binary cycle turbine engine composed of three isothermal processes, four adiabatic processes and control process for the thermodynamic turbine engine cycle

摘要

The present invention relates to a turbine-type thermal motor and its seven-process thermodynamic cycle, more specifically a thermal machine characterized by an energy conversion subsystem and an energy conservation subsystem and both perform a thermodynamic cycle. Interdependent but non-differential torque, operates on gas, this system performs a thermodynamic cycle composed of seven continuous processes, that is, all processes occur simultaneously, three of these? isothermal? and four? adiabatic? with variable mass transfer from one of the subsystems to the other dynamically, which may be null or partial.