3xxx (Mn), 5xxx (Mg)
 |     `-- Heat-treatable     : 2xxx (Cu), 6xxx (Mg-Si), 7xxx (Zn)
 `-- Cast
       |-- Non-heat-treatable : Al-Si (LM6)
       `-- Heat-treatable     : Al-Cu, Al-Si-Mg
SeriesMain elementFeatures
1xxx99%+ AlConductors, chemical equipment
2xxxCuHigh strength, aircraft
3xxxMnModerate strength, cans, utensils
5xxxMgGood corrosion resistance, marine
6xxxMg and SiExtrusions, architectural frames
7xxxZnHighest strength, aircraft

Special alloys

  • Duralumin: 3.5-4.5% Cu, 0.5% Mg, 0.5-1% Mn, rest Al. Age hardened; used in aircraft structures and automobile parts.
  • Y-alloy: 4% Cu, 2% Ni, 1.5% Mg, rest Al. Retains strength at high temperature; used in pistons, cylinder heads and aero engine parts.
  • Al-Si (silumin): 10-13% Si; excellent castability for engine casting and housings.
  • Practice · 8 marks

Explain precipitation (age) hardening of an Al-4% Cu alloy. Describe the three steps of the heat treatment, the sequence of precipitates formed, and why the alloy becomes stronger. Why does over-ageing reduce the strength?

Answer

Age hardening raises the strength of alloys whose solid solubility decreases with falling temperature, by forming very fine precipitates that block dislocations. Al-4% Cu is the classic example (duralumin).

Conditions for age hardening

The phase diagram must show a solvus line, i.e., the solute (Cu) is soluble at high temperature (up to 5.65% at 548 °C) but only about 0.2% at room temperature.

Heat-treatment steps

 T
 |   solution  ______
 |   treat.   |      | (500-550 C)
 |            |      | quench
 |            |      `--.   ageing
 |            |           `----_____ (130-190 C, hours)
 +------------------------------------> time
  1. Solution treatment: heat to about 520-540 °C, a single-phase α\alpha region, and hold to dissolve all Cu.
  2. Quenching in water to room temperature: Cu is trapped in a supersaturated solid solution.
  3. Ageing: hold at room temperature (natural ageing) or 130-190 °C (artificial ageing). Cu atoms diffuse and cluster to form precipitates.

Precipitation sequence

Supersaturated α\alpha →\rightarrow GP zones (Cu-rich discs, coherent) →\rightarrow θ′′\theta'' →\rightarrow θ′\theta' (semi-coherent) →\rightarrow θ\theta (CuAl2_2, incoherent, equilibrium).

Why strength increases

Coherent GP zones and θ′′\theta'' distort the surrounding lattice. Dislocations must cut through the particles or bow around them, which needs a higher stress. Maximum hardness occurs with a fine, dense dispersion of θ′′\theta''/θ′\theta'.

Over-ageing

Long time or high temperature lets precipitates coarsen into large, widely spaced incoherent θ\theta particles. Dislocations can easily bypass them (Orowan looping), so hardness and strength fall.

StageHardness
QuenchedLow
Under-aged (GP zones)Rising
Peak aged (θ′′\theta'', θ′\theta')Maximum
Over-aged (θ\theta)Falling
  • Practice · 5 marks

Compare aluminium alloys with steel for structural use. State the advantages and limitations of aluminium alloys and give examples of applications.

Answer

Aluminium alloys are used where low weight, corrosion resistance and good conductivity matter more than the highest stiffness or lowest cost.

PropertyAluminium alloysStructural steel
Densityabout 2.7 g/cm3^3about 7.85 g/cm3^3
Young's modulusabout 70 GPaabout 200 GPa
Yield strength30-500 MPa250-1500 MPa
Specific strength (strength/density)High (heat-treated alloys)Moderate
Corrosion resistanceGood (oxide film)Needs coating
Thermal/electrical conductivityHighLow
WeldabilityNeeds special process (TIG/MIG)Good (low-carbon steels)
Fatigue limitNone (no endurance limit)Distinct endurance limit
Cost per kgHigherLower

Advantages of aluminium alloys

  • Light weight and high strength-to-weight ratio.
  • Good corrosion resistance, easy to extrude and cast in complex shapes.
  • Recyclable using only about 5% of the energy needed for primary production.
  • Non-magnetic and non-sparking; retains toughness at low temperature (FCC).

Limitations

  • Low modulus gives larger deflection for same section.
  • Loses strength above about 150-200 °C; low melting point (660 °C).
  • Galvanic corrosion when in contact with steel or copper.

Applications

Aircraft skin and frames (2024, 7075), engine pistons and blocks (Al-Si), transmission lines (1350), beverage cans (3004, 5182), window frames (6063), and automotive body panels.

Written from the official syllabus. Questions and answers are written for this site; check them against your class notes.

Chapter titles and hours from the IOE syllabus ↗