Q Michalski, B Boust, M Bellenoue - 2018 Joint Propulsion Conference, 2018 - arc.aiaa.org
Pressure-gain combustion is expected to increase significantly the efficiency of air-breathing turbine engines. The corresponding Humphrey thermodynamic cycle may be implemented …
Les turbomachines actuelles ont atteint un niveau de maturité technique très élevé. De nouvelles architectures reposant sur des cycles thermodynamiques basés sur une …
B Robic - US Patent 11,391,202, 2022 - Google Patents
A module (4) for an aircraft turbomachine comprises an assembly of constant-volume combustion chambers, and including a first sub-assembly of first chambers succeeding each …