The body (1) has a wing box (2) provided with two opposite wing shells (4a, 4b). A wing leading edge (3) is arranged in front of the wing box along flow direction (S). The wing shells are made of fiber composite material. The wing shells and the wing leading edge are provided with projecting fastening elements (6a, 6b, 7) in interior of the wing body. Connection elements (8) are fixed in the projecting fastening elements. The wing leading edge is connected to the wing box to form an airfoil.
申请公布号
EP2712803(B1)
申请公布日期
2016.05.18
申请号
EP20130186492
申请日期
2013.09.27
申请人
DEUTSCHES ZENTRUM FÜR LUFT- UND RAUMFAHRT E.V.;AIRBUS OPERATIONS LIMITED
发明人
BOLD, JENS;ÜCKERT, CHRISTIAN;STEFFEN, OLAF;HÜHNE, DR. CHRISTIAN;HOLMES, VERNON