| 摘要 |
Device for gradually dismounting the wings of ultra-light aircrafts for their transportation. It is comprised of a leading edge box spar (1) of removable ribs (3) penetrating in the leading edge box through windows (2') arranged in its rear face. The wing receives a flexible coating (4) stretched rearwardly by a device (6) hooked to the rib, and maintaining the latter in place. The rib holds the upper coating and is guided by a sheath (5) sewn to the coating. The device according to the invention is particularly intended to the ultra-light motorized aircrafts or ultra-light unmotorized aircrafts. |
