Technique for Estimating the Residual Life of Gas Turbine Engine Blades under High-Temperature Creep

[1] Tyagunov A. G.(2021)Modeling of the dynamics of changes in the heat resistance of nickel alloys by machine learning methods Fiz. Met. Metalloved. 122 754-759

[2] Tarasov D. A.(2019)“Improving the methodology for assessing the residual life of a turbofan engine,” Crede Experto Transport, Obshchestvo, Obrazovanie, Yazyk, No. 2 10-24

[3] Mil’der O. B.(2016)Assessment of service induced degradation of microstructure and properties in turbine blades made of GH4037 alloy J. Alloys Compd. 657 777-786

[4] Karavaev Yu. A.(2020)“Influence of molybdenum and tungsten on the microstructural changes of an alloy after high-temperature holding,” Transport Nauka, Tekhnika, Upravlenie, No. 3 60-63

[5] Khodatskii S. A.(2012)“Development of operational reliability criteria for working and guiding blades of modern gas turbines,” Elektrich Stantsii, No. 2 36-40

[6] Tong J.(1995)Creep behavior of rapidly solidified and processed aluminum alloys Light Weight Alloys Aerospace Appl. III 319-332

[7] Ding X.(2019)Mechanical properties deterioration and its relationship with microstructural variation using small coupons sampled from serviced turbine blades Mater. Sci. Eng., A 757 134-145

[8] Wang M.(2019)A physically based model for correlating the microstructural degradation and residual creep lifetime of a polycrystalline Ni-based superalloy J. Alloys Compd. 783 565-573

[9] Yagi K.(2019)Evaluation of service-induced microstructural damage for directionally solidified turbine blade of aircraft engine Rare Met. 38 157-164

[10] Zheng Y.(2012)Particle size of gamma prime as a result of vacuum heat treatment of Inconel 738 super alloy J. Mater. Eng. Perfor. 22 1143-1148

[1] Tyagunov A. G.(2021)Modeling of the dynamics of changes in the heat resistance of nickel alloys by machine learning methods Fiz. Met. Metalloved. 122 754-759

[2] Tarasov D. A.(2019)“Improving the methodology for assessing the residual life of a turbofan engine,” Crede Experto Transport, Obshchestvo, Obrazovanie, Yazyk, No. 2 10-24

[3] Mil’der O. B.(2016)Assessment of service induced degradation of microstructure and properties in turbine blades made of GH4037 alloy J. Alloys Compd. 657 777-786

[4] Karavaev Yu. A.(2020)“Influence of molybdenum and tungsten on the microstructural changes of an alloy after high-temperature holding,” Transport Nauka, Tekhnika, Upravlenie, No. 3 60-63

[5] Khodatskii S. A.(2012)“Development of operational reliability criteria for working and guiding blades of modern gas turbines,” Elektrich Stantsii, No. 2 36-40

[6] Tong J.(1995)Creep behavior of rapidly solidified and processed aluminum alloys Light Weight Alloys Aerospace Appl. III 319-332

[7] Ding X.(2019)Mechanical properties deterioration and its relationship with microstructural variation using small coupons sampled from serviced turbine blades Mater. Sci. Eng., A 757 134-145

[8] Wang M.(2019)A physically based model for correlating the microstructural degradation and residual creep lifetime of a polycrystalline Ni-based superalloy J. Alloys Compd. 783 565-573

[9] Yagi K.(2019)Evaluation of service-induced microstructural damage for directionally solidified turbine blade of aircraft engine Rare Met. 38 157-164

[10] Zheng Y.(2012)Particle size of gamma prime as a result of vacuum heat treatment of Inconel 738 super alloy J. Mater. Eng. Perfor. 22 1143-1148