公开(公告)号：US08827206B2

公开(公告)日：2014-09-09

申请号：US13655382

申请日：2012-10-18

Applicant: Gatewing NV

Inventor： Maarten Maurits Van Speybroeck ,  Peter Hendrik Cosyn ,  Maarten Willem Vandenbroucke

IPC: B64C1/00 ,  B64C3/00 ,  B64C5/00

CPC classification number: B64C3/187 ,  A63H27/00 ,  B64C3/20 ,  B64C3/24 ,  B64C39/024 ,  B64C39/028 ,  B64C2039/105 ,  B64C2201/028 ,  B64C2201/127

Abstract: A single wing for an unmanned aircraft adapted for image acquisition, surveillance or other applications consists of a ribbed frame and a foam wherein the ribbed frame is integrated during molding for stiffness and strength. The foam has a container for holding the electric and/or electronic components. The foam constitutes the outer layer of the unmanned aircraft at impact side. 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.

Abstract translation: 适用于图像采集，监视或其他应用的无人驾驶飞机的单翼包括肋框架和泡沫，其中肋框架在模制期间被整合以获得刚度和强度。 泡沫具有用于保持电气和/或电子部件的容器。 泡沫构成冲击侧的无人驾驶飞机的外层。 机翼可以低成本和低复杂性大量生产，当在民用区域中使用时增加抗冲击性和安全性，并且是可拆卸的和一次性的，从而能够重复使用电气和/或电子部件。

公开(公告)号：US20130228645A1

公开(公告)日：2013-09-05

申请号：US13655382

申请日：2012-10-18

Applicant: GATEWING NV

Inventor： Maarten Maurits Van Speybroeck ,  Peter Hendrik Cosyn ,  Maarten Willem Vandenbroucke

IPC: B64C3/18

CPC classification number: B64C3/187 ,  A63H27/00 ,  B64C3/20 ,  B64C3/24 ,  B64C39/024 ,  B64C39/028 ,  B64C2039/105 ,  B64C2201/028 ,  B64C2201/127

Abstract: A single wing for an unmanned aircraft adapted for image acquisition, surveillance or other applications consists of a ribbed frame and a foam wherein the ribbed frame is integrated during molding for stiffness and strength. The foam has a container for holding the electric and/or electronic components. The foam constitutes the outer layer of the unmanned aircraft at impact side. 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.

Abstract translation: 适用于图像采集，监视或其他应用的无人驾驶飞机的单翼包括肋框架和泡沫，其中肋框架在模制期间被整合以获得刚度和强度。 泡沫具有用于保持电气和/或电子部件的容器。 泡沫构成冲击侧的无人驾驶飞机的外层。 机翼可以低成本和低复杂性大量生产，当在民用区域中使用时增加抗冲击性和安全性，并且是可拆卸的和一次性的，从而能够重复使用电气和/或电子部件。