Optimizing Gas-Turbine Cycle Network
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Questions and Answers

What is the primary reason for operating gas turbines at four times the air needed for complete combustion?

  • To reduce excessive temperatures (correct)
  • To increase thermal efficiency
  • To decrease fuel consumption
  • To increase power output
  • What happens to the working fluid temperature when intercooling and reheating are utilized?

  • It decreases at both the compressor and turbine
  • It increases at the compressor and decreases at the turbine
  • It decreases at the compressor and increases at the turbine (correct)
  • It increases at both the compressor and turbine
  • Why does the back work ratio of a gas-turbine cycle improve with intercooling and reheating?

  • Because the turbine exhaust temperature increases
  • Because the thermal efficiency increases
  • Because the regeneration potential increases (correct)
  • Because the compressor inlet temperature decreases
  • What is the effect of intercooling and reheating on the thermal efficiency of a gas-turbine cycle?

    <p>It decreases the thermal efficiency unless accompanied by regeneration</p> Signup and view all the answers

    What is the ideal limit of thermal efficiency that can be approached by a gas-turbine cycle with intercooling, reheating, and regeneration?

    <p>The Carnot efficiency</p> Signup and view all the answers

    What is the primary goal of multistage compression with intercooling in a gas-turbine cycle?

    <p>To decrease the compression work by reducing the specific volume of the fluid</p> Signup and view all the answers

    What happens to the compression process as the number of stages is increased?

    <p>The compression process becomes isothermal at the compressor inlet temperature</p> Signup and view all the answers

    What is the effect of reheating on the expansion process in a gas-turbine cycle?

    <p>It increases the expansion work output without raising the maximum temperature</p> Signup and view all the answers

    What is the principle behind the effect of multistage compression with intercooling and multistage expansion with reheating on the net work output?

    <p>The steady-flow work is proportional to the specific volume of the fluid</p> Signup and view all the answers

    What is the ultimate goal of optimizing the compression and expansion processes in a gas-turbine cycle?

    <p>To increase the net work output of the cycle</p> Signup and view all the answers

    Study Notes

    Net Work of a Gas-Turbine Cycle

    • Net work is the difference between turbine work output and compressor work input
    • Net work can be increased by decreasing compressor work, increasing turbine work, or both

    Multistage Compression with Intercooling

    • Compression work can be decreased by carrying out compression in stages and cooling the gas in between
    • As the number of stages increases, the compression process becomes nearly isothermal at the compressor inlet temperature
    • Compression work decreases as the number of stages increases

    Multistage Expansion with Reheating

    • Turbine work output can be increased by expanding the gas in stages and reheating it in between
    • Expansion process becomes nearly isothermal as the number of stages increases
    • Maximum temperature in the cycle remains unchanged

    Principle of Work

    • Steady-flow compression or expansion work is proportional to the specific volume of the fluid
    • Specific volume of the working fluid should be as low as possible during compression and as high as possible during expansion
    • Intercooling and reheating accomplish this by reducing and increasing specific volume, respectively

    Combustion in Gas Turbines

    • Combustion typically occurs with four times the amount of air needed for complete combustion to avoid excessive temperatures
    • Exhaust gases are rich in oxygen, allowing reheating by spraying additional fuel between expansion states

    Effects of Intercooling and Reheating

    • Working fluid leaves the compressor at a lower temperature and the turbine at a higher temperature
    • Makes regeneration more attractive and increases potential for regeneration
    • Back work ratio of a gas-turbine cycle improves
    • Thermal efficiency decreases unless accompanied by regeneration

    Ideal Gas-Turbine Cycle

    • Ideal cycle with intercooling, reheating, and regeneration approaches the Ericsson cycle
    • Thermal efficiency approaches the theoretical limit (Carnot efficiency) as the number of stages increases
    • However, the contribution of each additional stage to thermal efficiency is less and less, and more than two or three stages are not economically justified

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    Description

    This quiz covers the principles of optimizing gas-turbine cycle network by decreasing compressor work or increasing turbine work, including multistage compression with intercooling. It's based on Chapter 7 and Fig. 9-42.

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