A wing assembly for an aircraft is disclosed having a spar, a wing cover, and a rib. The spar has a web portion and a flange portion joined by a radius corner, wherein a gap is formed at an interface between the spar, the wing cover and the rib. The assembly further includes a seal member which substantially covers the gap, and sealant provided between the seal member and the rib and/or the wing cover and/or the spar so as to seal the gap.
Seal assembly for an aircraft wing
11.08.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |