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), movable relative to a surface (114). 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 continuous flexible line (106) comprises a non-resin component (108) and a thermosetting-resin component (110). The thermosetting-resin component (110) comprises a first part (253) and a second part (255). The system (100) further comprises a first resin-part applicator (236), configured to apply a first quantity of the first part (253) to the non-resin component (108), and a second resin-part applicator (237), configured to apply a second quantity of the second part (255) to the first quantity of the first part (253) of a thermosetting resin (252), applied to the non-resin component (108). The system (100) also comprises a feed mechanism (104), configured to pull the non-resin component (108) through the first resin-part applicator (236) and the second resin-part applicator (237), and to push the continuous flexible line (106) out of the delivery guide (112).
申请公布号 EP3124213(A1) 申请公布日期 2017.02.01
申请号 EP20160168652 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 主分类号 B29C67/00
代理机构 代理人
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