A boundary layer ingestion engine comprising a fan, the fan comprising a disc and a plurality of blades integrally formed with the disc.
BOUNDARY LAYER INGESTION ENGINE WITH INTEGRALLY BLADED FAN DISK
GRENZSCHICHTEINSAUGUNGSTRIEBWERK MIT INTEGRAL BESCHAUFELTER BLÄSERSCHEIBE
MOTEUR À INGESTION DE COUCHE LIMITE AVEC DISQUE AUBAGÉ MONOBLOC DE SOUFFLANTE
2022-04-06
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS |
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