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Ahmet Çelik

Chapter 1: Structure of Metals

MECH306 3 minute read

When metals solidify from the molten state, atoms arrange into orderly crystals. The smallest group of atoms showing the characteristic lattice is a unit cell. Three common structures:

  • Body-centered cubic (BCC)
  • Face-centered cubic (FCC)
  • Hexagonal close-packed (HCP)

Atoms are held by metallic bonding — attracting but repelling if too close; the stable structure minimizes total energy. Interatomic spacing ≈ 0.10.1 nm.

Allotropism (polymorphism) — a metal can take different crystal structures at different temperatures; this underlies heat treatment. For steel:

  • Quenching (rapid): Austenite (FCC) → Martensite (very hard, strong)
  • Slow cooling: Austenite → Pearlite (softer, ductile)

Deformation of Single Crystals

  • Elastic — recovers on unloading.
  • Plastic (permanent) — does not recover.

Two mechanisms:

  1. Slip — one atomic plane slides over an adjacent one under shear stress, along planes of maximum atomic density and closely packed directions. Direction-dependent behavior makes a single crystal anisotropic.
  2. Twinning.

Slip Systems

A slip system = slip plane + slip direction. Metals with ≥ 5 slip systems are generally ductile; fewer are not.

StructureSlip systemsBehavior
BCC48High required shear stress → good strength, moderate ductility
FCC12Low required shear → moderate strength, good ductility
HCP3Low slip probability → brittle at room T (more systems activate when hot)

Imperfections

Actual strength is ~1–2 orders of magnitude below theoretical, due to dislocations / defects.

  • They lower mechanical & electrical properties (yield, fracture strength, conductivity).
  • Physical & chemical properties (melting point, specific heat, thermal expansion, EE, GG) are not sensitive to defects.

Point defects: vacancy (missing atom), interstitial atom (extra), interstitial impurity atom (foreign).

A slip plane containing a dislocation needs less shear stress to slip than a perfect lattice — the main reason actual < theoretical strength.

Work (Strain) Hardening

Dislocations entangle and are blocked by grain boundaries, impurities, and inclusions, raising the shear stress for further slip — work / strain hardening.

Examples: rolling car-body sheet (Ch13), forging bolt heads (Ch14), drawing wire (Ch15).

Grains & Grain Boundaries

Crystals nucleate independently with random orientations and grow into grains.

  • High nucleation rate → many grains → small grain size.
  • Rapid cooling → smaller grains; slow cooling → larger grains.

Grain Size (ASTM)

ASTM number nn vs grains NN per in² at 100×:

N=2n−1N = 2^{n-1}

where NN is grains per 0.01textintimes0.01textin0.01text{ in} times 0.01text{ in}. In grains/mm² (that area =0.0645textmm2= 0.0645text{ mm}^2):

N′=10.0645⋅2n−1=16⋅2n−1=2n+3N' = \frac{1}{0.0645}\cdot 2^{n-1} = 16\cdot 2^{n-1} = 2^{n+3}

  • n=5n = 5–8 → fine grains; n≥7n \ge 7 acceptable for sheet (car bodies, appliances, utensils).
  • Large grains → low strength/hardness/ductility and a rough orange-peel surface after stretching.

Recovery, Recrystallization & Grain Growth

Cold work → ↑strength, ↓ductility, anisotropy. Heating (annealing) reverses it.

  • Pb, Sn, Cd, Zn recrystallize near room temperature → they don’t work-harden when cold-worked.
  • More prior cold work → lower recrystallization temperature.
  • Greater deformation → finer recrystallized grains (refines a coarse structure).
  • Grain growth: further heating enlarges grains → orange peel on stretched sheet.

Cold-, Warm-, Hot-Working

With TT and TmT_m in kelvin (T(textK)=273+circtextCT(text{K}) = 273 + {}^{circ}text{C}):

  • T/Tm<0.3T/T_m < 0.3 → cold-working
  • 0.3<T/Tm<0.50.3 < T/T_m < 0.5 → warm-working
  • T/Tm>0.6T/T_m > 0.6 → hot-working