An aircraft wing with a wing tip device and a strut

An aircraft wing 1 has a wing tip device 3 joined thereto. The root 7 of the wing tip device 3 is joined to the tip of the wing 1 at a first connection 11. An external strut 9 extends between the wing 1 and the wing tip device 3, the strut 9 being joined to the wing 1 at a second connection 13. The...

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Bibliographische Detailangaben
Hauptverfasser: ROBERT IAN THOMPSON, CHRISTOPHER LYNAS, LLIFON WILLIAMS, JOHN HOBDAY
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:An aircraft wing 1 has a wing tip device 3 joined thereto. The root 7 of the wing tip device 3 is joined to the tip of the wing 1 at a first connection 11. An external strut 9 extends between the wing 1 and the wing tip device 3, the strut 9 being joined to the wing 1 at a second connection 13. The second connection 13 is inboard of the first connection, such that loadings on the wing tip device 3 generated during use, are transferred, via the strut 9, to a location on the wing 1 that is inboard of where the root 7 of the wing tip device 3 is joined to the tip of the wing.