The Basic cycle Analysis of simple gas turbine cycle.
THE BASIC CYCLE
Simple cycle gas plants are a type of natural gas
power plant that produces electricity by forcing hot gas through a turbine.
They differ from combined cycle gas plants in that they are solely used to
supply the electrical grid's peak power needs since their waste heat is not
transferred to another external heat engine. These turbines have a high
specific power, which indicates that the amount of power they produce is
comparatively large for their size.
Different power plants, such as coal or nuclear,
provide baseload power to the grid, which meets the minimum electricity
requirements. Peaking power plants, such as simple cycle gas plants, can fulfil
the fluctuating electricity demands. As a result, simple cycle plants have
excellent operational flexibility and may be swiftly started up to suit these
needs. However, because they use less of the energy in the fuel they are using,
this is less efficient than combined cycle plants. These plants have an
efficiency of about 35%.
They compensate for any inefficiency with expense.
According to the EIA, mixed cycle plants cost between US$500 and 550/kW, and
simple cycle plants cost about US$389/kW.
Simple cycle power plants are not used for long
periods of time throughout the year due to their low efficiency and ability to
only provide peaking power. This gives them a very low capacity factor, which
means that they are, on average, not running very close to their maximum
output. At most, these plants are typically only running for a few hours per
day.
Analysis of a Simple Gas Turbine Cycle
The actual performance of a gas turbine plant
differs considerably from the Brayton cycle because of the deviations from the
ideal cycle. These deviations include friction, shock, and heat transfer and
aerodynamic losses in the compressor and turbine, losses in combustion chamber,
piping, mechanical losses, etc. With large number of variables affecting the
performance of the gas turbine plant, it will be really different! Unless it is
possible to estimate its performance, Certain assumptions are made. To simplify
the analysis, consider the following:
Assumptions are made:
l. There is no pressure loss in the combustion
chamber, and in piping, etc.
2. There is no increase in the rate of mass flow
due to the addition of the fuel.
3. The specific heat remains constant at all
temperatures and same for compressor as well as turbine flow.
4. Radiation and mechanical losses are neglected.
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