1. Introduction
Since the inception of sintered tungsten carbide cobalt (WC-Co) hardmetal by Karl Schröter in the 1920s, the quest among researchers and manufacturers to develop more efficient and cost-effective production methods for hardmetals with improved properties and intricate geometries has been ongoing. Also known as cemented carbides, hardmetals are composite materials of hard, brittle WC grains embedded within a soft, ductile metallic matrix, typically composed of Co, Fe, or Ni. Moreover, hardmetals often include additional carbides like TiC, TaC, Cr3C2, NbC, or Mo2C, which serve as inhibitors of WC-grain growth [
1,
2,
3]. WC-10Co hardmetals are highly valued for their exceptional hardness and toughness, qualities that render them ideal for producing tools subjected to heavy impact and wear. These applications include the manufacturing devices like anvils, cutters, slitters, drills, as well as tools used in cold-working and mining [
4].
Additive manufacturing (AM) offers a compelling alternative for producing WC-Co components, notable for its ability to create new geometries and cost-effectively produce small batches. Notably, AM allows for incorporating the complex features without increasing production costs, leading to its characterization as a “complexity for free” process [
5]. Additive Manufacturing technologies for hardmetals include beam-based methods like Directed Energy Deposition (DED), Laser Engineering Net Shaping (LENS)[
6], Direct Laser Fabrication (DLF)[
7], Selective Laser Sintering (SLS) [
8,
9], Selective Laser Melting (SLM) [
10], which sequentially produce each hardmetal layer and managing anisotropy variations is a key challenge. In contrast, beamless methods like Fused Filament Fabrication (FFF), Composite Extrusion Manufacturing (CEM), Binder Jetting (BJ), and 3D gel/direct-ink-write/robo-casting use a mix of powders and binder systems[
11]. Indeed, in beamless methods, so-called “green parts” are constructed layer by layer. However, these parts require further post-treatment processes. This involves the removal of the binder or debinding and a sintering step, both essential to achieving the final, fully structured part with desired physical and mechanical properties [
12]. Beamless methods tend to produce microstructures with lower residual stresses since the entire part is sintered simultaneously [
11,
13], and overcome the new layer cooling dynamics of beam-based AM methods [
14].
The material extrusion process, specifically for polymeric filaments, was first patented by Stratasys [
15] under the trademark Fused Deposition Modelling or (FDM
TM). Later, the term Fused Filament Fabrication (FFF), was introduced as an open, non-registered name for the technology [
16]. Influenced by Powder Injection Molding (PIM), FFF was adapted to shape metals, ceramics, and composites in a three-step process: Shaping (by PIM or FFF), Debinding (solvent and/or thermal), and Sintering (SDS) [
17,
18]. Pioneering research by Agarwala, et al. [
19] led to the first binder system developed for the FFF processing of Si
3N
4 parts. Subsequent studies highlighted the necessity for tailored binder systems for different powdered materials [
20].
In FFF, the filament serves dual purposes as the extrusion driver and the extruded material. If the viscosity of the filament is too high or its strength too low, the feedstock can become unprintable, often failing due to buckling [
21]. Additionally, the filament must withstand spooling processes and when printed, the part must support internal pressure generated during solvent and thermal debinding, which might cause defects like cracking and blistering [
22,
23]. Styrene-ethylene/butylene-styrene (SEBS) thermoplastic elastomers have been effective in FFF binder formulations due to their flexibility and solubility in the first debinding stage [
24,
25,
26,
27]. When working with submicrometric particles, adding Paraffin Wax to SEBS in the binder system can effectively modulate viscosity and facilitate the debinding [
28].
Polyolefins such as Polypropylene and Polyethylene are commonly used as backbone materials. Nevertheless materials such as EVA and PLA have been reported [
28]. MCNulty, et al. [
29] developed binder systems for the FFF of Lead zirconate titanate (PZT) samples, utilizing polyolefins and Hydrocarbon resin. Their research demonstrated the potential of adapting commercially available materials to create FFF-compatible feedstocks. Various research efforts, including those by Cano et al. [
30] ZrO2 and Momeni et al. [
31] for Al, have focused on using grafted and non-grafted polyolefins as backbones in FFF feedstocks. These studies revealed improvements in powder dispersion and rheological behavior, accompanied by a slight increase in the viscosity of the feedstocks. Lengauer, et al. [
32] successfully printed, debinded, and sintered WC-10Co and Ti(C,N)-Co/Ni-based Cermets using TPE as a soluble polymer and PP functionalized with maleic anhydride. They highlighted the need for optimized printing strategies to achieve defect-free microstructures, which aligns with Agarwala et al. [
33] who developed printing strategies to rectify defects in Si
3N
4 and 17-4ph stainless steel (SS) printed by FFF.
Additionally, Agarwala et al. [
34] crafted unique binder systems for WC-Co, SiO
2, 17-4 PH SS, Si
3N
4, and Al2O3, observed that smaller particle sizes in the same binder system, due to their increased surface area, led to higher viscosity in the feedstocks, prompting the need for reformulations incorporating different surfactants in the binder system to manage this challenge. Surfactants based on fatty acids with long carbon chains, such as Stearic Acid (SA) are effective for WC-Co in polymeric binders, as demonstrated in different studies [
35,
36]. The feedstock's viscosity, the liquefier system's geometrical factors, and the layer height have been modeled to relate them with the extrusion force of ABS and PLA [
37,
38] alloying to describe it with the final properties of the printed material.
This study will investigate various binder formulations for WC-10Co in Fused Filament Fabrication (FFF), focusing on how binder composition and backbone content impact the printing force, the emergence of green part defects and their dependence on the printing parameters, and their effects on the microstructure and hardness of sintered hard metals.
2. Materials and Methods
2.1. Materials
This study employed hardmetal ready-to-press powders, consisting of 10 wt% cobalt (Co) and a balance of tungsten carbide (WC). These powders were agglomerated using a spray drying process with an addition of 1 wt% paraffin wax, supplied by ZCC (China). The binder systems included a combination of both soluble and non-soluble polymers. The soluble components comprised Thermoplastic Elastomer TPE (Sungallon, China), Paraffin Wax (PW) as a viscosity modulator (Panreac), and Stearic Acid (SA) as a surfactant (Sigma Aldrich). Additionally, the system incorporated a mixture of Polypropylene Random-Copolymer (PP) (Essentia, Colombia) and Polypropylene Grafted with Maleic Anhydride (PP-MA), which served as the backbone.
We prepared four different formulations to investigate the impact of the backbone's content and composition on the feedstocks. We varied the backbone composition using ratios of PP-MA to PP at 3:2 and 2:3. Additionally, we used two distinct backbone contents in the binder system: 26 wt% and 31 wt%. To offset the variations in backbone content, we added additional TPE. Throughout the experiment, we kept both SA and PW constant (See
Table 1).
The feedstocks were prepared using a shear-based mixing apparatus. Initially, the polymers underwent a homogenization process for 10 minutes. This process was followed by the gradually adding powders into the molten mixture, executed in three distinct stages. The mixture was then continuously mixed for 60 minutes at a temperature of 160 °C. After mixing, the feedstocks were cut into small pieces, each measuring less than 5 mm in every dimension. These fragments were used to produce filament, employing a single-screw extruder with a 1.75 mm diameter die, operating at 180°C. To assess the changes in the binder system resulting from the powder addition, 50g of each binder type was mixed. However, the powder-free samples were subjected to an identical homogenization duration of 60 minutes to ensure a standardized comparison. To distinguish between the samples, 'M' without the suffix 'P' will denote the binder system alone, while 'M+P' will indicate the binder system mixed with the hardmetal powder.
2.2. Thermal Properties
The thermal properties of the feedstocks and the binder systems were analyzed using Differential Scanning Calorimetry (DSC) (Mettler Toledo). The materials were incrementally heated from room temperature to 250°C at a rate of 10 °C/min, under a nitrogen flow of 50ml/min. The crystallinity degree of each virgin polymer, binder system, and feedstock was calculated using the formula [
39]:
Where
represents the fusion enthalpy (derived from the integral of the endothermic peak on the DSC curve), and
is the enthalpy of fully crystalized PP (207 J/g) [
40], and
is the weight fraction of PP in the analyzed sample.
To evaluate the thermal stability of both the binder systems and the feedstocks, a Thermogravimetric Analysis (TGA) (Mettler Toledo). The samples were heated up to 700 °C at a rate of 10 °C/min under a nitrogen flow of 50.0 ml/min. During this process, the samples' weight and the rate of weight loss were measured.
2.3. Printing Force Measurements
A custom-built Arduino-based device was employed to measure the extrusion force of each filament. Equipped with two 5 kg load cells, this device featured a mechanism to maintain the FFF extrusion system's alignment and isolate it from the pulling motor. The filaments were tested at extrusion speeds of 7.5 and 10 mm/s, and at temperatures of 200, 210, and 220°C and 20 cm of tested material in each run. Each experimental setup was replicated three times, with the resulting data being collected at a frequency of 0.2 Hz, for further analysis to calculate the average extrusion force. The nozzle had a diameter of 0.6 mm, and the extrusion system was configured to mimic the standard FFF machine used in the printing experiments. The systematic error in measuring the extrusion force was determined to be less than 0.2N. Care was taken to use 1.75mm filaments to avoid error due to the higher transversal area of any filaments.
2.4. Printing
An Ender 3 V2 FFF printer, specifically modified to include a direct extrusion drive system, was used to shape cylindrical samples with a diameter of 17 mm and a height of 7 mm. Five samples were printed at three different printing temperatures for each feedstock: 200, 210, and 220°C for 80 samples (60 printed at 10 mm/s and 20 additional printed at 7.5mm/s). The layer thickness and nozzle diameter settings were maintained at 0.3 mm and 0.6 mm, respectively. A printing flow of 103% was used for all the samples.
2.5. Debinding and Sintering
After printing the samples were immersed in cyclohexane for 72 h to remove the soluble polymers. Next, a vacuum furnace performed the thermal debinding and sintering in one single step. Considering the focus of this study does not extend to the macro-scale analysis of sintering and debinding stages, a non-optimized thermal debinding cycle was utilized, featuring a heating rate of 0.2 °C/min between 400 and 550 °C, next a sintering plateau of 60 minutes at 1500°C was employed for final densification of the samples. The sintering process for the samples was conducted within graphite containers to prevent decarburization, using an argon atmosphere for protection.
2.5. Characterization
The density of the printed and sintered samples was determined using the Archimedes method, with 99.9% ethanol employed to enhance the wetting of the sample surfaces. To identify various defects after printing and correlate them with the feedstocks and printing temperatures used, a cryogenic 3-point bending test was conducted on one sample from each feedstock configuration. The test setup involved placing the samples on two rods, each 10 mm in diameter, spaced 14 mm apart at their centers. A third rod of the same diameter was advanced at a 1 mm/min rate until the sample fractured. Before testing, the green samples were immersed in liquid nitrogen for 10 minutes to ensure uniform internal temperature. After sintering, the samples were sectioned, subjected to diamond polishing for a smooth finish, and then analyzed. Both light-optical microscopy (OM) (Zeiss Z1.m) and Scanning Electron Microscopy (SEM) (Phenom XL) were used to examine the green and sintered samples closely. The Digital Image software ImageJ™ was utilized for analyzing SEM micrographs to measure the grain size.
5. Conclusions
Four distinct feedstocks were developed and assessed for their performance in Fused Filament Fabrication of WC-10Co samples. This research paves the way for future studies to refine depolymerization and sintering pathways, establishing a foundational understanding of the importance of feedstock and green sample. The main findings of this study were:
Feedstocks exhibiting lower printing forces tended to develop more defects, which typically persisted through the liquid phase sintering process. Enhancing the ratio of PP-MA to PP within the feedstock improved this situation by facilitating better interaction between the particle surfaces and the binder. This adjustment effectively reduced the melting feedstock's tendency to stick to the printing nozzle, thus mitigating the formation of printing defects.
An increased presence of PP-MA was not directly linked to a significant rise in printing force. Yet, it had a noticeable effect on the mechanical properties of the sintered hard metal. This highlights the importance of a binder system compatible with the powder surface in influencing the outcomes of the sintering process. Future efforts in feedstock formulation will focus on increasing PP-MA content within the binder system to enhance feedstock performance. However, it's crucial to understand that each specific feedstock will necessitate a customized thermal debinding curve. This tailored approach is vital to preventing defect formation during polymer degradation and optimizing the sintered density of the samples, ensuring the successful application of these materials in the FFF manufacturing processes.
The approach for measuring printing force proved to be a quick, cost-effective, and efficient method for rapidly validating different feedstock formulations. However, it necessitates additional efforts to accurately correlate the force response with rheological properties, ensuring that the method's effectiveness extends beyond preliminary assessments to provide a more comprehensive understanding of material behavior. Additionally, adjusting printing speed was found to be a more effective method for reducing printing force than increasing the printing temperature. This adjustment significantly impacts the mechanical properties of the printed parts, highlighting the need for a balance to minimize defects while maximizing final density and hardness.
Author Contributions
Conceptualization, J.D.R.B; methodology, J.D.R.B; software, J.D.R.B; validation, J.D.R.B, A.F.G.P, L.K.H,Q and L.A.B.M; formal analysis, J.D.R.B; investigation, J.D.R.B, A.F.G.P; resources, A.F.G.P, L.K.H,Q and L.A.B.M; data curation, J.D.R.B; writing—original draft preparation, J.D.R.B; writing—review and editing, J.D.R.B, A.F.G.P, L.K.H,Q and L.A.B.M; visualization, J.D.R.B; supervision, L.K.H,Q and L.A.B.M; project administration, L.K.H,Q; funding acquisition, L.K.H,Q.
Figure 1.
DSC curves of a) Raw polymers, binder systems and binder systems mixed with WC-10Co powders, b) Magnification of the binder systems mixed with the powders.
Figure 1.
DSC curves of a) Raw polymers, binder systems and binder systems mixed with WC-10Co powders, b) Magnification of the binder systems mixed with the powders.
Figure 2.
TGA results of the studied feedstocks, a) Mass-loss temperature diagram, b) Derivative mass calculation.
Figure 2.
TGA results of the studied feedstocks, a) Mass-loss temperature diagram, b) Derivative mass calculation.
Figure 3.
Force measurements for manufactured feedstocks: (a) Variation with temperature and extrusion speed, (b) Test at ambient temperature leading to filament failure.
Figure 3.
Force measurements for manufactured feedstocks: (a) Variation with temperature and extrusion speed, (b) Test at ambient temperature leading to filament failure.
Figure 4.
Relative green densities for different feedstocks and printing temperatures.
Figure 4.
Relative green densities for different feedstocks and printing temperatures.
Figure 5.
SEM-BSE details and Optical Microscopy of the Green Samples printed at 10 mm/s after cryogenic fracture for the different feedstocks: a), b) M1-P printed at 200°C and 220°C respectively, c), d) M2-P printed at 200°C and 220°C respectively, e), f) M3-P printed at 200°C and 220°C respectively, g), h) M4-P printed at 200°C and 220°C respectively.
Figure 5.
SEM-BSE details and Optical Microscopy of the Green Samples printed at 10 mm/s after cryogenic fracture for the different feedstocks: a), b) M1-P printed at 200°C and 220°C respectively, c), d) M2-P printed at 200°C and 220°C respectively, e), f) M3-P printed at 200°C and 220°C respectively, g), h) M4-P printed at 200°C and 220°C respectively.
Figure 6.
SEM-BSE details and Optical Microscopy of the green samples printed at 7.5 mm/s after cryogenic fracture for the different feedstocks: a) M1-P, a) M2-P, a) M3-P, a) M4-P.
Figure 6.
SEM-BSE details and Optical Microscopy of the green samples printed at 7.5 mm/s after cryogenic fracture for the different feedstocks: a) M1-P, a) M2-P, a) M3-P, a) M4-P.
Figure 7.
Relative densities of the samples printed at 200°C at different speeds, a) Green state, b) after sintering.
Figure 7.
Relative densities of the samples printed at 200°C at different speeds, a) Green state, b) after sintering.
Figure 8.
Backscattered SEM micrographs of the sintered samples printed at 200°C made with the developed feedstocks, centered in the carbon precipitated areas printed ad different speeds a) M1-P at 10 mm/s, b) M1-P at 7.5 mm/s, c) M2-P at 10 mm/s, d) M2-P at 7.5 mm/s, e) M3-P at 10 mm/s, f) M3-P at 7.5 mm/s, g) M4-P at 10 mm/s, h) M4-P at 7.5 mm/s.
Figure 8.
Backscattered SEM micrographs of the sintered samples printed at 200°C made with the developed feedstocks, centered in the carbon precipitated areas printed ad different speeds a) M1-P at 10 mm/s, b) M1-P at 7.5 mm/s, c) M2-P at 10 mm/s, d) M2-P at 7.5 mm/s, e) M3-P at 10 mm/s, f) M3-P at 7.5 mm/s, g) M4-P at 10 mm/s, h) M4-P at 7.5 mm/s.
Figure 9.
Developed feedstocks after printing at 200°C and sintering at 1500°C a) Violin-plot of grain size from data obtained with digital image processing, b) Vickers hardness.
Figure 9.
Developed feedstocks after printing at 200°C and sintering at 1500°C a) Violin-plot of grain size from data obtained with digital image processing, b) Vickers hardness.
Figure 10.
Persistence of printing defects after the sintering process: a) mountain-like defect found in M2-P feedstock, b) Lack of filling between internal infill lines and the outer layer found in M4-P Feedstock, c) Entrapped gas found in M3-P feedstock.
Figure 10.
Persistence of printing defects after the sintering process: a) mountain-like defect found in M2-P feedstock, b) Lack of filling between internal infill lines and the outer layer found in M4-P Feedstock, c) Entrapped gas found in M3-P feedstock.
Table 1.
Formulated binder Systems (52%vol) to be mixed with 48%vol WC-Co powders.
Table 1.
Formulated binder Systems (52%vol) to be mixed with 48%vol WC-Co powders.
Binder |
PP-MA |
PP |
TPE |
PW |
SA |
|
%wt. |
%wt. |
%wt. |
%wt. |
%wt. |
M1 |
18.62 |
12.42 |
46.56 |
18,00 |
4.40 |
M2 |
15.60 |
10.40 |
51.60 |
18.00 |
4.40 |
M3 |
12.42 |
18.62 |
46.56 |
18.00 |
4.40 |
M4 |
10.40 |
15.60 |
51.60 |
18.00 |
4.40 |
Table 2.
Key Printing Parameters Utilized.
Table 2.
Key Printing Parameters Utilized.
Infill Pattern |
Number of External Lines |
Infill Overlap |
Retraction |
Bed Temperature |
Cooling fan |
Lines |
1 |
50% |
No |
95 °C |
Off |
Table 3.
Calculated data.
Table 3.
Calculated data.
Description |
|
T onset |
T endset |
|
|
PP |
148.59 |
133.5 |
155.7 |
91.03 |
43.98% |
PP-MA |
161.05 |
153.7 |
168.5 |
105.18 |
50.81% |
TPE |
- |
|
|
- |
- |
M1 |
145.93 |
123.76 |
153.54 |
41.19 |
54.32% |
M1+P |
145.63 |
128.18 |
151.51 |
1.72 |
43.20% |
M2 |
144.22 |
130.40 |
149.86 |
29.33 |
46.24% |
M2+P |
144.43 |
123.42 |
150.32 |
1.04 |
31.20% |
M3 |
145.76 |
135.56 |
153.74 |
32.46 |
45.25% |
M3+P |
145.69 |
125.76 |
151.48 |
0.88 |
22.07% |
M4 |
146.06 |
133.25 |
151.68 |
18.23 |
28.76% |
M4+P |
143.59 |
126.31 |
149.55 |
0.83 |
24.77% |
Table 4.
Results of the Two-way ANOVA for Green Density of Printed Samples.
Table 4.
Results of the Two-way ANOVA for Green Density of Printed Samples.
Source of Variation |
Degrees of Freedom |
Sum Sq |
Mean Sq |
P Value |
Temperature |
2 |
5.88 |
8.78 |
5.65e-4 |
Feedstock |
3 |
8.38 |
8.33 |
1.46e-4 |
Temperature: Feedstock |
6 |
15.18 |
7.55 |
9.89e-6 |
Residuals |
48 |
16.09 |
|
|
Table 5.
Results of the Two-way ANOVA for green density of printed Samples at different feedstocks and velocity.
Table 5.
Results of the Two-way ANOVA for green density of printed Samples at different feedstocks and velocity.
Source of Variation |
Degrees of Freedom |
Sum Sq |
Mean Sq |
P Value |
Velocity |
1 |
0.156 |
0.1563 |
0.32372 |
Feedstock |
3 |
2.183 |
0.7277 |
0.00806 |
Velocity: Feedstock |
3 |
1.372 |
0.4572 |
0.04800 |
Residuals |
32 |
4.978 |
0.1556 |
|
Table 6.
Results of the Two-way ANOVA for sintered density of the samples printed at 200°C.
Table 6.
Results of the Two-way ANOVA for sintered density of the samples printed at 200°C.
Source of Variation |
Degrees of Freedom |
Sum Sq |
Mean Sq |
P Value |
Velocity |
1 |
17672 |
3.782 |
0.0696 |
Feedstock |
3 |
47619 |
10.192 |
0.0005 |
Velocity: Feedstock |
3 |
5685 |
1.217 |
0.3358 |
Residuals |
16 |
4672 |
|
|