The present invention provides an engine of a vertical take-off and landing aircraft, wherein the engine is configured to be movable with respect to an aircraft component of the aircraft between a hover position for take-off and landing, and a cruise position for forward flight, wherein the engine comprises an aerodynamic component having at least one aerodynamic element movable between a first position according to a first operational state of the aircraft, and a second position according to a second operational state of the aircraft, the aerodynamic element defining an aerodynamic surface in contact with an airstream passing through the engine.
AIRCRAFT ENGINE COMPRISING A VARIABLE AREA EXHAUST NOZZLE
03.11.2022
Patent
Elektronische Ressource
Englisch
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