The aircraft engine can have a core gas path having a first combustor, a second gas path parallel to the core gas path, the second gas path having a second combustor, a turbine driven by the second gas path, a gearbox driven by the turbine, and a valve configured for selectively opening and closing the second gas path.
AIRCRAFT ENGINE AND METHOD OF OPERATING SAME
MOTEUR D`AERONEF ET SON PROCEDE DE FONCTIONNEMENT
2020-12-06
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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