Methods for composite filament fabrication in three dimensional printing
Various embodiments related to three dimensional printers, and reinforced filaments, and their methods of use are described. In one embodiment, a void free reinforced filament is fed into an conduit nozzle. The reinforced filament includes a core, which may be continuous or semi-continuous, and a matrix material surrounding the core. The reinforced filament is heated to a temperature greater than a melting temperature of the matrix material and less than a melting temperature of the core prior to drag the filament from the conduit nozzle.
1. A method for additively manufacturing a part, the method comprising:
receiving a core material including a plurality of reinforcing strands;
receiving a resin material;
combining the core material and the resin material to form a reinforced filament to be deposited by a nozzle;
guiding the reinforced filament to drag through the nozzle;
moving a cutter together with the nozzle;
cutting the reinforced filament with the cutter;
depositing the reinforced filament with reinforcing strands substantially aligned along the deposited reinforced filament; and
applying mechanical pressure by pressing with the nozzle to continuously compact the reinforced filament into a previously added layer of the part as the reinforced filament is fused into the part.
2. The method according to claim 1 , wherein cutting comprises shearing the reinforced filament between a feeding mechanism and a nozzle outlet.
3. The method according to claim 1 , wherein cutting comprises shearing the reinforced filament at a temperature at which the resin material is substantially unmelted.
4. The method according to claim 1 , wherein cutting comprises shearing the reinforced filament at a temperature below a glass transition temperature of the resin material.
5. The method according to claim 1 , wherein applying mechanical pressure comprises continuously ironing with a nozzle tip of the nozzle.
6. The method according to claim 1 , wherein applying mechanical pressure comprises consolidating with a rounded lip of a nozzle outlet of the nozzle.
7. The method according to claim 1 , wherein applying mechanical pressure comprises applying a compaction force with the nozzle while heating the reinforced filament at the nozzle.
8. The method according to claim 1 , further comprising positioning the reinforced filament in a receiving tube separated from the nozzle by a thermal spacer to maintain the receiving tube at a temperature at which the matrix material is unmelted.
9. The method according to claim 1 , wherein cutting comprises shearing the reinforced filament in a shearing region including the nozzle, and wherein the shearing is performed at the nozzle.
10. The method according to claim 1 , wherein cutting comprises shearing the reinforced filament in a shearing region including a shear cutter, and wherein the shearing is performed at the shear cutter.
11. A method for additively manufacturing a part, the method comprising:
receiving a core material including a plurality of reinforcing strands;
receiving a resin material;
combining the core material and the resin to form a reinforced filament to be deposited by a nozzle;
guiding the reinforced filament to drag through the nozzle;
moving a cutter together with the nozzle;
cutting the reinforced filament with the cutter;
dragging forward the reinforced filament through the nozzle by applying a force at least via the plurality of reinforcing strands;
depositing the reinforced filament with the plurality of reinforcing strands substantially aligned along the deposited reinforced filament; and
compacting the deposited reinforced filament into a previously added layer of the part.
12. The method according to claim 11 , wherein cutting comprises cutting the reinforced filament between a feeding mechanism and a nozzle outlet of the nozzle.
13. The method according to claim 11 , wherein cutting comprises shearing the reinforced filament at a temperature below one of a melting temperature of the matrix material and a glass transition temperature of the resin material.
14. The method according to claim 11 , wherein compacting comprises continuously ironing with a nozzle tip of the nozzle.
15. The method according to claim 11 , wherein compacting comprises applying a compaction force with a rounded lip of a nozzle outlet of the nozzle while heating the reinforced filament to fuse at the nozzle.
16. The method according to claim 11 , wherein cutting comprises shearing the reinforced filament in a shearing region including the nozzle, and wherein the shearing is performed at the nozzle.
17. The method according to claim 11 , wherein cutting comprises shearing the reinforced filament in a shearing region including a shear cutter, and wherein the shearing is performed at the shear cutter.
18. A method for additively manufacturing a part, the method comprising:
receiving a core material including a plurality of reinforcing strands;
receiving a resin material;
combining the core material and the resin to form a reinforced filament to be deposited by a nozzle;
guiding the reinforced filament to drag through the nozzle;
depositing the reinforced filament with reinforcing strands substantially aligned along the deposited reinforced filament;
applying pressure with the nozzle to continuously compact the reinforced filament into the part as the reinforced filament is fused into the part;
dragging forward the reinforced filament through the nozzle by applying a force at least via the plurality of reinforcing strands; and
relatively moving the nozzle and the part along at least linear axes and about at least one pivot to permit the nozzle to trace an outer contour of the part.
19. The method according to claim 18 , further comprising shearing the reinforced filament in a shearing region moved together with the nozzle.
20. The method according to claim 18 , further comprising applying pressure with a nozzle tip of the nozzle to continuously iron the reinforced filament as the reinforced filament is fused into the part.
21. The method according to claim 18 , further comprising applying a compaction force with a rounded lip of a nozzle outlet of the nozzle while heating the reinforced filament to fuse at the nozzle.
22. A method for additively manufacturing a part, the method comprising:
feeding forward a core material including a plurality of reinforcing strands;
feeding forward a resin including a thermoplastic resin;
combining the core material and the resin to form a reinforced filament to be deposited by a nozzle;
guiding the reinforced filament to drag through the nozzle;
receiving the reinforced filament at a shearing region moved together with the nozzle;
shearing the reinforced filament in the shearing region;
guiding the reinforced filament to drag through the nozzle; and
pressing with mechanical pressure with the nozzle to continuously compact the reinforced filament into a previously added layer of the part as the reinforced filament is fused into the part.
23. The method according to claim 22 , wherein shearing comprises shearing the reinforced filament between a feeding mechanism of the core material and a nozzle outlet of the nozzle.
24. The method according to claim 22 , wherein pressing with mechanical pressure comprises applying pressure with a nozzle tip of the nozzle to continuously iron the reinforced filament as the reinforced filament is fused into the part.
25. The method according to claim 22 , further comprising dragging forward the reinforced filament through the nozzle.
26. The method according to claim 22 , further comprising articulating and pivoting the nozzle with a moving mechanism including a robotic arm to relatively move the nozzle and the part in at least four degrees of freedom to deposit a reinforced filament shell forming at least outer extremes of the part.
27. The method according to claim 22 , further comprising:
building a support core of the part as a series of planar layers in three relative degrees of freedom; and
forming a shell about the support core by following a non-planar contour of the support core in at least four degrees of freedom.
28. The method according to claim 22 , wherein the shearing region includes the nozzle, and the shearing is performed at the nozzle.
29. The method according to claim 22 , wherein the shearing region includes a shear cutter, and the shearing is performed at the shear cutter.