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 |
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代理人 |
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主权项 |
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地址 |
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