发明名称 SYSTEMS AND METHODS FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS
摘要 A method (300) of additively manufacturing a composite part (102) is disclosed. The method (300) comprises depositing a segment (120) of a continuous flexible line (106) along a print path (122). The continuous flexible line (106) comprises a non-resin component (108) and a thermosetting resin component (110) that is not fully cured. The method (300) further comprises, while advancing the continuous flexible line (106) toward the print path (122), delivering a predetermined or actively determined amount of curing energy (118) at least to a portion (124) of the segment (120) of the continuous flexible line (106) at a controlled rate after the segment (120) of the continuous flexible line (106) is deposited along the print path (122) to at least partially cure at least the portion (124) of the segment (120) of the continuous flexible line (106).
申请公布号 US2017028636(A1) 申请公布日期 2017.02.02
申请号 US201614995620 申请日期 2016.01.14
申请人 The Boeing Company 发明人 Evans Nick S.;Torres Faraón;Ziegler Ryan G.;Harrison Samuel F.;Grijalva, III Ciro J.;Osborn Hayden S.
分类号 B29C67/00;B29C69/00;B29C70/54;B29C70/38;B29C70/16 主分类号 B29C67/00
代理机构 代理人
主权项
地址 Chicago IL US