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公开(公告)号:US20100282897A1
公开(公告)日:2010-11-11
申请号:US11464973
申请日:2006-08-16
Applicant: Samuel de la Torre
Inventor: Samuel de la Torre
CPC classification number: B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/102 , B64C2201/105 , B64C2201/107 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/201 , B64C2201/203
Abstract: An aerial surveillance device is provided, comprising an image capturing device capable of being supported by an airframe structure above the ground. The airframe structure includes a body portion defining a longitudinal axis and configured to support the image-capturing device. A tail portion having control surfaces is operably engaged with the body portion along the axis. Transversely-extending wing portions are directly engaged with the body portion. Each wing portion is defined by longitudinally-opposed spars extending from a spaced-apart disposition at the body portion to a common connection distally from the body portion. The spars have a fabric extending therebetween to provide a wing surface. A support member extends along an aerodynamic center, transversely to the body portion, of each wing portion, to tension and rigidify the wing portions so as to provide a positive camber for the wing portions and to form an airfoil.
Abstract translation: 提供了一种空中监视装置,包括能够由地面上方的机身结构支撑的图像捕获装置。 机身结构包括限定纵向轴线并被配置为支撑图像捕获装置的主体部分。 具有控制表面的尾部部分沿着轴线与主体部分可操作地接合。 横向延伸的翼部直接与主体部分接合。 每个翼部分由纵向相对的翼梁限定,纵向相对的翼梁从主体部分处的间隔设置延伸到远离主体部分的公共连接。 翼梁具有在其间延伸的织物以提供机翼表面。 支撑构件沿着空气动力学中心横向于每个翼部的主体部分延伸,以使翼部被张紧和刚化,以便为翼部提供正弧形并形成翼型。