An aircraft wing torsion box having a front associated with a leading portion of the wing torsion box and a rear associated with a trailing portion of the wing torsion box. The wing torsion box includes a support member having a front spar and a rear spar and a connecting portion between the front and rear spars, the connecting portion includes at least one interposing spar, at least one portion of upper wing skin; and at least one portion of lower wing skin, and at least one portion of the upper wing skin and at least one portion of the lower wing skin being supported by the support member.
AIRCRAFT WING TORSION BOX, AIRCRAFT WING, AIRCRAFT AND SUPPORTING MEMBER FOR USE THEREIN
23.06.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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