Extrusion apparatus and method

Patent metadata

Field	Value
Publication number	US-9550319-B2
Application number	US-201414174892-A
Country	US
Kind code	B2
Filing date	Feb 7, 2014
Priority date	Feb 7, 2014
Publication date	Jan 24, 2017
Grant date	Jan 24, 2017

Abstract

One aspect of the disclosure relates to an apparatus including an extrusion nozzle. The nozzle includes an inlet end, an outlet end opposite the inlet end and an axis extending between the inlet end and the outlet end. The extrusion nozzle is configured to rotate about the axis. The extrusion nozzle also includes a rotary drive engagement portion between the inlet end and the outlet end. The extrusion nozzle further includes a cavity including an inlet opening at the inlet end and an outlet opening at the outlet end. The inlet opening has a different configuration than the outlet opening.

First claim

What is claimed is:

1. An apparatus comprising:
an extrusion nozzle including
an inlet end;
an outlet end opposite the inlet end;
an external surface extending between the inlet end and the outlet end;
an axis extending between the inlet end and the outlet end, wherein the extrusion nozzle is configured to rotate about the axis;
a rotary drive engagement portion between the inlet end and the outlet end; and
a cavity including an inlet opening at the inlet end and an outlet opening at the outlet end, wherein the inlet opening has a different configuration than the outlet opening and a wall thickness of the extrusion nozzle between the external surface of the extrusion nozzle and a surface of the cavity varies in a plane containing the axis that extends between the inlet end and the outlet end;
wherein the cavity has a path that is non-linear.

2. The apparatus of claim 1 , wherein the cavity includes a taper.

3. The apparatus of claim 2 , wherein the cavity is narrower near the outlet end than near the inlet end.

4. The apparatus of claim 1 , wherein the apparatus further includes at least one heating element thermally coupled with the extrusion nozzle.

5. The apparatus of claim 1 , wherein the path of the cavity is a tortuous path.

6. The apparatus of claim 5 , wherein the tortuous path is a spiral path.

7. The apparatus of claim 6 , wherein the spiral path is positioned around at least one heating element disposed at least partially within the extrusion nozzle.

8. The apparatus of claim 1 , wherein the outlet opening has a non-circular shape.

9. The apparatus of claim 1 , wherein the outlet opening is a non-planar opening.

10. The apparatus of claim. 1 , wherein the outlet opening is formed at least partly on a side portion of the extrusion nozzle.

11. The apparatus of claim 1 , wherein the rotary drive engagement portion comprises one of a pulley, a sprocket or a gear.

12. The apparatus of claim 1 , wherein a length of a path of the cavity is greater than a length of the extrusion nozzle.

13. The apparatus of claim 1 , wherein the extrusion nozzle is monolithic.

14. The apparatus of claim 1 , wherein the apparatus is a three-dimensional printing system comprising:
a build platform having a build plane; and
a print unit including the extrusion nozzle, wherein the print unit and the build platform are movable relative to each other.

15. The apparatus of claim 14 , wherein the print unit further includes a rotatory drive configured to engage the rotary drive engagement portion and to rotate the extrusion nozzle about the axis.

16. The apparatus of claim 15 , wherein the rotary drive is configured to directly drive the rotary drive engagement portion.

17. The apparatus of claim 14 , wherein the print unit includes a feed unit configured to provide material into the inlet opening.

18. The apparatus of claim 14 , wherein the print unit includes a first linear drive: and a second linear drive configured to move the extrusion nozzle in the build plane.

19. The apparatus of claim 18 , wherein the three dimensional printing system further includes a third linear drive configured to move the build platform in a direction perpendicular to the build plane.

Assignees

• Boeing Co

Inventors

• Larsen Ty A
• Murrish Richard E

Classifications

• B29C64/118

  using filamentary material being melted, e.g. fused deposition modelling [FDM] · CPC title

• B29C64/209

  Heads; Nozzles · CPC title

• B33Y10/00

  Processes of additive manufacturing · CPC title

• B29C2948/9258

  Velocity · CPC title

• B29C2948/92904

  Die; Nozzle zone · CPC title