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Extra info for Industrial Gas Turbines

Sample text

55, the discharge temperature, T2, is calculated. e. H2 – H1). 3. 13 Combustion charts Combustion temperature rise (K) The process described above may also be used to compute the heat input in a practical gas turbine cycle, taking into account the variation of specific heats or enthalpies during combustion. In practice, however, the heat input is computed from the combustion chart for a given fuel. The following describes the computation of the combustion temperature rise using combustion charts.

46] where MW is the molecular weight of the air or products of combustion and R0 is the universal gas constant. 2. 44 using the corresponding constants a, b and c given above. 1. When the changes in specific heat are considered in the calculation of compressor and turbine exit temperatures, the process is implicit or iterative. The iterative process begins with computation of the exit temperatures for the compression and expansion process by assuming the exit values for cp and γ for air or products of combustions are equal to the inlet values.

It has been stated that, in any thermodynamic process, the energy is degraded thus making the energy unavailable when increasing the entropy. This feature gives rise to the concept of efficiency in a thermodynamic process such as compression and expansion. 10, consider an ideal compression process where the pressure is increased from P1 to P2 along the process 1 to 2′ and is then followed by an ideal expansion from P2 to P1 along the process 2′ to 1. 10 Ideal and actual compression and expansion processes on the temperature–entropy diagram.

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