Morphing structure for a wing leading edge
The wing leading edge (1) has a deformable shell (2), which is connected to a supporting structure (8) at its two ends (3,4). A fiber composite has a shear-flexible intermediate layer in an area of a neutral fiber of the shell. The shear-flexible intermediate layer is made from an elastomer material...
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| Format: | Patent |
| Sprache: | eng ; fre ; ger |
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| Zusammenfassung: | The wing leading edge (1) has a deformable shell (2), which is connected to a supporting structure (8) at its two ends (3,4). A fiber composite has a shear-flexible intermediate layer in an area of a neutral fiber of the shell. The shear-flexible intermediate layer is made from an elastomer material. A reinforcing fiber areal density is decreased in the composite fiber of the two ends of the shell to a front area (21) of the wing leading edge. |
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