Aircraft leading edge apparatuses and corresponding methods

Aircraft leading edge apparatuses and corresponding methods

Aircraft leading edge apparatuses and corresponding methods are disclosed. In one embodiment, an aircraft system includes an airfoil (210) with a leading edge device (220) that is movable among a retracted position, at least one first extended position, and a second extended position. A first actuat...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: AMOROSI, STEPHEN R, RAMPTON, SCOTT N
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:Aircraft leading edge apparatuses and corresponding methods are disclosed. In one embodiment, an aircraft system includes an airfoil (210) with a leading edge device (220) that is movable among a retracted position, at least one first extended position, and a second extended position. A first actuator (260) can be operatively coupled to the leading edge device to move a flow surface (222) between the retracted and the at least one first extended position. A second actuator (270) can be operatively coupled to the leading edge device to move the flow surface between the at least one first extended position and the second extended position.