Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung

摘要

A wing (1) of composite material has an upper skin (2), a lower skin (3) and a plurality of intermediate spars (4) arranged between the upper (2) and the lower skin (3). The intermediate spars (4) extend from roots to tips of the upper (2) and the lower skins (3). The intermediate spars (4) are integrally formed with the upper (2) and the lower skins (3) or are adhesively bonded to the upper (2) and the lower skins (3). The wing (1) has a small number of parts, needs greatly reduced time for fabrication and can be fabricated at a low cost.