发明名称 Method of fabricating a compound contoured composite beam
摘要 <p>Structural components are disclosed that are fabricated from unidirectional carbon fiber composite materials into compound contour profiles along a longitudinal axis thereof without wrinkling of composite material plies oriented in various directions relative to the longitudinal axis. Methods of stacking, sequencing, and applying the material plies to fabricate the components are also disclosed.</p>
申请公布号 EP2502734(A1) 申请公布日期 2012.09.26
申请号 EP20120172778 申请日期 2008.08.05
申请人 THE BOEING COMPANY 发明人 GLEASON, GREGORY R.;ZENKNER, GRANT C.;HAWORTH, TROY A.;KAABOUR, NAZIR M.
分类号 B29C70/34;B29C70/20;B29D99/00;B29K707/04;B29L31/00;B64C1/18 主分类号 B29C70/34
代理机构 代理人
主权项
地址