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

Patent metadata

Field	Value
Publication number	US-10150262-B2
Application number	US-201514948057-A
Country	US
Kind code	B2
Filing date	Nov 20, 2015
Priority date	Nov 20, 2015
Publication date	Dec 11, 2018
Grant date	Dec 11, 2018

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 cutting mechanism, 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 ribbon including one or more perforations, wherein a feedstock is passed through at least one perforation of the one or more perforations and movement of the ribbon cuts the feedstock; and
a set of rotatable reels coupled to the ribbon, wherein rotating at least one of the reels causes movement of the ribbon in one or more directions.

2. The cutting device of claim 1 , wherein the cutting mechanism comprises one or more sharpened edges outlining each perforation.

3. The cutting device of claim 1 , wherein the one or more perforations are substantially teardrop shaped with respect to one direction.

4. The cutting device of claim 1 , wherein the one or more perforations are symmetrically shaped.

5. The cutting device of claim 1 further comprising one or more motors coupled to at least one reel, wherein the one or more motors causes at least one reel to rotate.

6. The cutting device of claim 1 further comprising one or more guides, wherein the ribbon passes through the one or more guides and remains within a predetermined space defined by the one or more guides.

7. The cutting device of claim 1 , wherein each movement of the ribbon causes at least one perforation 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; and
a cutting device including a cutting mechanism, wherein a portion of the cutting mechanism defines at least a partial perimeter of the feedstock pass through zones;
wherein the cutting mechanism comprises a ribbon including one or more perforations, wherein the feedstock is passed through at least one perforation of the ribbon; and
wherein the cutting device further comprises a set of reels coupled to the ribbon, wherein rotating the reels causes movement of the ribbon in one or more directions.

10. The system of claim 9 ,
wherein the cutting device further comprises:
one or more motors coupled to the set of reels, wherein the one or more motors causes at least one reel to rotate;
wherein movement of the ribbon cuts the feedstock; and
wherein each movement of the ribbon causes at least one perforation of the one or more perforations to substantially align with at least one opening of the one or more openings of the extruder.

Assignees

• Boeing Co

Inventors

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

Classifications

• B29C64/393

  for controlling or regulating additive manufacturing processes · CPC title

• B29C64/118

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

• B29C64/209

  Heads; Nozzles · CPC title

• B29C70/545

  Perforating, cutting or machining during or after moulding · CPC title

• B26D5/005

  Computer numerical control means · CPC title