About parameters of Paris equation at fatigue crack growth rate tests of heat-resistant titanium alloys

Gorbovets M.A., Nochovnaya N.A.
UDC
539.388.1:669.018.44:669.295
DOI
10.18577/2307-6046-2016-0-4-2-2
Article PDF (Russian) (642.78 KB)
How to cite
Gorbovets M.A., Nochovnaya N.A. About parameters of Paris equation at fatigue crack growth rate tests of heat-resistant titanium alloys // Proceedings of VIAM. 2016. No. 4. DOI: 10.18577/2307-6046-2016-0-4-2-2. URL: https://test.viam.ru/en/journal/2016/4/2
Abstract

Fatigue crack growth rate (FCGR) is a necessary component in the complex of mechanical properties characterizing reliability of materials for aviation engineering. Research of FCGR of heat-resistant titanium alloys VT8-1, VT41, VIT1 is conducted at room and working temperatures, two cycle ratios (0,1 and 0,5). It is established that parameters of Paris equation (C and n) for the studied heat-resistant titanium alloys are not independent and are approximated by the general direct line in «lgC–lgn» coordinates. Investigation is executed within implementation of the complex scientific direction 2.2. «Qualification and researches of materials» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Reference list
  1. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitiya materialov i tehnologij ih pererabotki na period do 2030 goda» [Innovative developments of FSUE «VIAM» SSC of RF on realization of «Strategic directions of the development of materials and technologies of their processing for the period until 2030»] // Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 3–33.
  2. Kablov E.N. Sovremennye materialy – osnova innovacionnoj modernizacii Rossii [Modern materials – basis of innovative modernization of Russia] // Metally Evrazii. 2012. №3. S. 10–15
  3. Antashev V.G., Nochovnaya N.A., Pavlova T.V., Ivanov V.I. Zharoprochnye titanovye splavy [Heat resisting titanium alloys] // Vse materialy. Enciklopedicheskij spravochnik. 2007. №3. S. 7–8.
  4. Birger I.A., Balashov B.F., Dulnev R.A. i dr. Konstrukcionnaya prochnost materialov i detalej gazoturbinnyh dvigatelej [Constructional durability of materials and details of gas turbine engines]. M.: Mashinostroenie, 1981. 222 s.
  5. Serensen S.V., Kogaev V.P., Shnejderovich R.M. Nesushhaya sposobnost i raschet detalej mashin na prochnost: rukovodstvo i spravochnoe posobie [Bearing capacity and calculation of details of machines on durability: management and handbook]. M.: Mashinostroenie, 1975. 488 s.
  6. Nochovnaya N.A. Perspektivy i problemy primeneniya titanovyh splavov [Perspectives and problems of application of titanium alloys] / V sb. Aviacionnye materialy i tehnologii. M.: VIAM, 2007. Vyp. «Perspektivy razvitiya i primeneniya titanovyh splavov dlya samoletov, raket, dvigatelej i sudov». S. 4–8.
  7. Horev A.I., Belov S.P., Glazunov S.G. Metallovedenie titana i ego splavov [Metallurgical science of titanium and its alloys]. M.: Mashinostroenie, 1992. 351 s.
  8. Antashev V.G., Nochovnaya N.A. Sovremennoe sostoyanie i tendencii razvitiya issledovanij v oblasti titanovyh splavov [Current state and tendencies of development of researches in the field of titanium alloys] // Vse materialy. Enciklopedicheskij spravochnik. 2008. №3. S. 24–27.
  9. Nochovnaya N.A., Ivanov V.I., Alekseev E.B., Kochetkov A.S. Puti optimizacii ekspluatacionnyh svojstv splavov na osnove intermetallidov titana [Ways of optimization of operational properties of alloys on the basis of titanium intermetallic compound] //Aviacionnye materialy i tehnologii. 2012. №S. S. 196–206.
  10. Kashapov O.S., Novak A.V., Nochovnaya N.A., Pavlova T.V. Sostoyanie, problemy i perspektivy sozdaniya zharoprochnyh titanovyh splavov dlya detalej GTD [Condition, problems and perspectives of creation of heat resisting titanium alloys for GTE details] // Trudy VIAM: elektron. nauch. tehnich. zhurn. 2013. №3. St. 02. Available at: http://www.viam-works.ru (accessed: January 11, 2016).
  11. Kablov E.N. Rossii nuzhny materialy novogo pokoleniya [Materials of new generation are necessary to Russia] // Redkie zemli. 2014. №3. S. 813.
  12. Horev A.I. Fundamentalnye i prikladnye raboty po konstrukcionnym titanovym splavam i perspektivnye napravleniya ih razvitiya [Fundamental and applied works on structural titanium alloys and perspective directions of their development] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №2. St. 04. Available at: http://www.viam-works.ru (accessed: January 11, 2016).
  13. Prohodtseva L.V., Erasov V.S., Lavrova O.Yu., Lavrov A.V. Vliyanie formy cikla na ustalostnye svojstva i mikrostroenie izlomov titanovogo splava VT3-1 [Influence of form of cycle on fatigue properties and microstructure of breaks of VT3-1 titanium alloy] //Aviacionnye materialy i tehnologii. 2012. №2. S. 54–58.
  14. Gorbovets M.A., Belyaev M.S., Hodinev I.A. Vliyanie ekspluatacionnoj temperatury na skorost rosta treshhiny ustalosti v intermetallidnom titanovom splave [An influence of operating temperature on fatigue crack growth rate for intermetallic titanium alloy] // Aviacionnye materialy i tehnologii. 2013. №3. S. 13–15.
  15. Prohodtseva L.V., Filonova E.V., Naprienko S.A., Moiseeva N.S. Issledovanie zakonomernostej razvitiya processov razrusheniya pri ciklicheskom nagruzhenii splava VT41 [Research of patterns of development of processes of destruction at cyclic loading of alloy VТ41] // Aviacionnye materialy i tehnologii. 2012. №S. S. 407–412.
  16. Belyaev M.S., Gorbovets M.A., Kashapov O.S., Hodinev I.A. Skorost rosta treshhiny ustalosti v zharoprochnom titanovom splave VT41 [Growth rate of crack of fatigue in heat resisting BT41 titanium alloy] // Problemy bezopasnosti poletov. 2013. №8. S. 36–45.
  17. Gorbovets M.A., Belyaev M.S., Hodinev I.A. Metodika ispytanij na skorost rosta treshhiny ustalosti novogo zharoprochnogo intermetallidnogo titanovogo splava [Technique of tests for the growth rate of crack of fatigue of new heat resisting intermetallidny titanium alloy] / V sb. materialov konf. «TestMat–2012». M.: VIAM, 2012 (CD-disk).
  18. Potapov S.D., Perepelitsa D.D. Sposob obrabotki rezultatov ispytanij obrazcov na skorost rosta treshhiny pri postoyannoj amplitude nagruzheniya [Way of processing of test results of samples on crack growth rate with constant amplitude of loading] // Vestnik Moskovskogo aviacionnogo instituta. 2012. T. 19. №.6. S. 94–100.
  19. Terentev V.F. Ciklicheskaya prochnost metallicheskih materialov: ucheb. posobie [Cyclic durability of metal materials: studies. grant]. Novosibirsk: NGTU, 2001. 61 s.
  20. Paris P., Erdogan F. A critical analysis of crack propagation laws // Journal of Basic Engineering (Trans. ASME). 1963. №12. P. 528–534.
  21. Golubovskij E.R., Volkov M.E., Emausskij N.M. Ocenka skorosti razvitiya treshhiny ustalosti v nikelevyh splavah dlya diskov GTD [Assessment of speed of development of crack of fatigue in nickel alloys for disks GTE] // Vestnik dvigatelestroeniya. 2013. №2. S. 229–235.
  22. Korsunsky A.V., Dini D.D., Walsh M.J. Fatigue crack growth rate analysis in a titanium alloy // Key Engineering Materials Vols. 2008. V. 385–387. Р. 5–8.
  23. Niccolls E.H. A correlation for fatigue crack growth rate // Scripta Metallurgica. 1976. V. 10. №4. P. 295–298.
  24. Tanaka K., Matsuoka S. A tentative explanation for two parameters, C and m, in Paris equation of fatigue crack growth // Int. Journal of Fracture. 1977. V. 13. №5. P. 563–584.
  25. Tumanov N.V. Kineticheskoe uravnenie ustojchivogo rosta treshhin malociklovoj ustalosti [Kinetic equation of strong growth of cracks of low-cyclic fatigue] // Vestnik SGAU. 2014. №5 (47). Ch. 1. S. 18–26.
  26. Potapov S.D., Perepelica D.D. Issledovanie ciklicheskoj skorosti rosta treshhin v materialah osnovnyh detalej aviacionnyh GTD [Research of cyclic growth rate of cracks in materials of the main details of aviation GTE] // Tehnologiya legkih splavov. 2013. №2. S. 5–19.
  27. Kumar V., Nagalaxmi G. Fatigue Crack Growth Behavior of a near α IMI-834 Titanium Alloy at Elevated Temperature // Engineering Fracture Mechanics. 2001. №68. Р. 129–147.
  28. Boyce B.L., Ritchie R.O. Effect of load ratio and maximum stress intensity on the fatigue threshold in Ti–6Al–4V // Engineering Fracture Mechanics. 2001. V. 68. №.2. P. 129–147.
  29. Oberwinkler B. Modeling the fatigue crack growth behavior of Ti–6Al–4V by considering grain size and stress ratio // Materials Science and Engineering A. 2011. V. 528. P. 5983–5992.
  30. Sansoz F., Ghonem H. Effects of loading frequency on fatigue crack growth mechanisms in α/β Ti microstructure with large colony size // Materials Science and Engineering: A. 2003. V. 356. №1–2. P. 81–92
  31. Bache M.R. A review of dwell sensitive fatigue in titanium alloys: the role of microstructure, texture and operating conditions // International Journal of Fatigue. 2003. №25 (9). P. 1079–1087.