Open rotor type turbomachine for aircraft, has free turbine placed between gas generator and power turbines, and power generator comprising rotor driven in rotation by free turbine, where gas generator comprises high pressure compressor
BEUTIN BRUNO ALBERT, YVON DIDIER JEAN LOUIS, COLIN ANTOINE OLIVIER FRANCOIS, REAUX CLARISSE SAVINE MATHILDE
Year of Publication 30.07.2010
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Year of Publication 30.07.2010
Patent