Model Composite (Layered) Material on the Basis of Titanium

  • L. A. Petrova
  • L. P. Grankova
  • V. I. Belyaev
  • A. P. Korshenevsky
  • A. A. Baikov

Abstract

Modern technology demands of material more and often incompatible requirements, for example, the combination of very high strength along the high fracture toughness and lightness. cently there appeared many publications on titanium alloys possess­ing much higher mechanical properties as compared with those known before. There are many publications about the improvement of properties of known alloys by using new kinds of heat treatment. By the latter is meant mild quenching including cooling in the furnace from the ß-field to the temperature of α+ß field followed by cooling in air (1);two stage aging, namely at first aging at the temperature of existing ω-phase and then at temperature field of (α+ß) phases (2); different variants of thermomechanical treatment (3,4). Additional doping of known grades of alloys is widely used with the purpose of increasing strength and toughness. New composites are being developed using multicomponent alloying and such elements as Cu, Si, As.(5,6)

Keywords

Fracture Toughness Titanium Alloy Impact Toughness Explosive Welding White Phase 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. 1.
    Auvinet, J., Leleu, G., Notton, G. and Marquier, G., “Mem. Sci. Rev. met.,” 1973, 70, NII, 809–821, II, III, V.Google Scholar
  2. 2.
    Alheritiere, E., Morinier, R. and Syre, R., “4 eme Sornee etude aciers el alliag. Spee. sew. aviat. Bourget, 1971, ” Paris, 1972, k/I–k2. Duscuss k/23–k26.Google Scholar
  3. 3.
    Boyer, R., Taggart, R. and Polonis, O. H., Metallography 7, 241–251 (1974).CrossRefGoogle Scholar
  4. 4.
    Nyffengger, W. and Schweisstechn., Z., 1972, 62, N 3, 61–76.Google Scholar
  5. 5.
    Seagle, S. R., Hall, G. S. and Bomberg, H. B., “Metals and Quart” 1975, 15, N I, 48–54.Google Scholar
  6. 6.
    Goosey Richard Ernest. Titanium-base alloys. (Imperial Metal Inds (Kynoch) Ltd.). Great Britain Pat. N 1298923. Cl.C7A. Int. cl. C22 015/00. Filed January, 7.71. Published December 6, 72.Google Scholar
  7. 7.
    Stubbington, C. A. and Bowen, A. W., The effect of section size on the fatigue properties of Ti-6A1-4V bars. “Titanium Sci. and Technol. Vol. 2”, New York-London, 1973, 1283–1296. Discuss. 1427–1428.Google Scholar
  8. 8.
    Collection. Applied questions of fracture toughness. Publisher “Mir, ”Moscow, 1968.Google Scholar

Copyright information

© Springer Science+Business Media New York 1982

Authors and Affiliations

  • L. A. Petrova
    • 1
  • L. P. Grankova
    • 1
  • V. I. Belyaev
    • 1
  • A. P. Korshenevsky
    • 1
  • A. A. Baikov
    • 1
  1. 1.Institute of MetallurgyUSSR

Personalised recommendations