发明名称 |
SYSTEM FOR ADDITIVELY MANUFACTURING COMPOSITE PARTS |
摘要 |
A system (100) for additively manufacturing a composite part (102) is disclosed. The system (100) 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 print path (122) is stationary relative to the surface (114). The continuous flexible line (106) comprises a non-resin component (108) and a thermosetting-epoxy-resin component (110) that is partially cured. The system (100) also comprises a feed mechanism (104), configured to push the continuous flexible line (106) through the delivery guide (112). The system (100) further comprises a cooling system (234), configured to maintain the thermosetting-epoxy-resin component (110) of the continuous flexible line (106) below a threshold temperature prior to depositing the segment (120) of the continuous flexible (106) along the print path (122) via the delivery guide (112). |
申请公布号 |
EP3124212(A2) |
申请公布日期 |
2017.02.01 |
申请号 |
EP20160168651 |
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;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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