| 摘要 |
<p>The invention relates to a structural frame for an aircraft fuselage, comprising a lower arched structure (1), a cross-piece (2), supporting a floor element (3) and a connecting lattice (4), between the lower arch (1) and the cross-piece (2). More particularly, said connecting lattice (4) may comprise bars (4a, 4b), the ends of which are spliced to the cross-piece (2) and the lower arch (1).</p> |
