An aircraft propulsion unit comprising an engine and a nacelle including an axisymmetric casing (16) delimiting an air flow path, wherein this casing has at least two openings closed by removable and interchangeable panels (18), at least one of these panels carrying one component (24) of the propulsion unit.
CASING FOR A PROPULSION UNIT
2015-06-25
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |