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Gas turbines: technology, efficiency, and performance / Donna J. Ciafone, editor

Published
Hauppauge, New York : Nova Science Publisher's, [2011]
Physical Description
1 online resource
Additional Creators
Ciafone, Donna J.
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Language Note
English.
Contents
GAS TURBINES: TECHNOLOGY, EFFICIENCY AND PERFORMANCE ; GAS TURBINES: TECHNOLOGY, EFFICIENCY AND PERFORMANCE; CONTENTS ; PREFACE ; COMPREHENSIVE TECHNO-ECONOMIC EVALUATION OF GAS TURBINE REPOWERING SYSTEMS FOR UTILIZING WASTE HEAT FROM A SMALL SCALE REFUSE INCINERATION PLANT ; ABSTRACT ; 1. INTRODUCTION ; 2. OUTLINE OF INVESTIGATED SYSTEMS ; 2.1. Outline of a Refuse Incineration Plant and a Waste Heat Which Is Utilized ; 2.2. Outline of a System to Be Repowered ; 2.3. Outline of a Conventional Repowering System ; 2.4. Outline of the Proposed Repowering System (S-P1)., 2.5. Outline of the Proposed Repowering System (S-P2) 3. EVALUATION OF THERMODYNAMIC CHARACTERISTICS; 3.1. Premises ; 3.2. Estimated Characteristics of the STPS ; 3.3. Estimated Characteristics of The S-C ; 3.4. Estimated Characteristics of the S-P1 ; 3.5. Estimated Characteristics of the S-P2 ; 3.6. Discussions on the Estimated Thermodynamic Characteristics ; 3.7. Comparison of Thermodynamic Characteristics of the Rpss ; 4. EVALUATION OF ECONOMICS AND CO2-REDUCTION CHARACTERISTICS ; 4.1. Premises ; 4.2. Evaluation Results of the System to Be Repowered., 4.3. Determination of the Best Operating Condition 4.4. Comparison of Economics and CO2 Reduction Characteristics of the Rpss ; 4.5. Discussions on Economical Effects of CO2-Capture of the S-P2 ; CONCLUSIONS; NOMENCLATURE ; ACKNOWLEDGMENTS ; REFERENCES ; IN-SERVICE DEGRADATION OF GAS TURBINE NOZZLES AND MOVING BLADES; ABSTRACT ; 1. INTRODUCTION ; 2. IN-SERVICE DEGRADATION OF THE FIRST STAGE NOZZLE OF A GAS TURBINE ; 2.1. Background ; 2.2. Microstructural Characterization of Nozzle Vane ; 2.3. Cracks Evaluating ; 2.4. Stress Evaluation ; 2.5. Discussion of Results ; 2.6. Conclusion., 3. IN-SERVICE DEGRADATION OF A GAS TURBINE MOVING BLADE MADE OF INCONEL 738LC ALLOY3.1. Background ; 3.2. Microstructural Characterization of a Gas Turbine Blade; Microstructural Evaluation of the Blade Root (Reference Zone) ; Microstructural Evaluation of Blade Hot Section (Airfoil) ; 3.3. Cracks Evaluating ; 3.4. Stress Evaluating ; 3.5 Discussion of Results ; 3.6. Conclusion ; FINAL CONCLUSION ; REFERENCES ; DESIGN AND DEVELOPMENT OF SMART COATINGS FOR TITANIUM ALLOYS USED IN GAS TURBINES ; ABSTRACT ; 1. INTRODUCTION ; 2. HIGH TEMPERATURE OXIDATION ; 3. LIFE PREDICTION MODELING., and 4. HOT CORROSION CHARACTERISTICS4.1. Degradation Mechanism ; 5. DEVELOPMENT OF HIGH PERFORMANCE COATINGS ; 6. DESIGN AND DEVELOPMENT OF SMART COATINGS ; SUMMARY ; REFERENCES ; THERMODYNAMIC OPTIMIZATION OF AN INTERCOOLED REHEAT REGENERATIVE GAS TURBINE POWER PLANT ; ABSTRACT ; INTRODUCTION; DESCRIPTION OF THE PROCESS ; THERMODYNAMIC MODELING ; Compressors Work ; Turbines Work ; Heat Input ; Work Output and Thermal Efficiency of the Plant ; Regenerator Criterion ; EFFICIENCY OPTIMIZATION ; FINAL NOTES ; CONCLUSION ; NOMENCLATURE ; REFERENCES.
Subject(s)
ISBN
9781614706106 ebook
1614706107
9781611228427 hardcover
1611228425 (electronic bk.)
9781611228427 (electronic bk.)
Digital File Characteristics
data file
Bibliography Note
Includes bibliographical references and index.
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