An aircraft wing including a fuel tank located in the wing, a channel defining a cavity in the fuel tank, the channel including at least two channel ends terminating at an upper or lower wing surface, a driveshaft located in the cavity; and an access panel located on the wing surface and being movable between an open position so that access to the cavity is permitted, and a closed position so that the cavity is at least partially covered by the access panel to inhibit access to the cavity.
CROSS-WING DRIVESHAFT CHANNEL
22.03.2018
Patent
Elektronische Ressource
Englisch
Dana takes flight with wing bearing driveshaft
British Library Online Contents | 2002