Formation of Optimum Structural Strength of Aviation Fastening Bolts from Titanium Alloys

O. M. Ivasishin, P. E. Markovsky, Yu. Ya. Meshkov, А. V. Shiyan

G.V. Kurdyumov Institute for Metal Physics, NAS of Ukraine, 36 Academician Vernadsky Blvd., UA-03142 Kyiv, Ukraine

Received: 26.07.2017. Download: PDF

A methodology of formation of the optimal structural strength $\tau_{slice}$ is developed. Aviation fastening bolts made from titanium alloys for the purpose of balance of the combination of strength and plasticity properties by rational selection of a set of their basic mechanical characteristics, i.e., the conditional yield strength $\sigma_{Y}$, the ultimate tensile strength $\sigma_{S}$, and the relative reduction in area $\psi$ at the moment of sample destruction. As determined, the value of the structural strength $\tau_{slice}$ of aviation fastening bolts made from titanium alloys is formed by these basic mechanical characteristics, $\sigma_{Y}$, $\sigma_{S}$, and $\psi$, as well as by the true fracture stress $S_f$ under uniaxial tension tests. As shown, in order to increase the structural strength of aviation fastening bolts made from titanium alloys up to the required level of $\tau_{slice} \cong$ 850 MPa, technologists’ efforts must be aimed to increase the level of parameter $\sigma_{Y}$/$\sigma_{S}$ and to reduce the strain hardening exponent $n$ for advanced titanium alloys. The formation conditions for such a complex of properties make possible not only to form the best values of $\tau_{slice}$ purposefully, but also to give a justified forecast estimation of the possibility of further increase of this parameter.

Key words: fastening bolts, titanium alloys, structural strength, embrittlement, optimization of mechanical properties.

URL: http://mfint.imp.kiev.ua/en/abstract/v39/i09/1197.html

DOI: https://doi.org/10.15407/mfint.39.09.1197

PACS: 46.50.+a, 62.20.fk, 62.20.mj, 62.20.mm, 81.40.Ef, 81.40.Jj, 81.40.Np

Citation: O. M. Ivasishin, P. E. Markovsky, Yu. Ya. Meshkov, and А. V. Shiyan, Formation of Optimum Structural Strength of Aviation Fastening Bolts from Titanium Alloys, Metallofiz. Noveishie Tekhnol., 39, No. 9: 1197—1211 (2017) (in Russian)


REFERENCES
  1. Metally. Metod Ispytaniya na Srez: OST 1.90148–74 [Metals Shear Test Method: OST 1.90148–74] (in Russian).
  2. O. M. Ivasishin, P. E. Markovsky, A. G. Molyar, S. L. Antonyk, and I. M. Gavrysh, Proc. International Conference 'Titan-2012 in CIS» (April 22–25, 2012, Kazan), p. 39 (in Russian).
  3. Yu. Ya. Meshkov and A. V. Shiyan, Mekhanika Mashin, Mekhanizmov i Materialov, No. 1: 79 (2017) (in Russian).
  4. I. A. Birger and G. B. Iosilevich, Rez'bovye i Flantsevye Soedineniya [Threaded and Flanged Connections] (Moscow: Mashinostroenie: 1990) (in Russian).
  5. A. V. Shiyan, Yu. Ya. Meshkov, and D. G. Savvakin, Mekhanika Mashin, Mekhanizmov i Materialov, No. 4: 70 (2015) (in Russian).
  6. G. B. Iosilevich, Kontsentratsiya Napryazheniy i Deformatsiy v Detalyakh Mashin [Concentration of Stresses and Strains in Machine Parts] (Moscow: Mashinostroenie: 1981) (in Russian).
  7. G. N. Savin and V. I. Tul'chiy, Spravochnik po Kontsentratsii Napryazheniy [Handbook of Stress Concentration] (Kiev: PO 'Vysshaya Shkola': 1976) (in Russian).
  8. J. H. Hollomon, Trans. AIME. Iron Steel Div., 162: 268 (1945).
  9. O. M. Ivasishin, P. E. Markovsky, Yu. V. Matviychuk, S. L. Semiatin, C. H. Ward, and S. Fox, J. Alloys Compd., 457, Iss. 1–2: 296 (2008). Crossref
  10. P. E. Markovsky, Metallofiz. Noveishie Tekhnol., 31, No. 4: 511 (2009) (in Russian).
  11. O. M. Ivasishin, P. E. Markovsky, A. G. Molyar, V. O. Mushegyan, and O. V. Mushegyan, Proc. International Conference 'Titan-2012 in CIS» (April 22–25, 2012, Kazan), p. 102 (in Russian).
  12. I. M. Havrysh, Formuvannya Vysokomitsnykh Strukturno-Fazovykh Staniv u Detalyakh Kriplennya z Tytanovogo Splavu VT22 pry Obroblenni v Nerivnovazhnykh Umovakh [Formation of High-Strength Structural-Phase States in the Fastening Parts from Titanium Alloy VT22 under Non-Equilibrium Treatment] (Disser. … for Cand. Techn. Sci.) (Kyiv: 'Antonov' Company: 2017) (in Ukrainian).
  13. O. M. Ivasishin, P. E. Markovsky, S. A. Kotrechko, Yu. Ya. Meshkov, and A. V. Shiyan, Metallofiz. Noveishie Tekhnol., 35, No. 1: 129 (2013) (in Russian).
  14. Yu. Ya. Meshkov, S. A. Kotrechko, and A. V. Shiyan, Mekhanicheskaya Stabil'nost' Metallov i Splavov [Mechanical Stability of Metals and Alloys] (Kyiv: Naukova Dumka: 2014) (in Russian).
  15. A. V. Shiyan, Naukovi Osnovy Formuvannya Ratsional'nogo Kompleksu Mekhanichnykh Vlastyvostey Konstruktsiynykh Staley i Tytanovykh Splaviv [Scientific Basis for the Formation of a Rational Complex of Mechanical Properties of Structural Steels and Titanium Alloys] (Disser. … for Dr. Techn. Sci.) (Dnipropetrovsk: Prydniprovs'ka State Academy of Civil Engineering and Architecture: 2016) (in Ukrainian).
  16. B. A. Kolachev and A. V. Mal'kov, Fizicheskie Osnovy Razrusheniya Titana [Physical Basis of Titanium Destruction] (Moscow: Metallurgiya: 1983) (in Russian).
  17. V. T. Troshchenko, V. V. Pokrovskiy, and V. L. Yarusevich, Problemy Prochnosti, No. 8: 30 (1991) (in Russian).