| 摘要 |
A structural element for use in aerospace applications comprises: (a) at least one member (12) having an inner surface (4) and an outer surface (2); (b) a rib (3) having a first end (34) and a second end (32); (c) a rib-receiving member (5) integral to the inner surface of the at least one member, wherein the rib-receiving member comprises a plurality of rib-receiving elements (22, 24, 26, 28) and openings therein for receiving the first end of the rib and at least one cover sheet (16) having an opening therein for receiving the first end of the rib; and (d) at least one anchoring element (100) interconnecting the rib-receiving elements. <IMAGE> |
