{"title":"燃气涡轮发动机高温蠕变工况下涡轮叶片剩余寿命估算方法","authors":"O. Ratenko, Y. Petrov, V. Samoilenko","doi":"10.31044/1814-4632-2022-0-2-12-17","DOIUrl":null,"url":null,"abstract":"A calculation methodology for estimating the residual life of a high-pressure turbine blade based on the taking into account of the morphological state of dispersion-strengthened material is proposed. A good convergence of the calculation results with the experimental data is shown.","PeriodicalId":11136,"journal":{"name":"Deformation and Fracture of Materials","volume":"2 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2022-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Methodology for estimation of residual life of turbine blades of gas turbine engine under high-temperature creep condition\",\"authors\":\"O. Ratenko, Y. Petrov, V. Samoilenko\",\"doi\":\"10.31044/1814-4632-2022-0-2-12-17\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A calculation methodology for estimating the residual life of a high-pressure turbine blade based on the taking into account of the morphological state of dispersion-strengthened material is proposed. A good convergence of the calculation results with the experimental data is shown.\",\"PeriodicalId\":11136,\"journal\":{\"name\":\"Deformation and Fracture of Materials\",\"volume\":\"2 1\",\"pages\":\"\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Deformation and Fracture of Materials\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.31044/1814-4632-2022-0-2-12-17\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Deformation and Fracture of Materials","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.31044/1814-4632-2022-0-2-12-17","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Methodology for estimation of residual life of turbine blades of gas turbine engine under high-temperature creep condition
A calculation methodology for estimating the residual life of a high-pressure turbine blade based on the taking into account of the morphological state of dispersion-strengthened material is proposed. A good convergence of the calculation results with the experimental data is shown.
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