An aircraft wing box 100 has a front associated with a leading portion of the wing box and a rear associated with a trailing portion of the wing box. The wing box comprises a support member 101 comprising a front spar 102, a rear spar 103 and a connecting portion between the front and rear spars. The connecting portion comprises at least one interposing spar 104,105. At least one portion of upper wing skin 120 and at least one portion of lower wing skin 130 are supported by the support member. Bracing portions 114,115 and 116 are located between spars and interposing spars.
Aircraft wing box, aircraft wing, aircraft and supporting member for use therein
29.06.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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