Национальный Университет Кораблестроения Имени Адмирала Макарова
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Priority to UAU201110305UpriorityCriticalpatent/UA67597U/en
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A gas-turbine engine comprises at least two connected in sequence compressors, a turbine and a heater of compressed air connected to utilization heat exchanger with a circuit of intermediate heat carrier. At that the heater is placed between the compressors. An electric pump of the circuit of intermediate heat carrier can be connected with a frequency transformer to which a sensor of air temperature at inlet to the second compressor is connected.
MODIFICATION OF A GAS TURBINE WITH A SIMPLE CYCLE FOR APPLICATION ASSOCIATED WITH THE ACCUMULATION OF COMPRESSED AIR ENERGY HAVING AN EXTENSION FOR THE GENERATION OF ADDITIONAL POWER
GAS TURBINE (OPTIONS), SYSTEM CONTAINING GAS TURBINE, AND A WAY TO REDUCE THERMAL AND MECHANICAL VOLTAGES ACTING ON A LOADING CONNECTION IN GAS TURBINE