发明名称 STRUCTURE FOR COMBINING LEADING EDGE OF WING FOR PLANE
摘要 PURPOSE: A combining structure of a leading edge is provided to offer the flat surface and to smoothen a load flow by equipping with an aluminum wedge portion having a long length and a short width neck. CONSTITUTION: A leading edge contains skins(120), a honeycomb core and a wedge portion(110). The honeycomb core is layered to have the section to be extended downward by sticking inside the skins. The wedge portion is arranged on the upper part of the honeycomb core. The wedge portion has the length to be corresponding to a leading edge(100) by sticking to the inner surface of the skins. Thereby, the number of assembling components in the leading edge is reduced, and the continuous load path is obtained.
申请公布号 KR20030037149(A) 申请公布日期 2003.05.12
申请号 KR20010068256 申请日期 2001.11.02
申请人 KOREA AEROSPACE INDUSTRIES, LTD. 发明人 LEE, SEONG UN
分类号 B64C5/06;(IPC1-7):B64C5/06 主分类号 B64C5/06
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