Methods for additively manufacturing composite parts
AssigneeThe Boeing Company
InventorsNick S. Evans, Faraón Torres, Ryan G. Ziegler, Samuel F. Harrison, Ciro J. Grijalva, III, Hayden S. Osborn
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AssigneeThe Boeing Company
InventorsNick S. Evans, Faraón Torres, Ryan G. Ziegler, Samuel F. Harrison, Ciro J. Grijalva, III, Hayden S. Osborn
Estimating the term…
A method of additively manufacturing a composite part is disclosed. The method comprises depositing, via a delivery guide, a segment of a continuous flexible line along a print path. The continuous flexible line comprises a non-resin component and a thermosetting-epoxy-resin component that is partially cured. The method also comprises maintaining the thermosetting-epoxy-resin component of at least the continuous flexible line being advanced toward the print path via the delivery guide below a threshold temperature. The method further comprises delivering a predetermined or actively determined amount of curing energy to the segment of the continuous flexible line at a controlled rate while advancing the continuous flexible line toward the print path to at least partially cure the segment of the continuous flexible line.
A method of additively manufacturing a composite part, the method comprising:
Dependencies are inferred from the claim text.