| 摘要 |
A method of manufacturing an aircraft component, the component comprising a pair of covers (2,3) joined by a pair of spars (4,5). The covers and spars form a closed box structure with four corners (6,7,8,9), each corner providing a transition between one of the covers and one of the spars. The method comprises: laying up a laminated sheet of fibre plies; and after the sheet has been laid up, folding the sheet to form the four corners and then joining the sheet to itself to provide the closed box structure. |
