Aerodynamic component with deformable skin
The aerodynamic component (1) has a supporting region formed between the supporting element and the outer shell, for transferring deformation forces from the supporting element to the outer shell. A supporting element changes the distance of the supporting region from a longitudinal plane of the aer...
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| Format: | Patent |
| Sprache: | eng ; fre ; ger |
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| Zusammenfassung: | The aerodynamic component (1) has a supporting region formed between the supporting element and the outer shell, for transferring deformation forces from the supporting element to the outer shell. A supporting element changes the distance of the supporting region from a longitudinal plane of the aerodynamic component with a rotation of the supporting element. The elastic deformation region deforms elastically by the deformation forces, with a change of the distance of the supporting region from the longitudinal plane caused by a rotation of the supporting element. |
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