The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 11, 2018

Filed:

Nov. 20, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

John C. Waldrop, III, St. Peters, MO (US);

Daniel D. Bloch, St. Peters, MO (US);

Michael W. Hayes, Belleville, IL (US);

Loren J. Strahm, Glen Carbon, IL (US);

Peter A. Szostak, St. Louis, MO (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B29C 47/00 (2006.01); B29C 70/30 (2006.01); B33Y 10/00 (2015.01); B33Y 30/00 (2015.01); B33Y 50/02 (2015.01); B33Y 70/00 (2015.01); B26D 1/14 (2006.01); B26D 1/25 (2006.01); B26D 3/16 (2006.01); B26D 5/00 (2006.01); B29C 69/00 (2006.01); B29C 70/16 (2006.01); B29C 70/38 (2006.01); B29C 70/54 (2006.01); B26D 1/143 (2006.01); B26D 1/46 (2006.01); B33Y 40/00 (2015.01); B29C 64/106 (2017.01); B29C 64/165 (2017.01); B29C 64/20 (2017.01); B29C 64/386 (2017.01); B22D 11/01 (2006.01); B29K 71/00 (2006.01); B29K 105/00 (2006.01); B29K 105/10 (2006.01); B29K 307/04 (2006.01); B26D 1/00 (2006.01);
U.S. Cl.
CPC ...
B29C 70/30 (2013.01); B26D 1/14 (2013.01); B26D 1/143 (2013.01); B26D 1/25 (2013.01); B26D 1/46 (2013.01); B26D 3/16 (2013.01); B26D 5/005 (2013.01); B29C 47/0066 (2013.01); B29C 64/106 (2017.08); B29C 64/165 (2017.08); B29C 64/20 (2017.08); B29C 64/386 (2017.08); B29C 69/001 (2013.01); B29C 70/16 (2013.01); B29C 70/382 (2013.01); B29C 70/545 (2013.01); B33Y 10/00 (2014.12); B33Y 30/00 (2014.12); B33Y 40/00 (2014.12); B33Y 50/02 (2014.12); B33Y 70/00 (2014.12); B22D 11/01 (2013.01); B26D 2001/006 (2013.01); B29K 2071/00 (2013.01); B29K 2105/0067 (2013.01); B29K 2105/10 (2013.01); B29K 2307/04 (2013.01);
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.


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