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 代理人
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