A WING ARRANGEMENT FOR AN AIRCRAFT

The present invention relates to a wing arrangement for an aircraft, comprising a wing (9) having a base section (11) and a tip section (13) pivotably connected to base section (11) such that the tip section (13) is pivotable about a tip section pivot axis (17) between a deployed position and a stow...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Briancourt, Stephen, Brakes, David, Ellmers, Wilfried, Winkelmann, Christoph
Format: Patent
Sprache:eng ; fre ; ger
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