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A comparison of gaseous hydrogen embrittlement, slow-strain-rate hydrogen embrittlement, and stress-corrosion cracking in Ti-8Al-1Mo-1V

Journal Article · · Metall. Trans., A; (United States)
DOI:https://doi.org/10.1007/BF02643767· OSTI ID:6902808

Metallographic, fractographic, and acoustic-emission studies have been carried out on the near-..cap alpha.. commercial alloy, heat treated to produce the Widmanstatten structure and in some cases aged to precipitate ..cap alpha../sub 2/. Both aged and unaged material underwent gaseous hydrogen embrittlement (GHE) in approx. 10kPa gaseous hydrogen, failure occurring along the ..cap alpha..-..beta.. interface. Electron-diffraction studies established the presence of a layer of fcc titanium hydride at the fracture surfaces, and acoustic-emission and fractographic observations indicated that propagation was discontinuous. The aged alloy underwent slow-strain-rate hydrogen embrittlement in inert environments and stress-corrosion cracking in 3 pct aqueous NaCl and, in contrast to CHE, failure occurred across the ..cap alpha..-plates in both cases, producing indistinguishable cleavage-like fracture surfaces. Again, titanium hydride was detected at the fracture surfaces and, from acoustic-emission studies, crack propagation appeared to be discontinuous. Based on these observations, it is suggested that the three forms of failure occur by a common mechanism namely by the repeated formation and rupture of the hydride phase.

Research Organization:
Univ. of Illinois, Urbana
DOE Contract Number:
AC02-76ER01198
OSTI ID:
6902808
Journal Information:
Metall. Trans., A; (United States), Journal Name: Metall. Trans., A; (United States) Vol. 12A; ISSN MTTAB
Country of Publication:
United States
Language:
English