Disclosed is a system for generating power for an aircraft. The system includes a boundary layer ingestion propulser that includes a propulsion fan configured to receive torsional energy from a boundary layer airstream, and a motor generator 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
2018-09-20
Patent
Elektronische Ressource
Englisch
EMERGENCY POWER GENERATION VIA ELECTRICALLY DRIVEN TAIL CONE BOUNDARY LAYER INGESTION THRUSTER
Europäisches Patentamt | 2018
|VARIABLE SPEED AC BUS POWERED TAIL CONE BOUNDARY LAYER INGESTION THRUSTER
Europäisches Patentamt | 2018
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