| 摘要 |
A single wing for an unmanned aircraft (400) adapted for image acquisition, surveillance or other applications consists of a ribbed frame (100) and a foam (200) wherein the ribbed frame (100) is integrated during molding for stiffness and strength. The foam (200) has a container (301, 302, 303) for holding the electric and/or electronic components. The foam (200) constitutes the outer layer of the unmanned aircraft (400) at impact side(204, 205, 206).The wing can be produced at low cost and low complexity in large volumes, increases the impact resistance and safety when used in civil areas, and is removable and disposable thereby enabling reuse of the electric and/or electronic components.
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