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Combustion and heat transfer in gas turbine systems : proceedings /
Combustion and Heat Transfer in Gas Turbine Systems is a compilation of papers from the Proceedings of an International Propulsion Symposium held at the College of Aeronautics, Cranfield in April 1969. This compilation deals with research done by academic and scientific institutions and of industria...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor Corporativo: | |
| Otros Autores: | |
| Formato: | Electrónico Congresos, conferencias eBook |
| Idioma: | Inglés |
| Publicado: |
Oxford ; New York :
Pergamon Press,
[1971]
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| Edición: | [1st ed.]. |
| Colección: | Cranfield international symposium series ;
v. 11. |
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Front Cover; Combustion and Heat Transfer in Gas Turbine Systems; Copyright Page; Table Of Contents; FOREWORD; SESSION 1; Chapter 1. THE COMBUSTION SYSTEM FOR THE OLYMPUS 593 CONCORDE ENGINE; Operating Conditions; Combustion Performance Criticality; Altitude Relight Considerations; Metal Temperatures; Smoke; Light-weight Fuel System Introduction; Flame Tube Design; Cooling Rings; Subsequent Development; Mechanical Improvements; Combustion Efficiency and Pressure Loss; L.P. Fuel Sprayer; Chapter 2. THE COMBUSTION SYSTEM FOR THE OLYMPUS 593 CONCORDE ENGINE; Discussion.
- Chapter 3. THE STATISTICAL ANALYSES OF COMBUSTION CHAMBER TEMPERATURE PROFILESIntroduction; Statistical Terminology; Tubo-Annular Chambers; Annular Chambers; Comments; Chapter 4. THE STATISTICAL ANALYSES OF COMBUSTION CHAMBER TEMPERATURE PROFILES; Discussion; SESSION 2; Chapter 5. THE EVOLUTION OF THE RB 162 COMBUSTION SYSTEM FOR V.T.O.L. APPLICATIONS; 1.0. Introduction; 2.0. Engine Design Requirements; 2.1. Engine Operational Requirements; 2.2. Description of Engine (Fig. 4); 3.0. Combustor Design Requirements; 3.1. Combustor Operational Requirements; 4.0. Research Experience.
- 4.1. Double Banking4.2. The Single Reversal Combustor; 5.0. The RB 162 Combustor Design; 6.0. The Development Process; 6.1. Acceleration Heat Release; 6.2. Aerodynamics; 6.3. Exit Temperature Distribution; 6.4. Ignition; 6.5. The Compressor/Combustor Interface; 6.6. Fuel Injection; 7.0. The Current Situation; 8.0. Acknowledgements; Reference; Chapter 6. THE EVOLUTION OF THE RB 162 COMBUSTION SYSTEM FOR V.T.O.L. APPLICATIONS; Discussion; Chapter 7. SOME COMBUSTION ASPECTS OF PLENUM CHAMBER BURNING; Summary; 1. Brief History; 2. Lift/Thrust or ""Vectored Thrust"" Turbofan Engines.
- 3. The Advantages of P.C.B.4. The Practical Problems of P.C.B.; 5. The Staggered Gutter Colander; 6. Adaptation to P.C.B. and Some Design Considerations; 7. The Experimental Research and Development Programme; 8. Development of Colander Details; 9. Performance Achieved; 10. Nozzles Vertical Testing; 11. Later P.C.B. Systems; 12. Acknowledgements; Chapter 8. SOME COMBUSTION ASPECTS OF PLENUM CHAMBER BURNING; Discussion; SESSION 3; Chapter 9. A SURVEY OF ANNULAR VAPORIZING COMBUSTION CHAMBERS; Introduction; Historical Background; General Concept of Mode of Operation; Performance Characteristics.
- ConclusionsAcknowledgements; Chapter 10. A SURVEY OF ANNULAR VAPORIZING COMBUSTION CHAMBERS; Discussion; Chapter 11. IGNITION THEORY AND ITS APPLICATION TO THE ALTITUDE RELIGHTING PERFORMANCE OF GAS TURBINE COMBUSTORS; Introduction; Ignition Theories; Alternative Theory; Application of Theory to Gas Turbine Ignition; Discussion; References; Nomenclature; Chapter 12. IGNITION THEORY AND ITS APPLICATION TO THE ALTITUDE RELIGHTING PERFORMANCE OFGAS TURBINE COMBUSTORS; Discussion; References; References; SESSION 4; Chapter 13. PREMIXED PRIMARY ZONE STUDIES USING A MULTIPLE-PORT BAFFLE.