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Gas turbine engines are widely used for power generation because of their high efficiency at many places such as in thermal power plant, aircraft engines etc. Turbine blade is one of the most important components of the engine. It is subjected to very severe working conditions at high temperature with high centrifugal forces. At this working condition, blades are prone to fail due to fatigue, creep and environmental failure. Fatigue failure may be thermal fatigue, mechanical fatigue or Thermo-Mechanical Fatigue (TMF). At high temperature and load, creep is one of the major reasons for failure of components. Therefore, it is necessary to predict the life of components for satisfactory working and to avoid damages due to failures. In this study, turbine blade of Nickel based super-alloy INCONEL-718 and variable amplitude type loading is considered for thermal, mechanical and thermo-mechanical analysis. Finite Element Analysis (FEA) software ABAQUS 6.11 is used to carry out analysis. FE-Safe 6.0, life estimation software was used to get the fatigue life of the turbine blade using Morrow strain-life. Creep life was calculated on the basis of Larson Miller Parameter (LMP).
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Estimation of Life Of Turbine Blade Considering Effect of Creep
Verlag:
LAP LAMBERT Academic Publishing Jun 2021, 2021
ISBN 10: 6203927341
ISBN 13: 9786203927344
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Taschenbuch. Zustand: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Gas turbine engines are widely used for power generation because of their high efficiency at many places such as in thermal power plant, aircraft engines etc. Turbine blade is one of the most important components of the engine. It is subjected to very severe working conditions at high temperature with high centrifugal forces. At this working condition, blades are prone to fail due to fatigue, creep and environmental failure. Fatigue failure may be thermal fatigue, mechanical fatigue or Thermo-Mechanical Fatigue (TMF). At high temperature and load, creep is one of the major reasons for failure of components. Therefore, it is necessary to predict the life of components for satisfactory working and to avoid damages due to failures. In this study, turbine blade of Nickel based super-alloy INCONEL-718 and variable amplitude type loading is considered for thermal, mechanical and thermo-mechanical analysis. Finite Element Analysis (FEA) software ABAQUS 6.11 is used to carry out analysis. FE-Safe 6.0, life estimation software was used to get the fatigue life of the turbine blade using Morrow strain-life. Creep life was calculated on the basis of Larson Miller Parameter (LMP). 88 pp. Englisch. Bestandsnummer des Verkäufers 9786203927344
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Estimation of Life Of Turbine Blade Considering Effect of Creep
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LAP LAMBERT Academic Publishing, 2021
ISBN 10: 6203927341
ISBN 13: 9786203927344
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Zustand: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Gupta Saurabh KumarDr. Saurabh Kumar Gupta is working as an Associate Professor in the Department of Mechanical Engineering Raj Kumar Goel Institute of Technology, Ghaziabad affiliated by AKTU Lucknow, UP India. His research area is . Bestandsnummer des Verkäufers 490936239
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Estimation of Life Of Turbine Blade Considering Effect of Creep
Verlag:
LAP LAMBERT Academic Publishing Jun 2021, 2021
ISBN 10: 6203927341
ISBN 13: 9786203927344
Neu
Taschenbuch
Anbieter: buchversandmimpf2000, Emtmannsberg, BAYE, Deutschland
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Taschenbuch. Zustand: Neu. Neuware -Gas turbine engines are widely used for power generation because of their high efficiency at many places such as in thermal power plant, aircraft engines etc. Turbine blade is one of the most important components of the engine. It is subjected to very severe working conditions at high temperature with high centrifugal forces. At this working condition, blades are prone to fail due to fatigue, creep and environmental failure. Fatigue failure may be thermal fatigue, mechanical fatigue or Thermo-Mechanical Fatigue (TMF). At high temperature and load, creep is one of the major reasons for failure of components. Therefore, it is necessary to predict the life of components for satisfactory working and to avoid damages due to failures. In this study, turbine blade of Nickel based super-alloy INCONEL-718 and variable amplitude type loading is considered for thermal, mechanical and thermo-mechanical analysis. Finite Element Analysis (FEA) software ABAQUS 6.11 is used to carry out analysis. FE-Safe 6.0, life estimation software was used to get the fatigue life of the turbine blade using Morrow strain-life. Creep life was calculated on the basis of Larson Miller Parameter (LMP).Books on Demand GmbH, Überseering 33, 22297 Hamburg 88 pp. Englisch. Bestandsnummer des Verkäufers 9786203927344
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Estimation of Life Of Turbine Blade Considering Effect of Creep
Verlag:
LAP LAMBERT Academic Publishing, 2021
ISBN 10: 6203927341
ISBN 13: 9786203927344
Neu
Taschenbuch
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
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Taschenbuch. Zustand: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Gas turbine engines are widely used for power generation because of their high efficiency at many places such as in thermal power plant, aircraft engines etc. Turbine blade is one of the most important components of the engine. It is subjected to very severe working conditions at high temperature with high centrifugal forces. At this working condition, blades are prone to fail due to fatigue, creep and environmental failure. Fatigue failure may be thermal fatigue, mechanical fatigue or Thermo-Mechanical Fatigue (TMF). At high temperature and load, creep is one of the major reasons for failure of components. Therefore, it is necessary to predict the life of components for satisfactory working and to avoid damages due to failures. In this study, turbine blade of Nickel based super-alloy INCONEL-718 and variable amplitude type loading is considered for thermal, mechanical and thermo-mechanical analysis. Finite Element Analysis (FEA) software ABAQUS 6.11 is used to carry out analysis. FE-Safe 6.0, life estimation software was used to get the fatigue life of the turbine blade using Morrow strain-life. Creep life was calculated on the basis of Larson Miller Parameter (LMP). Bestandsnummer des Verkäufers 9786203927344
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Estimation of Life Of Turbine Blade Considering Effect of Creep
Verlag:
LAP LAMBERT Academic Publishing, 2021
ISBN 10: 6203927341
ISBN 13: 9786203927344
Neu
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Taschenbuch. Zustand: Neu. Estimation of Life Of Turbine Blade Considering Effect of Creep | Saurabh Kumar Gupta | Taschenbuch | Englisch | 2021 | LAP LAMBERT Academic Publishing | EAN 9786203927344 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. Bestandsnummer des Verkäufers 120393156
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