首页>
外国专利>
Aircraft wing trailing edge composite flap - has leading edge of sharp curvature and pivoted straight trailing edge
Aircraft wing trailing edge composite flap - has leading edge of sharp curvature and pivoted straight trailing edge
展开▼
机译:飞机机翼后缘复合材料襟翼-具有锋利的曲率前缘和可旋转的直后缘
展开▼
页面导航
摘要
著录项
相似文献
摘要
The profiled extendable flap consists of at least two relatively moving sections for changing the flap configuration. The flap geometry is designed so that the air flow is not separated from the flap upper face even if the flap angle of attitude is very large. The trailing edge profile (22) of the first, forward component (6) of the flap moves in a slot (23) of the rear component (7). The curvature of the composite flap, which has relatively small radii of curvature at the leading edge, becomes straighter towards the trailing edge. The rear component is pivoted with a radius (R) which is larger than the radius (r) of the leading edge curvature.
展开▼