System and method for cutting material in continuous fiber reinforced additive manufacturing

Patent metadata

Field	Value
Publication number	US-10814511-B2
Application number	US-201816215419-A
Country	US
Kind code	B2
Filing date	Dec 10, 2018
Priority date	Nov 20, 2015
Publication date	Oct 27, 2020
Grant date	Oct 27, 2020

Abstract

Methods, apparatus, and systems for cutting material used in fused deposition modeling systems are provided, which comprise a ribbon including one or more perforations. Material is passed through at least one perforation and movement of the ribbon cuts the material. A further embodiment comprises a disk including one or more blade structures, each forming at least one cavity. Material is passed through at least one cavity and a rotational movement of the disk cuts the material. A further embodiment comprises a slider-crank mechanism including a slider coupled to a set of parallel rails of a guide shaft. The slider moves along a length of the rails to cut the material. Yet another embodiment comprises one or more rotatable blade structures coupled to at least one rod. The rotation of the blade structures causes the blade structures to intersect and cut extruded material during each rotation.

First claim

What is claimed is:

1. A fiber reinforced feedstock cutting device comprising:
a feedstock pass through zone;
a controller; and
a cutting mechanism coupled to the controller, wherein a portion of the cutting mechanism defines at least a partial perimeter of the feedstock pass through zone, wherein the cutting mechanism comprises a disk including a plurality of blade structures positioned continuously along the entire perimeter of the disk, wherein each of the plurality of blade structures is shaped such that a partially enclosed cavity is defined by a curvature of each blade structure ending in a point, each partially enclosed cavity along the perimeter of the disk configured to line up with at least a partial perimeter of the feedstock pass through zone,
wherein the controller is configured to rotate the disk and then stop after rotating a predetermined distance to cut the feedstock, the predetermined distance being the distance between two consecutive partially enclosed cavities,
wherein at least one of the partially enclosed cavities comprises at least one fully enclosed perforation within a blade structure, the at least one fully enclosed perforation including a cutting edge.

2. The cutting device of claim 1 , wherein the cutting mechanism comprises:
wherein a feedstock is passed through at least one of the partially enclosed cavities and a rotational movement of the disk cuts the feedstock.

3. The cutting device of claim 1 , wherein the plurality of blade structures includes one or more sharpened edges outlining each cavity.

4. The cutting device of claim 1 , wherein the plurality of partially enclosed cavities are substantially teardrop shaped with respect to one direction.

5. The cutting device of claim 1 , wherein the fully enclosed perforation is substantially teardrop-shaped in at least one direction.

6. The cutting device of claim 1 , further comprising one or more motors coupled to the disk, wherein the one or more motors causes the disk to rotate.

7. The cutting device of claim 1 , wherein each rotational movement of the disk causes at least one partially enclosed cavity to substantially align with at least one opening of an extruder in a fused deposition modeling system, wherein the extruder includes one or more openings.

8. The cutting device of claim 1 , wherein the feedstock comprises a continuous carbon fiber or other continuous fiber reinforced composite.

9. A system of cutting fiber reinforced feedstock comprising:
a source of a feedstock;
an extruder configured to extrude the feedstock from one or more openings through a feedstock pass through zone, wherein the extruder includes one or more openings;
a controller; and
a cutting device including a cutting mechanism coupled to the controller, wherein a portion of the cutting mechanism defines at least a partial perimeter of the feedstock pass through zone, wherein the cutting mechanism comprises a disk including a plurality of blade structures along the entire perimeter of the disk, wherein each of the plurality of blade structures is shaped such that a partially enclosed cavity is defined by a curvature of each blade structure ending in a point, each partially enclosed cavity along the perimeter of the disk configured to line up with at least a partial perimeter of the feedstock pass through zone,
wherein the controller is configured to rotate the disk and then stop after rotating a predetermined distance to cut the feedstock, the predetermined distance being the distance between two consecutive partially enclosed cavities,
wherein at least one of the partially enclosed cavities comprises at least one fully enclosed perforation within a blade structure, the at least one fully enclosed perforation including a cutting edge.

10. The system of claim 9 , wherein the cutting mechanism comprises:
wherein a feedstock is passed through at least one of the partially enclosed cavities and a rotational movement of the disk cuts the feedstock.

11. The system of claim 9 , wherein the cutting mechanism includes one or more sharpened edges outlining each cavity.

12. The system of claim 9 , wherein the plurality of partially enclosed cavities is substantially teardrop shaped with respect to one direction.

13. The system of claim 9 , the fully enclosed perforation is substantially teardrop-shaped in at least one direction.

14. The system of claim 9 , further comprising one or more motors coupled to the disk, wherein the one or more motors causes the disk to rotate.

15. The system of claim 9 , wherein each rotational movement of the disk causes at least one partially enclosed cavity to substantially align with at least one opening of an extruder in a fused deposition modeling system, wherein the extruder includes one or more openings.

16. The system of claim 9 , wherein the feedstock comprises a continuous carbon fiber or other continuous fiber reinforced composite.

17. A method for cutting feedstock comprising:
passing a feedstock through a feedstock pass through zone of a fiber reinforced cutting device, the cutting device comprising:
the feedstock pass through zone:
a controller: and
a cutting mechanism coupled to the controller, wherein a portion of the cutting mechanism defines at least a partial perimeter of the feedstock pass through zone, wherein the cutting mechanism comprises a disk including a plurality of blade structures positioned continuously along the entire perimeter of the disk, wherein each of the plurality of blade structures is shaped such that a partially enclosed cavity is defined by a curvature of each blade structure ending in a point, each partially enclosed cavity along the perimeter of the disk configured to line up with at least a partial perimeter of the feedstock pass through zone,
wherein the controller is configured to rotate the disk and then stop after rotating a predetermined distance to cut the feedstock, the predetermined distance being the distance between two consecutive partially enclosed cavities,
wherein at least one of the partially enclosed cavities comprises at least one fully enclosed perforation within a blade structure, the at least one fully enclosed perforation including a cutting edge; and

cutting the feedstock with either one of the partially enclosed cavities or one of the fully enclosed perforations of the cutting mechanism.

18. The method of claim 17 , wherein the feedstock is passed through at least one of the partially enclosed cavities and a rotational movement of the disk cuts the feedstock.

19. The method of claim 18 , wherein after the feedstock is cut using a rotational movement of the disk, the disk stops moving when a downstream partially enclosed cavity lines up with the feedstock pass through zone.

20. The method of claim 17 , wherein the feedstock is cut using a substantially teardrop shaped partially enclosed cavity.

Assignees

• Boeing Co

Inventors

• Waldrop Iii John C
• Bloch Daniel D
• Hayes Michael W
• Strahm Loren J
• Szostak Peter A

Classifications

• B33Y70/00

  Materials specially adapted for additive manufacturing · CPC title

• B33Y40/00

  Auxiliary operations or equipment, e.g. for material handling · CPC title

• B29C70/30

  Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core · CPC title

• B29C48/266

  Means for allowing relative movements between the apparatus parts, e.g. for twisting the extruded article or for moving the die along a surface to be coated · CPC title

• B29C70/16

  using fibres of substantial or continuous length {(non-woven fabrics per se D04H3/00)} · CPC title