Invention Grant
US08376278B2 Cover trailing edge profile 有权
盖后缘轮廓

Cover trailing edge profile
Abstract:
An aircraft wing assembly, comprising a front spar, a rear spar, and upper and lower wing covers extending between the front and rear spars, wherein the upper and/or lower wing cover overhangs the rear spar and has a non-linear trailing edge profile forming an array of tabs and cut-outs. Also, a method of assembling the aircraft wing.
Public/Granted literature
Information query
Patent Agency Ranking
0/0