ELECTRONICALLY SYNCHRONIZED FLAP SYSTEM

An electronically-synchronized flap system for a fixed-wing aircraft including a first wing (120) including a first flap panel (122), the first flap panel (122) being connected with a first in-board actuator (124) and a first out-board actuator(126), and a second wing (130) including a second flap p...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BAKER, JEFFREY, A, NEELY, JOHN, D, THOMPSON, ANDREW, TORRES, PETER, A
Format: Patent
Sprache:eng ; fre
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