An aircraft (101) is provided and includes fuselage (110) having a nose (111), a main section (112) aft of the nose (111) and a tail (113) aft of the main section (112), an engine nacelle (130) partially embedded in the tail (113) and including a boundary layer ingestion (BLI) propulsor (131) with an inlet (132) directly adjacent to the fuselage (110) and a nozzle element (140) disposed upstream from the inlet (132) and configured to accelerate boundary flows flowing toward the interior side (1321) of the engine nacelle (130).
SYSTEM TO PROMOTE ACCELERATED BOUNDARY LAYER INGESTION
SYSTEM ZUR FÖRDERUNG VON BESCHLEUNIGTER GRENZSCHICHTAUFNAHME
SYSTÈME VISANT À PROMOUVOIR L'INGESTION ACCÉLÉRÉE DE COUCHES LIMITES
2022-03-16
Patent
Elektronische Ressource
Englisch
System to promote accelerated boundary layer ingestion
Europäisches Patentamt | 2021
|SYSTEM TO PROMOTE ACCELERATED BOUNDARY LAYER INGESTION
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