Non Ferrous alloys MSE 528 Mg alloys for

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Non Ferrous alloys MSE 528

Non Ferrous alloys MSE 528

Mg alloys for automotive

Mg alloys for automotive

Copper and its Alloys

Copper and its Alloys

Beta stabilizer

Beta stabilizer

Ti alloy • Alpha stabilizers: C, O, N and Al • Beta Stabilizers: Cr,

Ti alloy • Alpha stabilizers: C, O, N and Al • Beta Stabilizers: Cr, Fe, Pd, Co, Mn, H, V, Mo, Ta, Nb • Alpha alloys: Ti-5 Al-2. 5 Sn, Ti-4 al-1 Mo • Beta alloys: Beta 21 S (13%Mo), • Alpha + Beta alloys: Ti-6 Al-4 V, • ELI: extra low level Interstitials

Tix. Al

Tix. Al

PRECIPITATION HARDENING • Particles impede dislocations. • Ex: Al-Cu system • Procedure: --Pt A:

PRECIPITATION HARDENING • Particles impede dislocations. • Ex: Al-Cu system • Procedure: --Pt A: solution heat treat (get a solid solution) --Pt B: quench to room temp. --Pt C: reheat to nucleate small q crystals within a crystals. • Other precipitation systems: • Cu-Be • Cu-Sn • Mg-Al Adapted from Fig. 11. 22, Callister 6 e. (Fig. 11. 22 adapted from J. L. Murray, International Metals Review 30, p. 5, 1985. ) Adapted from Fig. 11. 20, Callister 6 e. 20

PRECIPITATE EFFECT ON TS, %EL • 2014 Al Alloy: • TS peaks with precipitation

PRECIPITATE EFFECT ON TS, %EL • 2014 Al Alloy: • TS peaks with precipitation time. • Increasing T accelerates process. • %EL reaches minimum with precipitation time. Adapted from Fig. 11. 25 (a) and (b), Callister 6 e. (Fig. 11. 25 adapted from Metals Handbook: Properties and Selection: Nonferrous Alloys and Pure Metals, Vol. 2, 9 th ed. , H. Baker (Managing Ed. ), American Society for Metals, 1979. p. 41. ) 21

PRECIPITATION STRENGTHENING • Hard precipitates are difficult to shear. Ex: Ceramics in metals (Si.

PRECIPITATION STRENGTHENING • Hard precipitates are difficult to shear. Ex: Ceramics in metals (Si. C in Iron or Aluminum). • Result: 24

APPLICATION: PRECIPITATION STRENGTHENING • Internal wing structure on Boeing 767 Adapted from Fig. 11.

APPLICATION: PRECIPITATION STRENGTHENING • Internal wing structure on Boeing 767 Adapted from Fig. 11. 0, Callister 5 e. (Fig. 11. 0 is courtesy of G. H. Narayanan and A. G. Miller, Boeing Commercial Airplane Company. ) • Aluminum is strengthened with precipitates formed by alloying. Adapted from Fig. 11. 24, Callister 6 e. (Fig. 11. 24 is courtesy of G. H. Narayanan and A. G. Miller, Boeing Commercial Airplane Company. ) 1. 5 mm 26