A thermal calculation based on a table of thermal properties of gas was
carried out for a micro gas turbine system without a recuperator. The
performance parameters of the micro gas turbine system were obtained. The
results of the thermal calculations were verified using Aspen Plus, and it
shows that the thermal calculations fit well with the Aspen simulation
results. Based on this thermal calculation method, the variation of the
performance parameters of the micro gas turbine system under different
pressure and temperature ratios was analyzed. The results show that there is
no optimum pressure ratio within the general design parameters of micro gas
turbines, which leads to extreme values of thermal efficiency. The NOx
generation in the combustion chamber of the micro gas turbine based on the
Zeldovich mechanism was modeled and analyzed by coupling the one-dimensional
thermal calculation model with the NOx emission model. The relationship
between NOx generation rate, molar fuel factor, the characteristic pressure,
and the characteristic temperature was obtained. The results of the analysis
show that, in terms of controlling NOx emissions from a gas turbine, the use
of an increased pressure ratio has a significant advantage over an increased
temperature ratio to improve the thermal efficiency of the micro gas
turbine.