| 摘要 |
Interface arrangement between a first component (11) and a second component (21) of an aircraft structure having an aerodynamic contour, such as a wing skin and a wing leading edge panel, both components being made of composite material, the first component (11) having a joggle so that it includes a first area (13) which surface (15) belongs to the aircraft aerodynamic contour and a second area (17) where the joint with the second component (21) takes place, the second component (21) having a surface (23) belonging to the aircraft aerodynamic contour, in which an intermediate part (31) made of a composite material or a plastic material and suitable shaped for maintaining the continuity of the aircraft aerodynamic contour in the interface area between said components (11, 13) as well as to fill the expected gap (25) between said components (11, 13), is joined to the first component (21). |
