Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel

An aircraft wing arrangement including a wing and at least one strut for attaching the aircraft engine suspended under the wing and including a front zone situated projecting towards the front with respect to a leading edge of the wing. The front zone includes a lateral projection delimiting a later...

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Bibliographische Detailangaben
Hauptverfasser: DANTIN STEPHANIE, FOL THIERRY, JIMENEZ PHILIPPE, GERARD LUDOVIC
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:An aircraft wing arrangement including a wing and at least one strut for attaching the aircraft engine suspended under the wing and including a front zone situated projecting towards the front with respect to a leading edge of the wing. The front zone includes a lateral projection delimiting a lateral air flow channel while being projected towards a proximal end of the wing.