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21-Mat-B7 Structure and Properties of Polymers · December 2016

Question 4 of 8: Magnesium Alloys — Alloying, Grain Refinement, Precipitation and Galvanic Compatibility

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Exams, December 2016 — 10-Met-B7, Physical Metallurgy of Non-Ferrous Metals and Alloys. Three hours, closed book, approved Casio/Sharp calculator only. Eight questions of 20 marks each; the rubric states that any five questions constitute a complete paper (100 marks total) and that only the first five appearing in the answer book are marked. All eight are answered here, because this set is a study resource rather than an exam script. The rubric explicitly notes that most questions require an essay-format answer and that clarity and organization are marked, so the answers below are written as structured prose rather than as note form.

Nothing on this paper is a polymer question; the syllabus actually examined is the physical metallurgy, strengthening and heat treatment of non-ferrous engineering alloys — aluminum, magnesium, copper-base alloys (brasses and bronzes), nickel- and cobalt-base superalloys, titanium, and the refractory/noble metals and intermetallic compounds.

Reference texts. The answers below are keyed to the works normally recommended for this syllabus code:



Question 4: Magnesium Alloys — Alloying, Grain Refinement, Precipitation and Galvanic Compatibility (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

4.1 — (a) Major magnesium alloying elements

Aluminum (solid-solution and precipitation strengthening, the base of the AZ/AM series), zinc (added with aluminum for extra strength and to counter the corrosion effect of iron impurities, AZ series; also alloyed with zirconium in the ZK series), manganese (controls iron content and improves corrosion resistance rather than providing strength), zirconium (a potent grain refiner used in aluminum-free alloys such as ZK and ZE, since Zr and Al cannot coexist — they form a stable intermetallic), and rare earths/thorium/silver (added for creep resistance and strength retention at elevated temperature, e.g. the WE and EZ series) are the major alloying additions used in engineering magnesium alloys.

4.2 — (b) Why die-cast Mg alloys don't need grain refining

Grain refinement in sand- or permanent-mold-cast magnesium (by superheating, carbon inoculation, or Zr additions) exists to counteract the naturally slow, coarse-grained solidification of those slower-cooling processes. High-pressure die casting injects molten metal into a water-cooled steel die under high pressure, giving an extremely high solidification rate and correspondingly severe undercooling; this alone nucleates a very fine as-cast grain structure without any chemical or process grain-refining step, so the additional refining practice needed for sand/permanent-mold castings would be redundant (and, for aluminum-bearing die-cast alloys, is precluded anyway because Zr cannot be used in the presence of Al).

4.3 — (c) Precipitation sequence and hardening response in Mg–Al alloys

On quenching from the single-phase solid-solution field, an Mg–Al alloy such as AZ91 is supersaturated in aluminum. Two competing precipitation reactions then occur during aging: a continuous reaction, in which fine, plate-shaped, semicoherent $\beta'$ precipitates nucleate homogeneously on the basal planes throughout the grain interior; and a discontinuous (cellular) reaction, in which lamellar colonies of coarse, incoherent equilibrium $\beta$ (Mg17Al12) nucleate at the grain boundaries and sweep inward, consuming solute as the cell front advances. The overall precipitation hardening response in Mg–Al alloys is comparatively small: the discontinuous cellular reaction dominates the transformed volume, and its widely spaced, incoherent lamellae produce little coherency strain and offer only a modest Orowan-type obstacle to dislocations, while the continuous reaction — the one that could in principle give a fine, closely spaced, more effective coherent dispersion — is starved of solute by the faster-advancing cellular front before it can develop fully. This is why Mg–Al alloys age-harden only modestly compared with a system like Al–Cu, where the equivalent continuous, fully coherent precipitation sequence is not competing with a discontinuous reaction for solute.

4.4 — (d) Why Mg cannot be directly coupled to steel or copper

Magnesium is the most anodic (electrochemically active) common structural metal, with a standard electrode potential of about −2.37 V for Mg2+/Mg — far more negative than iron (−0.44 V) or copper (+0.34 V). Direct metal-to-metal contact between magnesium and either steel or copper, in the presence of any electrolyte (moisture, condensation, road salt), forms a galvanic couple in which the enormous potential difference drives magnesium to corrode rapidly as the sacrificial anode while the steel or copper cathode is protected; because the anodic Mg area is often much smaller than the cathodic area in a typical fastener/bracket joint, the attack is also intensely localized. Engineering practice therefore isolates the joint electrically — insulating gaskets, coatings or plating on the mating part, sealed fasteners, and paint/primer barriers — rather than allowing bare Mg-to-steel or Mg-to-Cu contact in service.