Selection of reference specimens for assessing the efficiency of part surface nitriding


Cite item

Full Text

Abstract

The use of corset reference specimens for carrying out fatigue tests and smooth reference specimens for determining residual stresses in a surface layer to assess the sufficiency of nitriding (thermochemical processing) is substantiated in the paper. The calculations are carried out by finite element simulation using the ANSYS and PATRAN/NASTRAN software complexes. The ANSYS complex is used to determine the stress concentration factor for the case of corset specimen bending. The employed models with harmonic axisymmetric finite elements make it possible to find the stress concentration factors in the case of tension- and- compression and bending of body-of-rotation parts. The obtained value of the influence of the coefficient of residual stresses on the endurance limit increase is in quite good agreement with its experimental values for nitriding and other types of thermochemical treatment of corset specimens. The PATRAN/NASTRAN complex is used to calculate the stress-strain state in corset specimens depending on residual stresses arising on a part surface under nitriding. Modeling is performed by the thermoelasticity method, with experimental diagrams of residual stresses in smooth specimens used as initial data. It is established that the distribution of axial residual stresses in the dangerous (smallest) section of a corset specimen practically does not differ from the distribution in smooth specimens. The results obtained provide the basis for determining average integral residual stresses by the distribution of residual stresses in smooth specimens and using them to calculate the endurance limit for hardened corset specimens. The results of the study allow making a conclusion that the most optimal nitriding practices are those wherein the average integral residual stresses are maximal. 

About the authors

V. V. Sazanov

Samara National Research University

Author for correspondence.
Email: sopromat@ssau.ru

Postgraduate Student of the Department of Strength of Materials

Russian Federation

References

  1. Pavlov V.F., Kirpichev V.A, Vakulyuk V.S. Prognozirovanie soprotivleniya ustalosti poverkhnostno uprochnennykh detaley po ostatochnym napryazheniyam [Prediction of surface hardened parts’ fatigue resistance by residual stresses]. Samara: Samarskiy Nauchnyy Tsentr RAN Publ., 2012. 125 p.
  2. Pavlov V.F. On connection between residual stresses and the endurance limit under bending in stresses concentration conditions. Proceedings of Higher Educational Institutions. Маchine Building. 1986. No. 8. P. 29-32. (In Russ.)
  3. Pavlov V.F. Influence of a value and a distribution of residual stresses in the surface layer of a part with a concentrator on the endurance limit. Report 1. Solid parts. Proceedings of Higher Educational Institutions. Маchine Building. 1988. No. 8. P. 22-26. (In Russ.)
  4. Kirpichyov V.A., Filatov A.P., Karanaeva O.V., Chirkov A.V., Semyonova O.Yu. Surface hardened parts endurance limit prediction under various degree of stress concentration. Proceedings International Conference «Strength of materials and structural elements». Kiev: G.S. Pisarenko Institute for Problems of Strength of the National Ac. Sci. of Ukraine Publ., 2011. P. 678-685. (In Russ.)
  5. Peterson R.E. Stress concentration factors. New York: Wiley, 1974. 146 p.
  6. Chirkov A.V., Sazanov V.P., Samoylov V.A., Larionova Y.S. Modeling of redistribution of residual stresses in the cylindrical specimens after advancing surface plastic forming. Vestnik of the Samara State Aerospace University. 2011. No. 3 (27), part 3. P. 171-174. (In Russ.)
  7. Ivanov S.I. K opredeleniyu ostatochnykh napryazheniy v tsilindre metodom kolets i polosok. Sb. trudov «Ostatochnye napryazheniya». Iss. 53. Kuibyshev: Kuibyshev Aviation Institute Publ., 1971. P. 32-42. (In Russ.)

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2017 VESTNIK of Samara University. Aerospace and Mechanical Engineering

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies