Systems and methods are provided for a thrust reverser. The thrust reverser may include one or more flapper doors. The flapper doors may be stored in a stored position within a housing portion of a nacelle of an aircraft propulsor. The flapper doors may then move to a deployed position (e.g., through rotation of the flapper doors or through other movements) when thrust reversing is desired. The aircraft propulsor may further include a thrust reverser door that covers an aperture within the nacelle. When the thrust reverser door is in an open position and the flapper doors are in the deployed position, airflow within the aircraft propulsor may be deflected by the flapper doors and out of the aircraft propulsor through the aperture.
THRUST REVERSER
2017-07-13
Patent
Elektronische Ressource
Englisch
AIAA | 1981
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