发明名称 LAMINAR STRUCTURE WITH INTEGRITY PROTECTION ELEMENT AND METHOD OF ITS FABRICATION
摘要 FIELD: process engineering.SUBSTANCE: invention relates to structural composite, particularly, to laminar structure with integrity protection element and to method of its fabrication. It includes light composite filler arranged between laminar composite linings. Said filler consists of section connected at buts with built-in elements for protection of integrity of lining. Retaining means composed by composite straps, plates covering the filler edges and sections located between filler and every lining are arranged between filler and every lining.EFFECT: higher duration, higher strength of filler, its resistance to cracking, fracturing.10 cl, 17 dwg
申请公布号 RU2540653(C2) 申请公布日期 2015.02.10
申请号 RU20120127691 申请日期 2010.10.12
申请人 THE BOEING COMPANY 发明人 CHARL'Z R. SAFF;DZHON KH. FOGARTI;KHAOCHZHUN GU;TERRI D. RICHARDSON;KEVIN M. RETTS
分类号 B32B3/06;B32B3/12 主分类号 B32B3/06
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