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Introduction:
In a Gas Turbine , a Compressor forces air into a combustion chamber where it mixes with fuel. A spark ignites the fuel-air mixture, creating hot high-pressure gas that powers the turbine.
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- Air enters the axial flow compressor at point 1 at ambient conditions.
- Air entering the compressor at point 1 is compressed to some higher pressure. No heat is added; however, compression raises the air temperature so that the air at the discharge of the compressor is at a higher temperature and pressure.
- The air enters the combustion system at point 2, where fuel is injected and combustion occurs.
- The combustion process occurs at essentially constant pressure.
CONTENTS:
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- Introduction & Basics Of Gas Turbine
- Details of Gas Turbine
- Turbine Performance
- Maintenance - inspections
- Some typical problems encountered
- Annexure
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