| 摘要 |
The invention relates mainly to a wing for the propulsion of a vehicle, characterised in that it comprises an outer shell (11) and at least one airfoil structure (10) surrounded by said outer shell (11), said airfoil structure (10) having a hinged inner structure (12), and a set of means (13.1-13.5, 14) for controlling a deformation of said outer shell (11), each control means (13.1-13.5, 14) being rotatably mounted relative to said inner structure (12). Furthermore each control means (13.1-13.5, 14) is rotatably mounted relative to said outer shell (11) via at least one rotary link (16, 17, 21) and comprises at least one curved surface (18, 19, 18', 19', 22) configured such as to guide a curve of said outer shell (11) locally between said control means (13, 14) and an adjacent control means (13, 14). |
