System zur Additiven Fertigung von Verbundstoffteilen

Details

Veröffentlichungs-Nr.

EP3124215

Aktenzeichen

EP16168654

Anmeldetag

6. Mai 2016

Veröffentlichung

29. April 2020

Erteilung

29. April 2020

Rechtsraum

EP

IPC

B29C67/00B29C70/38B29B15/12B29C70/52B29C64/106B29C64/165B29C64/386

Abstract

A system (100) for additively manufacturing a composite part (102) comprises a delivery assembly (266), a feed mechanism (104), and a source (116) of curing energy (118). The delivery assembly (266) comprises a delivery guide (112) movable relative to a surface (114) and is configured to deposit a continuous flexible line (106) along a print path (122). The delivery assembly (266) further comprises a first inlet (170), configured to receive a non-resin component (108), and a second inlet (250), configured to receive a photopolymer resin (252). The delivery assembly (266) applies the photopolymer resin (252) to the non-resin component (108). The feed mechanism (104) pushes the continuous flexible line (106) out of the delivery guide (112). The source (116) of the curing energy (118) delivers the curing energy (118) to a portion (124) of the continuous flexible line (106) after it exits the delivery guide (112).

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete