A propulsor system comprising a propulsor and an exhaust area control mechanism are described. The exhaust area control mechanism is connected to an outlet of the propulsor and is configured to vary the area through which air exits the propulsor system.
PROPULSOR WING TRAILING EDGE EXHAUST AREA CONTROL
PROPULSORFLÜGEL-HINTERKANTENABGASBEREICHSSTEUERUNG
COMMANDE DE ZONE D'ÉCHAPPEMENT DE BORD DE FUITE D'AILE DE PROPULSEUR
2025-03-26
Patent
Electronic Resource
English