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1. (WO2018195622) BINARY-CYCLE TURBINE ENGINE COMPRISING THREE ISOTHERMAL PROCESSES AND FOUR ADIABATIC PROCESSES AND A METHOD FOR CONTROLLING THE THERMODYNAMIC CYCLE OF THE TURBINE ENGINE

Pub. No.:    WO/2018/195622    International Application No.:    PCT/BR2018/050111
Publication Date: Fri Nov 02 00:59:59 CET 2018 International Filing Date: Wed Apr 18 01:59:59 CEST 2018
IPC: F01D 1/04
F02C 1/05
F01D 17/00
Applicants: ASSOCIAÇÃO PARANAENSE DE CULTURA - APC
Inventors: IOCKHECK, Marno
FINCO, Saulo
MOURA, Luis Mauro
Title: BINARY-CYCLE TURBINE ENGINE COMPRISING THREE ISOTHERMAL PROCESSES AND FOUR ADIABATIC PROCESSES AND A METHOD FOR CONTROLLING THE THERMODYNAMIC CYCLE OF THE TURBINE ENGINE
Abstract:
The present invention relates to a heat engine containing an isothermal expansion heating chamber (22), a three-way proportional control valve (23), two turbine rotors (24) and (25) and two compressor rotors (26) and (27), all connected to the shaft (210), a thermally insulated isothermal compression chamber (29) and an isothermal compression cooling chamber (28). These components form two subsystems, an energy conversion subsystem and an energy conservation subsystem, wherein both implement an interdependent, but not differential, binary thermodynamic cycle. Operating with gas, implementing a thermodynamic cycle comprising seven continuous processes, that is to say all the processes take place simultaneously, three of these processes being "isobaric" and four being "adiabatic" with variable mass transfer from one of the subsystems to the other dynamically, which transfer may be zero or partial.