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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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