This document provides an overview of gas turbine technologies for electric power generation. It discusses the basic components and principles of operation for gas turbines, including compressors, combustors, and turbines. It also describes the different types of gas turbine plants, such as simple and combined cycle, and their typical applications. The principles of the Brayton cycle and energy transformations within the gas turbine are also summarized. The document outlines the major components and systems of gas turbines as well as common fuels used. Diagrams are included to illustrate gas turbine arrangements and sections.
4. 4
Types of Gas Turbine Plants
Simple Cycle
Operate When Demand is High – Peak Demand
Operate for Short / Variable Times
Designed for Quick Start-Up
Not designed to be Efficient but Reliable
Not Cost Effective to Build for Efficiency
Combined Cycle
Operate for Peak and Economic Dispatch
Designed for Quick Start-Up
Designed to Efficient, Cost-Effective Operation
Typically Has Ability to Operate in SC Mode
5. 5
The energy contained in a flowing ideal gas
is the sum of enthalpy and kinetic energy.
Pressurized gas can store or release energy.
As it expands the pressure is converted to
kinetic energy.
Principles of
Operation
Open Cycle
Also referred to as simple cycle)
Link to picture
8. 8
Principles of Operation
Compressor
As air flows into the compressor, energy is transferred from its
rotating blades to the air. Pressure and temperature of the air
increase.
Most compressors operate in the range of 75% to 85% efficiency.
Combustor
The purpose of the combustor is to increase the energy stored in
the compressor exhaust by raising its temperature.
Turbine
The turbine acts like the compressor in reverse with respect to
energy transformation.
Most turbines operate in the range of 80% to 90% efficiency.
9. 9
Principles of Operation
Overall Energy Transformations (Thermal Efficiency)
Useful Work = Energy released in turbine minus energy absorbed by
compressor.
The compressor requires typically approximately 50% of the energy released by
the turbine.
Overall Thermal Efficiency =
Useful Work/Fuel Chemical Energy *100
Typical overall thermal efficiencies of a combustion turbine are 20% - 40%.