Polymer composites for fused filament fabrication and methods of making the same
10744695 ยท 2020-08-18
Assignee
Inventors
- Rebecca L. Erikson (Richland, WA, US)
- Josef F. Christ (Pasco, WA, US)
- Zachary C. Kennedy (Richland, WA, US)
- Kent A. Evans (San Jose, CA, US)
- Christopher A. Barrett (Richland, WA, US)
- Satish K. Nune (Richland, WA, US)
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
C08L67/04
CHEMISTRY; METALLURGY
B29C64/118
PERFORMING OPERATIONS; TRANSPORTING
D01F6/625
TEXTILES; PAPER
C08J9/26
CHEMISTRY; METALLURGY
C08L67/04
CHEMISTRY; METALLURGY
B29C48/16
PERFORMING OPERATIONS; TRANSPORTING
B33Y70/10
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/046
PERFORMING OPERATIONS; TRANSPORTING
International classification
B33Y70/00
PERFORMING OPERATIONS; TRANSPORTING
C08J9/26
CHEMISTRY; METALLURGY
C08J9/00
CHEMISTRY; METALLURGY
Abstract
Disclosed are compositions of a fused filament fabrication (FFF) composite filament having embedded functional materials in a thermoplastic matrix. Methods of making the composite filaments are also disclosed. In one example, a FFF composite filament incorporates a MOF, in an amount greater than 10% by mass, dispersed in a matrix polymer. One example of a method of synthesizing FFF composite filaments involves mixing a suspension that has a MOF with a matrix polymer solution to yield a polymer-MOF mixture. The mixture is cast and dried into a solid composite material, which is formed a FFF composite filament having the MOF in an amount greater than 10% by mass.
Claims
1. A method of synthesizing a FFF composite filament, the method comprising: mixing a sacrificial polymer solution in a sacrificial polymer solvent in a suspension that comprises a MOF with a matrix polymer solution that comprises a matrix polymer in a matrix polymer solvent to yield a polymer-MOF mixture and wherein the sacrificial polymer solution and the matrix polymer solution are at least partially miscible with one another; casting and drying the polymer-MOF mixture into a solid composite material; forming the solid composite material into a FFF composite filament comprising the MOF in an amount greater than 10% by mass and selectively removing the sacrificial polymer from the FFF composite filament or from an item printed from the FFF composite filament.
2. The method of claim 1, wherein said removing comprises dissolving the sacrificial polymer with a sacrificial polymer removal solvent in which the solubility of the sacrificial polymer is greater than the solubility of the matrix polymer.
3. The method of claim 1, wherein the sacrificial polymer comprises a fluoropolymer.
4. The method of claim 1, wherein the solid composite material comprises greater than 10% sacrificial polymer by mass.
5. The method of claim 1, further comprising: replacing at least a portion of residual solvent that remains in pores of the FFF composite filament, or an item printed from the FFF composite filament, with an exchange solvent having a boiling temperature that is less than that of the residual solvent; and evaporating the exchange solvent from the pores and activating chemical functionality of the MOF.
6. The method of claim 5, wherein after said evaporating, the FFF composite filament, or an item printed from the FFF composite filament, has a surface area greater than or equal to 250 m.sup.2/g.
7. The method of claim 1, wherein the FFF composite filament comprises the MOF in an amount greater than 25% by mass.
8. The method of claim 1, wherein the FFF composite filament comprises the matrix polymer in an amount greater than 15% by mass.
9. The method of claim 1, wherein the matrix polymer comprises polylactic acid, thermoplastic polyurethane, acrylonitrile butadiene styrene, nylon 12, nylon 66, polyvinylidene difluoride, polycarbonate, or a combination thereof.
10. The method of claim 1, wherein the MOF comprises ZIF-08, UiO-66, MIL-101(Cr), FeBTC, or a combination thereof.
11. The method of claim 1, wherein the FFF composite filament has a surface area greater than or equal to 2.5 m.sup.2/g.
12. The method of claim 1, wherein said forming comprises providing the solid composite material to an extruder and pressing the material through a die to yield the FFF composite filament.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
(16) Material formulation for additive manufacturing (AM) can be a critical component to the progression of the industry as it moves from novelty to a mainstream, disruptive technology. The problems associated with handling MOFs and fabricating them into useful forms that retain native MOF functionality are solved by a FFF composite filament having greater than 10% MOF by mass in a matrix polymer. The inventors have determined unexpectedly that an insufficient MOF loading in the composite filament results in poor chemical functionality. In other words, sufficiently high loadings are required to attain the functionality of the native MOF.
(17) Disclosed herein are polymer-MOF composite materials, and methods of making the same, that are compatible with 3D printing technologies and that can retain the chemical functionality of the native MOF. The compositions and methods of making enable advanced manufacturing of MOF-based articles including, but not limited to, printable chemical sensors, functional textiles, and collection devices having complex geometry. The inventors have determined that the instant FFF composite filaments, and items printed therefrom, not only retain native MOF characteristics, such as high surface area and chemical reactivity, but also exhibit high mechanical strength and a simplification of use. FFF as a 3D printing technique differs from direct ink writing, and the composite filaments described herein differ from MOF-based slurries used in direct ink writing. 3D printing of the FFF, polymer-MOF, composite filament avoids the need for forms of invasive densification often associated with traditional MOF-related manufacturing techniques. MOF pellets, beads and membranes typically suffer from a sharp loss in total surface area, with some MOFs being completely destroyed in the process. The shapes available with conventional fabrication processes are limited and can be very fragile. For these and other reasons, MOFs are difficult to integrate with important applications such as wearable technologies.
(18) Referring to
(19) As illustrated in
(20) Referring to
(21) The following explanations of terms and abbreviations are provided to better describe the present disclosure and to guide those of ordinary skill in the art in the practice of the present disclosure. As used herein, comprising means including and the singular forms a or an or the include plural references unless the context clearly dictates otherwise. The term or refers to a single element of stated alternative elements or a combination of two or more elements, unless the context clearly indicates otherwise.
(22) Unless explained otherwise, all technical and scientific terms used herein have the same meaning as commonly understood to one of ordinary skill in the art to which this disclosure belongs. Although methods and materials similar or equivalent to those described herein can be used in the practice or testing of the present disclosure, suitable methods and materials are described below. The materials, methods, and examples are illustrative only and not intended to be limiting. Other features of the disclosure are apparent from the following detailed description and the claims.
(23) Unless otherwise indicated, all numbers expressing quantities of components, molecular weights, percentages, temperatures, times, and so forth, as used in the specification or claims are to be understood as being modified by the term about. Accordingly, unless otherwise implicitly or explicitly indicated, or unless the context is properly understood by a person of ordinary skill in the art to have a more definitive construction, the numerical parameters set forth are approximations that may depend on the desired properties sought and/or limits of detection under standard test conditions/methods as known to those of ordinary skill in the art. When directly and explicitly distinguishing embodiments from discussed prior art, the embodiment numbers are not approximates unless the word about is recited.
EXAMPLES AND COMPARISONS
(24) To further illustrate certain embodiments of the disclosed FFF composite filaments and methods of making the same, and to provide various comparative analyses and data, below are some Examples with comparison test data.
(25) Generally, the examples illustrate the uniform incorporation of MOFs into three dimensional objects via an additive manufacturing process and methods to enable retention of valuable framework structural and functional characteristics while also imparting robust mechanical properties from the polymeric foundation. Selection of polymer matrices with a solubility profile compatible with solutions of suspended MOFs can enable sufficient preservation of the parent polymer's thermoplastic properties for processing, spooling into filament, and printing with very high particulate loadings. Characterization of rigid and flexible classes of printed materials revealed vastly different gas adsorption properties, where a hierarchical porous internal network was observed in the former case and nearly complete pore occlusion in the latter. One remedy to this undesirable pore blockage is described involving a technique to template the MOF crystals with a sacrificial polymer additive miscible with the matrix polymer, followed by printing, then selective removal of the sacrificial polymer by chemical treatment. Access to the MOF microporous structure is restored and, consequently, the item exhibits high surface area. In each material class, the printed objects interacted with small molecule and gaseous guests in a typical fashion to free powdered (i.e., native) MOF.
(26) 3D printing and characterization of rigid polymer-MOF composites with hierarchical porosity
(27) ZIF-8 composites were processed into FFF composite filaments with PLA base polymer matrices. A PLA stock solution (0.05 g mL.sup.1) was prepared by dissolving PLA pellets (7.5 g) in CHCl.sub.3 (150 mL) while stirring at room temperature. A typical composite with a total mass of 2 g and a ZIF-8 loading of 40% by mass was achieved first by dispersing ZIF-8 (800 mg) in ethyl acetate (10 mL) by bath sonication for 15 min. The PLA stock solution (24 mL) was then added to the MOF solution, briefly stirred (1 min), and the mixture was sonicated by ultrasonic horn for 20 min. The resulting mixture was cast onto a Teflon dish, most of the solvents removed by placing the dish on a hot plate at 75 C., then the composite was fully dried at 75 C. for 16 h in a vacuum oven under low vacuum to obtain a thick film.
(28) In one instance, PLA/ZIF-8 composites were obtained by suspending ZIF-8 in ethyl acetate (EtOAc) by sonication, followed by addition of a dilute PLA solution (0.05 g/mL in CHCl.sub.3) to the MOF suspension. After additional sonication, the mixtures were cast and dried. The resulting thick films were cut, fed into a heated (185 C.) barrel of an extruder, and pressed through a die to yield composite filaments with diameters of approximately 1750 m. Filaments were prepared with up to 40% ZIF-8 loading by mass with no flaking or powdering of the MOF upon visual inspection suggesting good adhesion to the PLA matrix. By comparison, the direct addition of ZIF-8 powder into polymer solutions resulted in large aggregation of ZIF-8 and clumping within the polymer matrix regardless of subsequent extended sonication treatments. Structural analysis of the (60:40)-PLA/ZIF-8 filament feedstock (1750 m diameter) by powder X-ray diffraction (PXRD) confirmed that the ZIF-8 framework retained a very high crystallinity after the processing steps (
(29) The PLA filaments were then used to FDM-print materials, in the form of 400 m cylindrical strands as a standardized geometry, for further characterization of the physical characteristics of the embedded MOFs in the composites. Thermogravimetric analysis (TGA) measurements recorded in air on printed (60:40)-PLA/ZIF-8 (
(30) PLA is insoluble in CH.sub.3OH, therefore no morphological changes were observed in the test object. The TGA trace for the activated (60:40)-PLA/ZIF-8 composite (
(31) The surface areas (SAs) of extruded and printed ZIF-8/PLA composites, an important metric to further assess the gas accessibility to the MOFs and their presentation within the composites, were determined using the Brunauer-Emmett-Teller (BET) method from nitrogen adsorption experiments at 196 C. Extruded filament (d=1750 m) with 40% ZIF-8 loading and no other post-processing yielded a low BET surface area (<5 m.sup.2 g.sup.1). After solvent exchange (CH.sub.3OH soak for 48 hours) and evacuation, higher N.sub.2 adsorption occurred, yielding a SA BET of 105 m.sup.2 g.sup.1 with a slight increase in apparent microporosity (
(32) An additional demonstration of MOF functionality in an item printed using the (60:40)-PLA/ZIF-8 composite filament is provided according to the results in
(33) Visualization of the activated, printed (60:40)-PLA/ZIF-8 object using HeIM (
(34) The formation of the complex internal structure in the printed PLA composites was unexpected. One would reasonably expect that PLA, as well as other rigid matrix polymers, extruded rapidly during the printing of the composite filament may not have sufficient time to fully reorganize around the MOF particles. To address a possible effect of the residence time at the print nozzle and the relationship to the pore network, a (60:40) PLA/ZIF-8 filament feedstock was printed at a wide range of extrusion speeds from 1-186 mm s.sup.1, treated with CH.sub.3OH, evacuated for activation, and submitted to obtain N.sub.2 adsorption isotherms. The print speed over this range was found to have little effect on the total surface area or the features of the isotherm and the average SA across print conditions was 53136 m.sup.2 g.sup.1 for printed samples with (60:40)-PLA/ZIF-8 composition. The gas adsorption of the printed strands decreased with lower ZIF-8 loadings (20 and 30%) when fabricated by similar means to the 40% sample (
(35) PLA/ZIF-8 based composite formulations are promising in that they can be reproducibly processed, printed up to loadings of at least 40% MOF by mass to yield large surface areas, and participate in chemical interactions as if they were free powders as demonstrated by their ability to undergo solvent exchange in the pores of ZIF-8 and to uptake a test-dye. The materials can be routinely handled and fabricated into complex devices such as a waffle shaped sorbent (
(36) 3D printing and characterization of flexible polymer-MOF composites
(37) ZIF-8 composites were processed into FFF composite filaments with TPU base polymer matrices. TPUs can demonstrate substantial flexibility by sustaining up to 600% elongation while simultaneously retaining structural stability with a shore hardness of 98 A. Applying the methods of making described herein to a non-rigid matrix polymer shows the methods' versatility. TPU-based 3D printing, although less established than PLA or ABS matrices for FDM, offers a significant advantage of high flexibility that if conferred to a MOF composite could be useful in device fabrication. A TPU (e.g., Ninjatek Semiflex) stock solution (0.1 g mL.sup.1) was prepared by dissolving TPU filament (5.0 g) in DMF (50 mL) while stirring at 55 C. Upon dissolution, the stock solution was stored at room temperature. A typical composite with a total mass of 2 g and ZIF-8 loading of 40% by mass was achieved first by dispersing ZIF-8 (800 mg) in acetone (15 mL) by bath sonication for 15 min. The TPU stock solution (24 mL) was then added to the MOF solution, blended, cast, then dried as with the PLA-MOF composite.
(38) Ternary composites can also be made. In some embodiments, in addition to the matrix polymer and the MOF, a sacrificial polymer is included to affect the internal structure and porosity of the composite filament. For a composite with composition (50:40:10)-Semiflex/ZIF-8/PVDF-HFP and a total mass of 2 g, ZIF-8 was first dispersed in acetone by bath sonication for 10 min. A PVDF-HFP stock solution (0.1 g mL.sup.1 in DMF, 2 mL) was added to the MOF solution and blended by bath sonication for 10 min. The PVDF-HFP is a sacrificial polymer. Lastly, a Semiflex solution (0.1 g mL.sup.1 in DMF) was added to the ZIF-8/PVDF-HFP mixture, stirred by gently shaking the mixture (1 min), then blended by ultrasonic horn for 10 min. The composite was cast and dried as above. Unexpectedly, Semiflex composites without MOF, with composition of (80:20)-Semiflex/PVDF-HFP, exhibited excessive swelling prohibiting access to printable filament material. The control experiment result provides support for high MOF filler ratios contributing in the reduction of die swell when working with PVDF-HFP.
(39) Post-printing treatment was applied to remove the sacrificial polymer. Removal of PVDF-HFP from Semiflex/ZIF-8/PVDF-HFP composites was performed by submerging the material in boiling acetone for 10 min, removing the acetone, washing the material with deionized water (3), and drying the sample in a low vacuum oven as with the activation procedure. The procedure for solvent exchange and activation of the TPU-based composite filaments was similar to that for the PLA-based composite filaments.
(40) Semiflex/ZIF-8 composites were prepared and successfully extruded into filament feedstocks with ZIF-8 loadings as high as 50% wt. The Semiflex/ZIF-8 composite filament retained high flexibility even with these high loadings and PXRD experiments confirmed that the Zn-framework particles remained highly crystalline after processing (
(41) Printed binary composites of Semiflex/ZIF-8 were observed to have low specific surface areas (68 m.sup.2 g.sup.1 at 50% ZIF-8 loading) only slightly larger than that of printed Semiflex without any MOF loaded as determined from N.sub.2 adsorption experiments. The surface area increased marginally after CH.sub.3OH solvent exchange treatment to 98 m.sup.2 g.sup.1 at 50% ZIF-8 loading (
(42) To increase the specific surface area and exposure of the pores within embedded MOF crystals in the Semiflex matrix, a second highly flexible fluoropolymer was introduced to form a Semiflex/ZIF-8/PVDF-HFP ternary composite (
(43) Initially, the printed and untreated Semiflex/ZIF-8 composites with PVDF-HFP incorporated had similarly poor N.sub.2 adsorption characteristics to the binary composites, where 10% PVDF-HFP yielded SA BET=32 m.sup.2 g.sup.1 (
(44) The macro- and micro-structure on the surface and the interior of the as-printed (40:40:20)-Semiflex/ZIF-8/PVDF-HFP and after acetone treatment was further examined by HeIM (in some cases scanning electron microscopy (SEM)) with accompanying elemental mapping (
(45) The approach to first prime the MOF crystals with PVDF-HFP prior to incorporation into the Semiflex matrix and the resulting higher relative concentration at the surface in the ternary composites helped enable rapid exposure of the MOFs post-printing. The dissolution and removal of 59% PVDF-HFP in the sample results in widespread micron to submicron scale-etching of the surface. MOF particles appear intertwined through the remaining polymeric matrix at the surface (
(46) The chemistry of the MOFs within the printed Semiflex composites was further assessed. CO.sub.2 sorption in the post-acetone treated Semiflex/ZIF-8/PVDF-HFP sample, measured at pressures up to 1 bar at 298 K, increased significantly over a (100%)-Semiflex sample printed control (
(47) The method of formulating a ternary polymer-MOF composite filament, printing, removing the sacrificial polymer, and retaining a high surface-area can be extended to other types of MOFs. UiO-66, a versatile framework comprised of Zr centers with 1,4 benzenedicarboxylate linkers and a measured surface area of 1144 m.sup.2 g.sup.1 was formulated into a filament with composition (40:40:20)-Semiflex/UiO-66/PVDF-HFP without any modification of the procedure (used for ZIF-8) and was readily printed. After acetone treatment, the surface area was 303 m.sup.2 g.sup.1 and the microporous character within the composite, which was absent prior to sacrificial polymer removal (
(48) In view of the many possible embodiments to which the principles of the disclosed invention may be applied, it should be recognized that the illustrated embodiments are only preferred examples of the invention and should not be taken as limiting the scope of the invention. Rather, the scope of the invention is defined by the following claims. We therefore claim as our invention all that comes within the scope and spirit of these claims.