References
- [1] Kolotnikov, M.ye., 2003, “Predel’noe sostoyanie i prognozirovanie resursa GTD v usloviyah mnogokomponentnogo nagruzheniya” [Marginal State and Life Prediction of GTE Under Multi- Component Loading. Edited by V.M. Chepkin], Rybinsk State Aviation Engineering Academy, Rybinsk.
- [2] Ceytlin, v.I., 1974, “Ocenka prochnosti detalej v usloviyah mnogokomponentnogo nagruzheniya” [Strength of Parts Estimation Under Multi-Component Loading Conditions], Aero Gas Turbine Engines Designing and Development, Issue 67, pp. 123-131.
- [3] Kuznetsov, N.D., and Ceytlin, v.I., 1976, Ekvivalentnye ispytaniya gazoturbinnyh dvigatelej [Equivalent Testing of Gas Turbine Engines], Mechanical Engineering publishing, Moscow.
- [4] Ceytlin, v.I., and Fedorchenko, D.G., 1983, “Ocenka ciklicheskoj dolgovechnosti detalej, rabotayushchih pri slozhnyh programmah nagruzheniya” [Estimation of Cyclic Durability of the Parts that Operate Under Complex Loading Programs], problems of Strength, 2, pp. 13-19.
- [5] Anurov, yu.M., and Fedorchenko, D.G., 2004, “Osnovy obespecheniya prochnostnoj nadezhnosti aviacionnyh dvigatelej i silovyh ustanovok” [Bases of Strength Reliability of Aero Engines and Power Plants], Saint-petersburg State polytechnic University, Saint-petersburg.
- [6] Birger, I.A., Shorr, B.F., and Iosilevych, G.B., 1979, Raschet na prochnost’ detalej mashin [Strength Analysis of Machine Elements], Mechanical Engineering publishing, Moscow.
- [7] Sinayskii, B.N., pogrebnyak, A.D., and Ischenko, I.I., 1976, “O temperaturnoj zavisimosti ustalostnoj prochnosti zharoprochnyh nikelevyh splavov” [About Temperature Relation of Heat-Resistant Nickel- base Alloys], problems of Strength, 5, pp. 13-18.
- [8] Orlov, A.F., Balashov, B.F., 1990, “Nekotorye osobennosti nakopleniya povrezhdenij dlya GTD pri malociklovom nagruzhenii i povyshennyh temperaturah” [Several Peculiarities of Damage Accumulation for GTE Under Lo-Cyclic Loading and High Temperature], Low-Cycle Fatigue of Structural Elements, III All-Union Symposium, pp. 45-54.
- [9] Balashov, B.F., Birger I.A., Bychkov, N.G. et. al., 1990, “Resursnoe proektirovanie aviacionnyh GTD. Rukovodstvo dlya konstruktorov” [Life-Time Designing of Aero Engines. Designer’s Textbook], Central Institute of Aero Engines, Moscow, Issue 1.
- [10] Birger, I.A., Shorr B.F., 1975, Termoprochnost’ detalej mashin [Thermal Strength of Machine Elements], Mechanical Engineering publishing, Moscow.
- [11] He, J., Sandstrom, R., and Vujic, S., 2016, “Creep, low cycle fatigue and creep-fatigue properties of a modified HR3C”, 21st European Conference on Fracture, ECF21, 20-24 June 2016, Catania, Italy.
- [12] Porter, A.M., Bukatii, S.A., and Vodolagin, A.L., 2009, “Issledovanie vliyaniya dlitel’nosti dejstviya maksimal’nyh napryazhenij v cikle nagruzheniya na malociklovuyu ustalost’ i dlitel’nuyu prochnost’ vala GTD iz materiala EI 961-SH” [Investigation of influence of maximum stresses action duration in loading cycle on the low-cyclic fatigue and long-term strength of gas turbine engine shaft made of EI 961-Sh material], Bulletin of Samara State Aerospace University, 3(19), pp. 56-63.
- [13] Bukatii, S.A., and Okrugin, A.A., 2014, “Issledovanie ciklicheskoj dolgovechnosti materiala v usloviyah malociklovoj ustalosti i dlitel’noj prochnosti” [Investigation of material cyclic durability under conditions of low-cycle fatigue and long-term strength], Bulletin of Samara State Aerospace University, 5(47), pp. 72-77.
- [14] Sheremetev, A.v., 2018, “Ob uchete mnogokomponentnogo nagruzheniya pri obespechenii prochnostnoj nadezhnosti detalej aviacionnyh GTD” [About the calculation of polycomponent loading at the providing strength reliability of the aviation GTE components], Bulletin of Engine Design, 2, pp. 164-169.