Disclosed is a system for generating power for an aircraft. The system includes a boundary layer ingestion propulser (102) that includes a propulsion fan (104) configured to receive torsional energy from a boundary layer airstream, and a motor generator (106) in operable communication with the propulsion fan and configured to generate power in response to rotation of the propulsion fan.
EMERGENCY POWER GENERATION VIA ELECTRICALLY DRIVEN TAIL CONE BOUNDARY LAYER INGESTION THRUSTER
NOTSTROMERZEUGUNG ÜBER ELEKTRISCH ANGETRIEBENES HECKKEGEL-GRENZFLÄCHENAUFNAHME-GEGENDRUCKELEMENT
GÉNÉRATION D'ÉNERGIE D'URGENCE PAR L'INTERMÉDIAIRE D'UN PROPULSEUR D'INGESTION DE COUCHE LIMITE DE CÔNE DE QUEUE ENTRAÎNÉ ÉLECTRIQUEMENT
2018-09-19
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
EMERGENCY POWER GENERATION VIA ELECTRICALLY DRIVEN TAIL CONE BOUNDARY LAYER INGESTION THRUSTER
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