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/cm, one third of steel), FCC structure (ductile at all temperatures).
- Good electrical and thermal conductivity, high reflectivity.
- Natural AlO 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
| Series | Main element | Features |
|---|---|---|
| 1xxx | 99%+ Al | Conductors, chemical equipment |
| 2xxx | Cu | High strength, aircraft |
| 3xxx | Mn | Moderate strength, cans, utensils |
| 5xxx | Mg | Good corrosion resistance, marine |
| 6xxx | Mg and Si | Extrusions, architectural frames |
| 7xxx | Zn | Highest 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
- Solution treatment: heat to about 520-540 °C, a single-phase region, and hold to dissolve all Cu.
- Quenching in water to room temperature: Cu is trapped in a supersaturated solid solution.
- Ageing: hold at room temperature (natural ageing) or 130-190 °C (artificial ageing). Cu atoms diffuse and cluster to form precipitates.
Precipitation sequence
Supersaturated GP zones (Cu-rich discs, coherent) (semi-coherent) (CuAl, incoherent, equilibrium).
Why strength increases
Coherent GP zones and 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 /.
Over-ageing
Long time or high temperature lets precipitates coarsen into large, widely spaced incoherent particles. Dislocations can easily bypass them (Orowan looping), so hardness and strength fall.
| Stage | Hardness |
|---|---|
| Quenched | Low |
| Under-aged (GP zones) | Rising |
| Peak aged (, ) | Maximum |
| Over-aged () | 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.
| Property | Aluminium alloys | Structural steel |
|---|---|---|
| Density | about 2.7 g/cm | about 7.85 g/cm |
| Young's modulus | about 70 GPa | about 200 GPa |
| Yield strength | 30-500 MPa | 250-1500 MPa |
| Specific strength (strength/density) | High (heat-treated alloys) | Moderate |
| Corrosion resistance | Good (oxide film) | Needs coating |
| Thermal/electrical conductivity | High | Low |
| Weldability | Needs special process (TIG/MIG) | Good (low-carbon steels) |
| Fatigue limit | None (no endurance limit) | Distinct endurance limit |
| Cost per kg | Higher | Lower |
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.
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