发明名称 SYSTEM FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS
摘要 A system (100) for additively manufacturing a composite part (102) comprises a delivery guide (112) and a surface (114), at least one of which is movable relative to another. The delivery guide (112) is configured to deposit at least a segment (120) of a continuous flexible line (106) along a print path (122). The print path (122) is stationary relative to the surface (114). The continuous flexible line (106) comprises a non-resin component (108) and a photopolymer-resin component (110) that is partially cured. The system 100 further comprises a feed mechanism (104) configured to push the continuous flexible line (106) through the delivery guide (112). The system 100 further comprises a source (116) of a curing energy (118). The source (116) is configured to deliver the curing energy (118) at least to a portion (124) of the segment (120) of the continuous flexible line (106) after the segment (120) of the continuous flexible line (106) exits the delivery guide (112).
申请公布号 EP3124216(A2) 申请公布日期 2017.02.01
申请号 EP20160168656 申请日期 2016.05.06
申请人 The Boeing Company 发明人 EVANS, Nick S.;TORRES, Faraón;ZIEGLER, Ryan G.;HARRISON, Samuel F.;GRIJALVA, Ciro J.;OSBORN, Hayden S.
分类号 B29C67/00;B29B15/12;B29C70/38;B29C70/52 主分类号 B29C67/00
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