| 摘要 |
The present invention relates to a tip fairing (200) of a horizontal airfoil of an aircraft, comprising stiffening elements (202) and a skin (203) covering the stiffening elements (202), the stiffening elements (202) comprising a central web and two flanges located at the tips of the web, contact between the skin (203) and the stiffening elements (202) being made through the flanges of the stiffening elements (202), characterized in that it is manufactured from a composite material, it is manufactured from a single part, and the planes defining the webs of any pair of stiffening elements (202) taken in twos form an angle less than 30°. |
