A. Rusanov, Gennadii Martynenko, K. Avramov, V. Martynenko
{"title":"用数值模拟方法检测汽轮发电机组事故原因","authors":"A. Rusanov, Gennadii Martynenko, K. Avramov, V. Martynenko","doi":"10.1109/IEPS.2018.8559546","DOIUrl":null,"url":null,"abstract":"The method for an identification of accident causes of turbine-generator sets is suggested. The accident causes can be factors, which are related to the failure of an equipment, and technological factors. For example, a deviation of the structural components from design values is related to these technological factors. The suggested approach is interdisciplinary as a gas dynamic behavior, thermal fields and a dynamic stress-strain state of the bladed disk are analyzed jointly. The approach is based on numerical methods of a gas dynamics and a dynamic strength. The vapor flow through the turbo machine blade lattice is calculated using the viscous compressible gas model. For a numerical integration of the structure a nonlinear finite element model is applied to analyze forced vibrations of the bladed disk under an action of aerodynamic loads.","PeriodicalId":340150,"journal":{"name":"2018 IEEE 3rd International Conference on Intelligent Energy and Power Systems (IEPS)","volume":"23 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"16","resultStr":"{\"title\":\"Detection of Accident Causes on Turbine-Generator Sets by Means of Numerical Simulations\",\"authors\":\"A. Rusanov, Gennadii Martynenko, K. Avramov, V. Martynenko\",\"doi\":\"10.1109/IEPS.2018.8559546\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The method for an identification of accident causes of turbine-generator sets is suggested. The accident causes can be factors, which are related to the failure of an equipment, and technological factors. For example, a deviation of the structural components from design values is related to these technological factors. The suggested approach is interdisciplinary as a gas dynamic behavior, thermal fields and a dynamic stress-strain state of the bladed disk are analyzed jointly. The approach is based on numerical methods of a gas dynamics and a dynamic strength. The vapor flow through the turbo machine blade lattice is calculated using the viscous compressible gas model. For a numerical integration of the structure a nonlinear finite element model is applied to analyze forced vibrations of the bladed disk under an action of aerodynamic loads.\",\"PeriodicalId\":340150,\"journal\":{\"name\":\"2018 IEEE 3rd International Conference on Intelligent Energy and Power Systems (IEPS)\",\"volume\":\"23 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"16\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 IEEE 3rd International Conference on Intelligent Energy and Power Systems (IEPS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/IEPS.2018.8559546\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 IEEE 3rd International Conference on Intelligent Energy and Power Systems (IEPS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/IEPS.2018.8559546","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Detection of Accident Causes on Turbine-Generator Sets by Means of Numerical Simulations
The method for an identification of accident causes of turbine-generator sets is suggested. The accident causes can be factors, which are related to the failure of an equipment, and technological factors. For example, a deviation of the structural components from design values is related to these technological factors. The suggested approach is interdisciplinary as a gas dynamic behavior, thermal fields and a dynamic stress-strain state of the bladed disk are analyzed jointly. The approach is based on numerical methods of a gas dynamics and a dynamic strength. The vapor flow through the turbo machine blade lattice is calculated using the viscous compressible gas model. For a numerical integration of the structure a nonlinear finite element model is applied to analyze forced vibrations of the bladed disk under an action of aerodynamic loads.