Invention Application
US20110001010A1 ARRANGEMENT OF TWO FUSELAGE SECTIONS OF AN AIRCRAFT AND A CONNECTING STRUCTURE FOR CONNECTING FUSELAGE SKINS 有权
飞机的两个熔接部分的安装和连接熔融皮肤的连接结构

ARRANGEMENT OF TWO FUSELAGE SECTIONS OF AN AIRCRAFT AND A CONNECTING STRUCTURE FOR CONNECTING FUSELAGE SKINS
Abstract:
A coupling element for connecting stringers in the process of joining two fuselage sections by means of at least one transverse splicing plate, wherein in each case the fuselage sections on the inside comprise a multitude of stringers arranged on fuselage skins, as well as annular frame elements, wherein the coupling element comprises a base flange and a frame element flange, and by way of the coupling element in each case a connection between the opposing stringers, the annular frame element and the fuselage skins or the transverse splicing plate takes place so that the coupling element beyond a connection of the stringer base also supports the connection of stringers on the flank side.
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