IP Library Granted Patent US 10,696,039
Granted Patent B2
US 10,696,039 · App. 15/808,081 · Granted Jun 30, 2020

Multilayer fiber reinforcement design for 3D printing

Inventors: Gregory Thomas Mark (Brookline, MA); Rick Bryan Woodruff (Somerville, MA); Abraham Lawrence Parangi (Lincoln, MA); David Steven Benhaim (Cambridge, MA); Benjamin Tsu Sklaroff (Somerville, MA)
Assignee: MARKFORGED, INC.
B33Y70/00B29C64/106B29C64/386B29C70/16B33Y10/00B33Y50/02G05B19/4099G06F30/00B29C64/118B29K2025/08B29K2063/00B29K2071/00B29K2077/00B29K2079/085B29K2101/12B29K2105/08G05B2219/35134G05B2219/49007Y02P90/265
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Quick Facts
Patent No.
US 10,696,039
App. No.
15/808,081
Granted
Jun 30, 2020
Kind
B2
Abstract

A method comprising receiving a first 3D toolpath defining a fill material curved shell, receiving first 2D toolpaths defining support material flat shells, receiving a second 3D toolpath defining a long fiber composite material curved shell, the long fiber composite material including a filament having a matrix embedding fibers having a length longer than two times a diameter of the filament, actuating a fill material deposition head to trace the first 3D toolpath to deposit the fill material curved shell non-parallel to a printing substrate, actuating a support material deposition head to trace the first 2D toolpaths to deposit support material in a succession of substantially flat shells, and actuating a long fiber deposition head to trace the second 3D toolpath non-parallel to the printing substrate to deposit the long fiber composite material curved shell to enclose at least a portion of the fill material curved shell.

Claims (17)

1. A method for depositing a 3D printed part with a composite material 3D printer, comprising:

receiving a first 3D toolpath defining a fill material curved shell;

receiving first 2D toolpaths defining support material flat shells;

receiving a second 3D toolpath defining a long fiber composite material curved shell, the long fiber composite material curved shell including a filament having a matrix embedding fibers having a length longer than two times a diameter of the filament;

actuating a fill material deposition head to trace the first 3D toolpath to deposit the fill material curved shell at least in part non-parallel to a printing substrate;

actuating a support material deposition head to trace the first 2D toolpaths to deposit support material in a succession of substantially flat shells; and

actuating a long fiber deposition head to trace the second 3D toolpath at least in part non-parallel to the printing substrate to deposit the long fiber composite material curved shell to enclose at least a portion of the fill material curved shell.

2. The method according to claim 1 , further comprising:

actuating one of the support material deposition head and the fill material deposition head to deposit the printing substrate upon a build platform.

3. The method according to claim 2 , further comprising:

actuating the build platform to rotate in at least one degree of freedom additional to degrees of freedom of one of the support material deposition head and the fill material deposition head.

4. The method according to claim 2 , further comprising:

actuating the build platform to rotate through 180 degrees or more in at least one degree of freedom additional to degrees of freedom of one of the support material deposition head and the fill material deposition head to form at least one of a substantially rotationally symmetric printing substrate and a substantially rotationally symmetric fill material deposition.

5. The method according to claim 1 , further comprising:

actuating the support material deposition head to trace the first 2D toolpaths to deposit a separable or dissolvable material in a succession of shells forming a curved printing substrate.

6. The method according to claim 1 , wherein the filament of the long fiber composite material curved shell includes a prepreg filament including the matrix embedding fibers having a length of between 0.6-15 mm, and between two and ten times longer than a diameter of the prepreg filament.

7. The method according to claim 1 , wherein the printing substrate includes at least one rotationally symmetric portion.

Assignments (2)
SECURITY INTEREST Recorded Dec 4, 2024
From: MARKFORGED, INC.
To: CONTINUOUS COMPOSITES INC.
Reel/Frame 069508/0868 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 9, 2017
From: MARK, GREGORY THOMAS; WOODRUFF, RICK BRYAN; PARANGI, ABRAHAM LAWRENCE; BENHAIM, DAVID STEVEN; SKLAROFF, BENJAMIN TSU
To: MARKFORGED, INC.
Reel/Frame 044082/0437 →
Continuity (26)
Division 15174645 · Jun 6, 2016
Continuation In Part 14944093 · Nov 17, 2015
Continuation In Part 14491439 · Sep 19, 2014
Continuation In Part 14333881 · Jul 17, 2014
Continuation In Part 14297437 · Jun 5, 2014
Continuation In Part 14222318 · Mar 21, 2014
Continuation In Part 14222318
Continuation In Part 14297437
Continuation In Part 14222318
Continuation In Part 14944088 · Nov 17, 2015
Continuation In Part 14491439
Continuation In Part 14876073 · Oct 6, 2015
Continuation 14333881
Provisional Application 62172021 · Jun 5, 2015
Provisional Application 62080890 · Nov 17, 2014
Provisional Application 61907431 · Nov 22, 2013
Provisional Application 61902256 · Nov 10, 2013
Provisional Application 61883440 · Sep 27, 2013
Provisional Application 61881946 · Sep 24, 2013
Provisional Application 61880129 · Sep 19, 2013
Provisional Application 61878029 · Sep 15, 2013
Provisional Application 61847113 · Jul 17, 2013
Provisional Application 61831600 · Jun 5, 2013
Provisional Application 61815531 · Apr 24, 2013
Provisional Application 61804235 · Mar 22, 2013
Related Publication 20180072040A1 · Mar 15, 2018