The effect of lamellar morphology on tensile and high-cycle fatigue behavior of orthorhombic Ti-22Al-27Nb alloy

Cited 38 time in webofscience Cited 37 time in scopus
  • Hit : 372
  • Download : 0
The room-temperature tensile and high-cycle fatigue (HCF) behavior of orthorhombic Ti-22Al-27Nb alloy with varying lamellar morphology was investigated. Varying lamellar morphology was produced by changing the cooling rate after annealing in the single 132 phase region. A slower cooling rate of 0.003 K/s, for example, resulted in several large packets or colonies of similarly aligned O-phase lamellae and a nearly continuous massive alpha(2) phase at the prior 132 grain boundaries, while a faster cooling rate of 0.1 K/s led to the refinement of colony sizes and the O-phase lamellae. The interface of O-phase lamellae and 132 phases was semicoherent. Water quenching produced a very fine tweed-like microstructure with a thin continuous 0 phase at the prior B2 grain boundaries. The 0.2 pct yield stress, tensile strength. and HCF strength increased with increasing cooling rate. For example, the tensile strength and HCF strength at 10(7) cycles of 0.003 and 0.1 K/s-cooled were 774 and 450 MPa, and 945 and 620 MPa, respectively. Since the fatigue ratio, which is the ratio of HCF strength at 10(7) cycles to tensile strength, did not show a constant value, but instead increased with increasing cooling rate, part of the fatigue improvement was the result of improved resistance to fatigue associated with the microstructural refinement of the lamellar morphology. Fatigue failure occurred by the subsurface initiation, and every initiation site was found to contain a flat facet. Concurrent observation of the fatigue initiation facet and the underlying microstructure revealed that the fatigue crack initiated in a shear mode across the colony, irrespective of colony size, indicating that the size of the initiation facet corresponded to that of the colony. Therefore, the colony size is likely a major controlling factor in determining the degree of fatigue improvement due to the microstructural refinement of lamellar morphology. For the water-quenched specimens, fatigue crack initiation appeared to be associated with shear cracking along the boundary between the continuous grain boundary 0 phase and the adjacent prior 132 grain.
Publisher
Springer
Issue Date
2004
Language
English
Article Type
Article
Keywords

AL-NB SYSTEM; CREEP-BEHAVIOR; INTERMETALLIC ALLOYS; TITANIUM-ALLOY; CRACK-GROWTH; MICROSTRUCTURE; TI-6AL-4V; EVOLUTION

Citation

METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, v.35A, no.7, pp.2161 - 2170

ISSN
1073-5623
DOI
10.1007/s11661-004-0164-y
URI
http://hdl.handle.net/10203/82785
Appears in Collection
Files in This Item
There are no files associated with this item.
This item is cited by other documents in WoS
⊙ Detail Information in WoSⓡ Click to see webofscience_button
⊙ Cited 38 items in WoS Click to see citing articles in records_button

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0