COMPOSITE MATERIAL REINFORCED STEREOLITHOGRAPHY METHODS AND SYSTEMS
20230241835 · 2023-08-03
Assignee
Inventors
- Jackson Hamilton (Somerville, MA, US)
- Cole Durbin (Cambridge, MA, US)
- Maxim Lobovsky (Cambridge, MA, US)
Cpc classification
B29C64/236
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B29C64/135
PERFORMING OPERATIONS; TRANSPORTING
B33Y30/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y40/00
PERFORMING OPERATIONS; TRANSPORTING
B29C70/30
PERFORMING OPERATIONS; TRANSPORTING
B29C64/223
PERFORMING OPERATIONS; TRANSPORTING
B29C64/307
PERFORMING OPERATIONS; TRANSPORTING
B29C64/20
PERFORMING OPERATIONS; TRANSPORTING
B29C64/124
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C64/124
PERFORMING OPERATIONS; TRANSPORTING
B29C64/307
PERFORMING OPERATIONS; TRANSPORTING
B29C64/20
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y30/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for producing a three-dimensional object on an additive fabrication device includes placing a first composite material patch on a bottom of a vessel of the additive fabrication device. The method also includes moving a build plate of the additive fabrication device whereby at least one of the build platform or a layer of at least partially cured resin on the build plate touches the first composite material patch. The method further includes irradiating resin contained inside the vessel with an energy source to at least partially cure a layer of resin integrated with the first composite material patch.
Claims
1. A method for producing a three-dimensional object on an additive fabrication device, comprising: placing a first composite material patch on a bottom of a vessel of the additive fabrication device; moving a build plate of the additive fabrication device whereby at least one of the build plate or a layer of at least partially cured resin on the build plate touches the first composite material patch; and irradiating resin contained inside the vessel with an energy source to at least partially cure a layer of resin integrated with the first composite material patch.
2. The method of claim 1, wherein the first composite material patch is cut into a shape corresponding to a respective cross-sectional area of the three-dimensional object and is automatically placed on the bottom of the vessel via a transfer device.
3. The method of claim 2, further including: moving the build plate with the at least partially cured layer of resin integrated with the composite material patch away from the bottom of the vessel; and placing a second composite material patch onto the bottom of the vessel.
4. The method of claim 3, wherein the second composite material patch is at least one of a same shape and size as that of the first composite material patch.
5. The method of claim 3, wherein the second composite material patch is at least one of a different shape or size from that of the first composite material patch.
6. An additive fabrication device configured to manufacture a three-dimensional object, comprising: a vessel with a transparent bottom configured to hold a photocurable composition; a build platform positioned above the vessel and configured to translate with respect to the vessel; an energy source configured to emit an energy through the transparent bottom of the vessel; a composite material dispenser; a sheet cutting device; a transfer device; and a controller communicably coupled to the build platform, the composite material dispenser, the energy source, the sheet cutting device, and the transfer device, wherein the controller executes instructions which causes: the energy source to irradiate the photocurable composition in the vessel to form a first at-least-partially-cured layer of the photocurable composition on the build platform or on a previously-formed at-least-partially-cured layer of the photocurable composition; the composite material dispenser to supply portions of a composite material sheet; the cutting device to cut one or more portions of the composite material sheet into one or more patches each with geometry corresponding to a respective cross-section of the three-dimensional object, the transfer device to transfer a first patch of the one or more patches onto the transparent bottom of the vessel, and the energy source to irradiate the photocurable composition, resulting in a second at-least-partially-cured layer of the photocurable composition integrated with the first patch and the first at-least-partially-cured layer of the photocurable composition.
7. The additive fabrication device of claim 6, wherein the cutting device includes at least one of a roller cutter, a drag knife, a vibrating/ultrasonic knife, or a laser cutter.
8. The additive fabrication device of claim 6, wherein the composite material sheet includes a fiberglass reinforced composite.
9. The additive fabrication device of claim 6, wherein the photocurable composition includes at least one of a dual-curing component or a dark-curing polymer and the composite material sheet includes material not transmissive to the energy source.
10. The additive fabrication device of claim 6, wherein the composite material sheet includes carbon fiber.
11. The additive fabrication device of claim 6, wherein the one or more patches are nested on the composite material sheet thereby minimizing the required sheet area.
12. The additive fabrication device of claim 6, wherein the transfer device includes a vacuum-assisted gripper for picking up the first patches from the composite material sheet and placing the first patch onto the first at-least-partially-cured layer of the photocurable composition.
13. The additive fabrication device of claim 6, wherein the transfer device includes an electrostatics-assisted gripper for picking up the first patch from the composite material sheet and placing the first patch onto the first at-least-partially-cured layer of the photocurable composition.
14. The additive fabrication device of claim 6, wherein the transfer device includes a gantry system for translating the build platform and causing the build platform to transfer the first patch onto the first at-least-partially-cured layer of the photocurable composition.
15. The additive fabrication device of claim 6, wherein each of the one or more patches includes a fixed inward offset from a perimeter of the corresponding respective cross-section of the three-dimensional object.
16. The additive fabrication device of claim 6, wherein each of the one or more patches includes a fixed outward offset from a perimeter of the corresponding respective cross-section of the three-dimensional object.
17. The additive fabrication device of claim 6, wherein the one or more patches are impregnated with binder material or supported by peel-away solid sheets to prevent fraying.
18. An additive fabrication device configured to manufacture a three-dimensional object, comprising: a vessel with a transparent bottom; a build platform positioned above the vessel and configured to translate with respect to the vessel; an energy source configured to emit an energy through the transparent bottom of the vessel; a composite material dispenser; a sheet cutting device; a transfer device; and a controller communicably coupled to the build platform, the dispenser, the energy source, the cutting device, and the transfer device, wherein the controller executes instructions which causes: the composite material dispenser to supply portions of a composite material sheet, the cutting device to cut the portions of the composite material sheet into one or more patches, the composite material dispenser to wet a first patch of the one or more patches with a photocurable composition, the transfer device to transfer the wet first patch onto the transparent bottom of the vessel, and the energy source to irradiate the wet first patch, resulting in the first wet patch suspended in a first at-least-partially-cured layer of the photocurable composition on the build platform.
Description
BRIEF DESCRIPTION OF DRAWINGS
[0014] Various aspects and examples will be described with reference to the following figures. It should be appreciated that the figures are not necessarily drawn to scale. In the drawings, each identical or nearly identical component that is illustrated in various figures is represented by a like numeral. For purposes of clarity, not every component may be labeled in every drawing.
[0015] The technology described below relates to reinforcing 3D printed objects with composite materials such as fiberglass in stereolithography (SLA). The system and method involve adding composite material patches to print layers and selectively curing through them. The composite material patches may have been previously cut to correspond to respective cross-sections of the object to be produced, and may be automatically transferred to desired position on the bottom of the resin vessel of the stereolithography device.
[0016]
[0017]
[0018]
[0019]
[0020]
[0021]
DETAILED DESCRIPTION
[0022]
[0023] A build plate or build platform 105 may be positioned along a vertical axis 103 (oriented along the z-axis direction as shown in
[0024] In the example of
[0025] Following the curing of a layer of material, the build platform 105 may be moved along the vertical axis of motion 103 in order to reposition the build platform 105 for the formation of a new layer and/or to impose separation forces upon any bond with the bottom 121 of basin 120. In addition, the basin 120 is mounted onto the support base 101 such that the stereolithographic printer 100 may move the basin 120 along horizontal axis of motion 110, the motion thereby advantageously introducing additional separation forces in at least some cases. The basin 120 may include a wiper 126 capable of motion along the horizontal axis of motion 110 and may be removably or otherwise mounted onto the support base 101 at 109.
[0026]
[0027] In some examples, the composite material patch 204 may be cut by a roller cutter, a drag knife, a vibrating/ultrasonic knife, or a laser cutter from a large composite material sheet such as a fiberglass sheet. In some examples, cutting a composite material sheet can cause the sheet (especially along the cut edge) to fray. To mitigate sheet fraying, the patches 204 may be previously impregnated with binder material or supported by peel-away solid sheets.
[0028] In some examples, the patch of composite material 204 is automatically placed at the desired location on the bottom of the resin tank 206 by a gantry system with a gripper. For example, the composite material patch 204 may be placed by a gantry system with a vacuum-assisted gripper that is configured to pick up the pre-cut composite material patch 204. In another example, the gripper is an electrostatics-assisted gripper for picking up the pre-cut patches.
[0029] In some examples, multiple patches are pre-cut from the composite material sheet and nested on the sheet to minimize the required sheet area. For example, each patch 204 would correspond to a respective cross-sectional area of the print to be produced.
[0030] In some examples, the composite material patch 204 is made of fiberglass due to fiberglass' transmissivity to UV and near-UV light, as well as its tendency to bond with resin R. Alternatively, the composite material patch 204 may be made of carbon fiber or other materials that are not significantly transmissive to UV or near-UV light, and the resin R may include dual-curing component or a dark-curing polymer.
[0031] In
[0032] In
[0033] Although only one composite material patch 204 is shown in
[0034]
[0035]
[0036] A transfer device that includes two rollers 402 holding composite material sheet 404 is placed at each end of the system 400, with the composite material sheet 404 being moved freely from one roller 402 to the other. An automated cutting device 410 such as a laser cutter is configured to cut patches from the sheet 404, which is then transferred to the bottom of the resin tank 406, below the build platform 405. Two smaller rollers 402a are placed inside the resin tank 406 to hold the composite material sheet 404 flat against the bottom of the resin tank 406.
[0037] In
[0038] In
[0039]
[0040] Alternatively, the SLA machine may cure through the composite material sheet 404 without cutting away a blank area. For example, the energy source may cure resin with a higher power and the build platform 405 will lower to a new position that causes one layer thickness between the top surface of the composite material sheet 404 and the bottom surface of the partially produced print.
[0041]
[0042] A number of implementations have been described. Nevertheless, it will be understood that various modifications may be made without departing from the spirit and scope of the disclosure. Accordingly, other implementations are within the scope of the following claims.