An aircraft wing (308) including a fuel tank (314) located in the wing (308), a channel (336) defining a cavity (313) in the fuel tank (314), the channel (336) including at least two channel ends terminating at an upper or lower wing surface (340, 342), a driveshaft (316) located in the cavity (313); and an access panel (390) located on the wing surface (340, 342) and being movable between an open position so that access to the cavity (313) is permitted, and a closed position so that the cavity (313) is at least partially covered by the access panel (390) to inhibit access to the cavity (313).
CROSS-WING DRIVESHAFT CHANNEL
ANTRIEBSKANAL IN FLÜGELLÄNGSRICHTUNG
CANAL TRANSVERSAL AILAIRE POUR ARBRE DE TRANSMISSION
28.11.2018
Patent
Elektronische Ressource
Englisch
Dana takes flight with wing bearing driveshaft
British Library Online Contents | 2002