IP Library Granted Patent US 8,834,666
Granted Patent B2
US 8,834,666 · App. 13/961,510 · Granted Sep 16, 2014

Monolithic fabrication of three-dimensional structures

Inventors: Pratheev Sabaratnam Sreetharan (Cambridge, MA); John Peter Whitney (Pittsburgh, PA); Robert J. Wood (Cambridge, MA)
Assignee: President and Fellow of Harvard College
B32B37/0076B32B38/14B32B38/0004
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Quick Facts
Patent No.
US 8,834,666
App. No.
13/961,510
Granted
Sep 16, 2014
Kind
B2
Abstract

A multi-layer, super-planar structure can be formed from distinctly patterned layers. The layers in the structure can include at least one rigid layer and at least one flexible layer; the rigid layer includes a plurality of rigid segments, and the flexible layer can extend between the rigid segments to serve as a joint. The layers are then stacked and bonded at selected locations to form a laminate structure with inter-layer bonds, and the laminate structure is flexed at the flexible layer between rigid segments to produce an expanded three-dimensional structure, wherein the layers are joined at the selected bonding locations and separated at other locations.

Claims (34)

1. A method for fabricating a three-dimensional structure, comprising:

producing a plurality of layers with distinct patterns, wherein the layers include at least one rigid layer, at least one flexible layer, and at least one adhesive layer that bonds the rigid layer to the flexible layer, wherein the rigid layer includes a plurality of rigid segments that are substantially more rigid than the flexible layer; then

stacking the plurality of layers and bonding the plurality of layers at selected locations to form a laminate structure with inter-layer bonds; and

flexing the laminate structure at joints between the rigid segments to produce an expanded three-dimensional structure, wherein the layers are joined at the selected bonding locations and separated at other locations.

2. A method for fabricating a three-dimensional structure, comprising:

producing a plurality of layers with distinct patterns, wherein the layers include at least one rigid layer and at least one flexible layer, wherein the rigid layer includes a plurality of rigid segments that are substantially more rigid than the flexible layer; then

stacking the plurality of layers by passing dowel pins through aligned orifices in the layers and bonding the plurality of layers by a press at selected locations to form a laminate structure with inter-layer bonds; and

flexing the laminate structure at joints between the rigid segments to produce an expanded three-dimensional structure, wherein the layers are joined at the selected bonding locations and separated at other locations.

3. A method for fabricating a three-dimensional structure, comprising:

producing a plurality of layers with distinct patterns, wherein the layers include at least one rigid layer and at least one flexible layer, wherein the rigid layer includes a plurality of rigid segments that are substantially more rigid than the flexible layer; then

stacking the plurality of layers and bonding the plurality of layers at selected locations to form a laminate structure with inter-layer bonds;

flexing the laminate structure at joints between the rigid segments to produce an expanded three-dimensional structure, wherein the layers are joined at the selected bonding locations and separated at other locations; and

locking at least one of the joints in the structure after flexing to form the expanded three-dimensional structure.

4. The method of claim 3 , further comprising leaving at least one other joint free to fold after the expanded three-dimensional structure is formed.

5. The method of claim 3 , wherein the structure comprises at least one sacrificial bridge joining rigid segments, the method further comprising severing the sacrificial bridge after locking the joint to release at least one additional degree of freedom for displacement the rigid links.

6. A method for fabricating a three-dimensional structure, comprising:

producing a plurality of layers with distinct patterns, wherein the layers include at least one rigid layer and at least one flexible layer, wherein the rigid layer includes a plurality of rigid segments that are substantially more rigid than the flexible layer, wherein at least one of the layers in the laminate structure includes a pre-strained flexure spring; then

stacking the plurality of layers and bonding the plurality of layers at selected locations to form a laminate structure with inter-layer bonds; and

flexing the laminate structure at joints between the rigid segments to produce an expanded three-dimensional structure, wherein the layers are joined at the selected bonding locations and separated at other locations.

7. The method of claim 6 , wherein the laminate structure includes at least one sacrificial bridge that prevents folding of the laminate structure, the method further comprising releasing the strain in the spring by severing the sacrificial bridge, wherein the release of the strain actuates the folding to self-assemble the three-dimensional structure with one degree of freedom for assembly.

8. A method for fabricating a three-dimensional structure, comprising:

producing a plurality of layers with distinct patterns, wherein the layers include at least one rigid layer and at least one flexible layer, wherein the rigid layer includes a plurality of rigid segments that are substantially more rigid than the flexible layer; then

stacking the plurality of layers and bonding the plurality of layers at selected locations to form a laminate structure with inter-layer bonds; and

flexing the laminate structure at joints between the rigid segments to produce an expanded three-dimensional structure, wherein the layers are joined at the selected bonding locations and separated at other locations, wherein the laminate structure includes a frame and at least one structure that is flexed to produce a final product, and wherein the frame and the structure that is flexed to produce the final product are joined by at least one sacrificial bridge, the method further comprising severing the sacrificial bridge.

9. The method of claim 8 , wherein the laminate structure includes a plurality of structures that can be flexed to form a final product, each joined by at least one sacrificial bridge to the frame and released from the frame by severing the sacrificial bridge.

10. A method for fabricating a three-dimensional structure, comprising:

producing a plurality of layers with distinct patterns, wherein the layers include at least one rigid layer and at least one flexible layer, wherein the rigid layer includes a plurality of rigid segments that are substantially more rigid than the flexible layer; then

stacking the plurality of layers and bonding the plurality of layers at selected locations to form a laminate structure with inter-layer bonds;

flexing the laminate structure at joints between the rigid segments to produce an expanded three-dimensional structure, wherein the layers are joined at the selected bonding locations and separated at other locations; and

providing a scaffold, wherein the layers of the laminate structure form a plurality of inter-connected faces mounted for expansion and rotation in the scaffold, and wherein the method further comprises:

expanding the scaffold;

lifting at least one of the faces with the scaffold expansion;

rotating at least some of the faces with the scaffold expansion; and

locking the raised and rotated faces in the resulting three-dimensional structure.

Assignments (2)
CONFIRMATORY LICENSE Recorded Aug 14, 2014
From: HARVARD UNIVERSITY
To: NATIONAL SCIENCE FOUNDATION
Reel/Frame 033541/0668 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 8, 2014
From: SREETHARAN, PRATHEEV S.; WHITNEY, JOHN PETER; WOOD, ROBERT J.
To: PRESIDENT AND FELLOWS OF HARVARD COLLEGE
Reel/Frame 031913/0925 →
Continuity (6)
Continuation In Part 13519901
Continuation In Part 13961510
Continuation PCTUS2012024682 · Feb 10, 2012
Provisional Application 61561144 · Nov 17, 2011
Provisional Application 61467765 · Mar 25, 2011
Related Publication 20140202628A1 · Jul 24, 2014