发明名称 COMPOSITE INTEGRAL WEB STIFFENING METHOD
摘要 "I" beam or web structures (30) of laminated composite material or sheets (32, 34) are being stiffened by transverse web stiffeners (22) having a tubular configuration with flattened end portions (24). The flattened end (24) is inserted between the laminated web material or sheets (32, 34) and cured therewith to form an integral stiffened web structure (30).
申请公布号 WO8401128(A1) 申请公布日期 1984.03.29
申请号 WO1982US01248 申请日期 1982.09.15
申请人 THE BOEING COMPANY 发明人 HAMM, ROBERT, ALTON
分类号 B29C70/86;B29D24/00;B29D99/00;E04C3/29;(IPC1-7):32B31/18 主分类号 B29C70/86
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