| 摘要 |
An aircraft wing torsion box (100) is provided, the 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 comprising:
a support member (101) comprising a front spar (102) and a rear spar (103) and a connecting portion (106,104,108,105,107) between the front and rear spars, the connecting portion comprising 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),
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. |
