Nonferrous metals and alloys

For thick plate and forgings of alloy 7075, the overaged T73 temper is sometimes chosen over T6, which gives the highest strength. Which is the main reason?

  1. AIn T73 the precipitates are finer and denser than in T6, so the strength rises considerably and the fatigue strength rises too
  2. BT73 skips artificial aging and is finished by natural aging alone, which lowers the cost of heat treatment and improves weldability
  3. CThe strength is 10 to 15% lower than T6, but coarse, discontinuous grain-boundary precipitates raise resistance to stress corrosion cracking
Show answer and explanation

Answer: C. The strength is 10 to 15% lower than T6, but coarse, discontinuous grain-boundary precipitates raise resistance to stress corrosion cracking

The 7000 series, containing Zn, Mg and Cu, are the strongest aluminum alloys, but in the T6 condition, when tensile stress acts through the thickness of a thick part in a humid environment, stress corrosion cracking along grain boundaries readily occurs. T73 is an overaged temper in which aging is carried further than T6, at a higher temperature or for a longer time; the tensile and yield strengths are about 10 to 15% lower than T6, but the grain-boundary precipitates become coarse and discontinuous, so cracks along grain boundaries advance less easily. Overaging coarsens the precipitates, so the option in which they become finer and denser and raise the strength is backward. T7 indicates overaging; it does not skip aging, and finishing by natural aging alone corresponds to T4. Tempers such as T76 and T74, with other balances of strength and corrosion resistance, are also used.

Report an error

Practice this topic Back to topic

More Nonferrous metals and alloys questions

  1. Suppose that adding lithium to aluminum lowers the density by about 3% and raises Young's modulus by about 6% per mass% of Li. About how many times that of pure aluminum is the specific stiffness (Young's modulus/density) of an Al-Li alloy containing 2.0 mass% Li? Assume the changes are proportional to the amount added.
  2. Tough-pitch copper (copper containing about 0.02 to 0.05% oxygen, mostly dispersed as Cu₂O) can become brittle when it is heated in a reducing atmosphere containing hydrogen or is gas welded or brazed. Which gives the correct cause and remedy?
  3. Among copper alloys for springs and connectors, which is the correct pairing of the strengthening mechanisms of phosphor bronze and beryllium copper?
  4. The corrosion resistance of magnesium alloys depends strongly on the amounts of the impurities Fe, Ni and Cu, and in high-purity alloys such as AZ91D the upper limits for Fe and Ni are set very low, at about 0.005% or less. Which is the correct reason?
  5. A flat panel whose thickness is chosen to give a fixed bending stiffness is changed from an aluminum alloy (Young's modulus 70 GPa, density 2.70 g/cm³) to a magnesium alloy (Young's modulus 45 GPa, density 1.74 g/cm³). If the area of the panel is the same and the bending stiffness is proportional to E × (thickness)³, about how many times the mass of the aluminum alloy panel is the mass of the magnesium alloy panel?