An aircraft is provided and includes fuselage having a nose, a main section aft of the nose and a tail aft of the main section, an engine nacelle partially embedded in the tail and including a boundary layer ingestion (BLI) propulsor with an inlet directly adjacent to the fuselage and a nozzle element disposed upstream from the inlet and configured to accelerate boundary flows flowing toward the interior side of the engine nacelle.
SYSTEM TO PROMOTE ACCELERATED BOUNDARY LAYER INGESTION
2020-06-18
Patent
Elektronische Ressource
Englisch
System to promote accelerated boundary layer ingestion
Europäisches Patentamt | 2021
|SYSTEM TO PROMOTE ACCELERATED BOUNDARY LAYER INGESTION
Europäisches Patentamt | 2022
|