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 in successive layers, the method comprising:
supplying a reinforced filament having a matrix material impregnating a plurality of reinforcing strands aligned along the reinforced filament;
receiving the reinforced filament at a shearing region moved together with a nozzle;
shearing the reinforced filament at the shearing region;
guiding the reinforced filament to drag through the nozzle;
heating the reinforced filament at the nozzle as the reinforced filament is displaced out of the nozzle;
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 shearing comprises shearing the reinforced filament between a feeding mechanism and a nozzle outlet.
3. The method according to claim 1 , wherein shearing comprises shearing the reinforced filament at a temperature below a melting temperature of the matrix material.
4. The method according to claim 1 , wherein shearing comprises shearing the reinforced filament at a temperature below a glass transition temperature of the matrix 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 to fuse at the nozzle.
8. The method according to claim 1 , further comprising:
positioning the reinforced filament in a receiving tube separated from the heated nozzle by a thermal spacer to maintain the receiving tube at a temperature at which the matrix material is unmelted.
9. A method for additively manufacturing a part in successive layers, the method comprising:
supplying a reinforced filament having a matrix material impregnating a plurality of reinforcing strands aligned along the reinforced filament;
feeding forward the reinforced filament into a nozzle;
receiving the fed forward 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;
heating the reinforced filament at a heated zone as the reinforced filament is displaced out of the nozzle;
dragging forward the reinforced filament through the nozzle by applying a force at least via the plurality of reinforcing strands; and
pressing with mechanical pressure to compact the reinforced filament into a previously added layer of the part.
10. The method according to claim 9 , further comprising shearing the reinforced filament between a feeding mechanism and a nozzle outlet of the nozzle.
11. The method according to claim 10 , wherein shearing 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 matrix material.
12. The method according to claim 9 , wherein pressing with mechanical pressure comprises continuously ironing with a nozzle tip of the nozzle.
13. The method according to claim 9 , wherein pressing with mechanical pressure 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.
14. A method for manufacturing a part, the method comprising:
supplying a reinforced filament having a matrix material impregnating a plurality of reinforcing strands aligned along the reinforced filament;
feeding forward the reinforced filament into a nozzle;
heating the reinforced filament as the reinforced filament is displaced out of the nozzle;
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 in at least four degrees of freedom, including at least one pivot, to permit the nozzle to trace an outer contour of the part.
15. The method according to claim 14 , further comprising shearing the reinforced filament in a shearing region moved together with the nozzle.
16. The method according to claim 14 , 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.
17. The method according to claim 14 , 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.
18. A method for additively manufacturing a part in successive layers, the method comprising:
supplying a reinforced filament having a matrix material impregnating a plurality of reinforcing strands aligned along the reinforced filament;
feeding forward the reinforced filament into a nozzle;
receiving the fed forward 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 a nozzle;
heating the reinforced filament at a heated zone as the reinforced filament is displaced out of the nozzle;
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.
19. The method according to claim 18 , wherein shearing comprises shearing the reinforced filament between a feeding mechanism and a nozzle outlet of the nozzle.
20. The method according to claim 18 , 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.
21. The method according to claim 18 , further comprising dragging forward the reinforced filament through the nozzle by applying a force greater than a force threshold of the feeding forward at least via the plurality of reinforcing strands.
22. The method according to claim 1 , wherein the shearing region includes the nozzle, and the shearing is performed at the nozzle.
23. The method according to claim 1 , wherein the shearing region includes a shear cutter, and the shearing is performed at the shear cutter.
24. The method according to claim 9 , wherein the shearing region includes the nozzle, and the shearing is performed at the nozzle.
25. The method according to claim 9 , wherein the shearing region includes a shear cutter, and the shearing is performed at the shear cutter.
26. The method according to claim 14 , 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 the outer extremes of the part.
27. The method according to claim 14 , further comprising building a support core of the part as a series of planar layers in three relative degrees of freedom, then forming a shell about the support core by following a non-planar contour of the support core at least four degrees of freedom.
28. The method according to claim 18 , wherein the shearing region includes the nozzle, and the shearing is performed at the nozzle.
29. The method according to claim 18 , wherein the shearing region includes a shear cutter, and the shearing is performed at the shear cutter.