PSI - Issue 50

E.A. Afanaseva et al. / Procedia Structural Integrity 50 (2023) 1–5 Afanaseva E.A and Afanaseva O.S. / Structural Integrity Procedia 00 (2023) 000–000

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4. Conclusion

The article considers a new numerical method for calculating the individual residual life for a leader-item. This method does not require analytical relations linking generalized loads with generalized forces, and accurate knowledge of the nature and magnitude of loads for a set of items. The article presents the approbation of the method on the example of individual forecasting of the wear of the landing gear of the aircraft.

References

Bolotin, V.V., 1984. Forecasting resource machines and structures. Mashinostroenie, Moscow, pp. 312. Frolov, K.V., 1984. Methods for improving machines and modern problems of mechanical Engineering. Mashinostroenie, Moscow, pp. 223. Frolov, K.V., Zubov, I. V., Izrailev, Yu. L., et al.,1986. Extending the period of safe operation of power-generating equipment between major overhauls. Strength of Materials, vol. 18, no. 5, 553–563. Radchenko, V.P., Dudkin, S.A., Timofeev, M. I., 2002. Experimental study and analysis of the inelastic micro- and macro-inhomogeneity fields of AD-1 alloy. J. Samara State Tech. Univ., Ser. Phys. Math. Sci. no. 16, 111–117. Gromakovskii, D.G., Radchenko, V.P., Averkieva, V.I., et al., 1988. Development of a system for diagnosing friction units based on the sti ff ness method. Vestnik mashinostroeniya, no. 8, 10–14. Venttsel’, E.S., Ovcharov, L.A., 1969. Theory of Probability. Nauka, Moscow, pp. 368.

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