发明名称 FABRIC JACKETED UNIDIRECTIONAL NOODLE
摘要 A composite, radius filler noodle for a co-cured spar or stringer used in aircraft construction has a unidirectional composite core and pluralities of pre-preg fabric strips stacked in layers surrounding the core.
申请公布号 US2016023431(A1) 申请公布日期 2016.01.28
申请号 US201414340982 申请日期 2014.07.25
申请人 The Boeing Company 发明人 Zarfos Joshua;Andryukov Vladislav;Campbell Darrell
分类号 B32B5/26;B32B37/00;B32B5/12;B32B37/18 主分类号 B32B5/26
代理机构 代理人
主权项 1. A composite, radius filler noodle comprising: a core having a triangular cross-section configuration and first, second and third surfaces that extend along a length of the core; a plurality of pre-preg fabric first strips stacked on the core first surface, the plurality of first strips having lengths that extend completely along the core length; a plurality of pre-preg fabric second strips stacked on the core second surface, the plurality of second strips having lengths that extend completely along the core length; and, a plurality of pre-preg fabric third strips stacked on the core third surface, the plurality of third strips having lengths that extend completely along the core length.
地址 Chicago IL US