The invention relates to an aircraft (41) comprising a fuselage (14) comprising a skin (15) and extending along a longitudinal axis (39) from a front end to a rear end (17) of the aircraft, and an engine (30) comprising an air intake (31) forming an opening in the skin (15), as wells as an exhaust (32) forming another opening in the skin (15), said engine being located in a rear fuselage section, in which the exhaust (32) is situated ahead of the air intake (31) along the longitudinal direction (39).
AIRCRAFT WITH A COMBUSTION ENGINE HAVING AN EXHAUST AHEAD OF ITS AIR INTAKE
FLUGZEUG MIT EINER BRENNKRAFTMASCHINE MIT EINEM AUSPUFF VOR SEINEM LUFTEINLASS
AÉRONEF ÉQUIPÉ D'UN MOTEUR À COMBUSTION INTERNE AYANT UN ÉCHAPPEMENT EN AVANT DE SON ADMISSION D'AIR
2024-05-29
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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