Author Contributions
Conceptualization, G.D.B.-P. and M.V.C.-O.; methodology, G.D.B.-P. and M.J.T.-C.; software, G.D.B.-P.; validation, G.D.B.-P. and M.V.C.-O.; formal analysis, G.D.B.-P.; investigation, G.D.B.-P.; resources, M.V.C.-O.; data curation, G.D.B.-P.; writing—original draft preparation, G.D.B.-P. and M.V.C.-O.; writing—review and editing, G.D.B.-P. and M.V.C.-O.; visualization, M.V.C.-O. and M.J.T.-C.; supervision, M.V.C.-O.; project administration, M.V.C.-O.; funding acquisition, M.V.C.-O. All authors have read and agreed to the published version of the manuscript.
Figure 1.
Process of PDLLA oligomerization. (a) Product at the end of the reaction. (b) Dissolution of the formed product. (c) Precipitate formation. (d) Vacuum filtration for precipitate recovery. (e) Oligomer placed in a Petri dish for subsequent drying. (f) Dried oligomer.
Figure 1.
Process of PDLLA oligomerization. (a) Product at the end of the reaction. (b) Dissolution of the formed product. (c) Precipitate formation. (d) Vacuum filtration for precipitate recovery. (e) Oligomer placed in a Petri dish for subsequent drying. (f) Dried oligomer.
Figure 2.
Process of PDLLA depolymerization. (a) Oligomer used, obtained in the previous stage. (b) Reaction product. (c) Boiling ethyl acetate. (d) Onset of lactide crystallization. (e) Lactide after refrigeration. (f) Dried lactide.
Figure 2.
Process of PDLLA depolymerization. (a) Oligomer used, obtained in the previous stage. (b) Reaction product. (c) Boiling ethyl acetate. (d) Onset of lactide crystallization. (e) Lactide after refrigeration. (f) Dried lactide.
Figure 3.
Process of ring-opening polymerization. (a) Dried lactide used for the reaction. (b) Catalyst addition. (c) Initiator. (d) Dissolution in chloroform. (e) Precipitation in methanol. (f) Vacuum filtration result. (g) Dried high-molecular-weight PDLLA.
Figure 3.
Process of ring-opening polymerization. (a) Dried lactide used for the reaction. (b) Catalyst addition. (c) Initiator. (d) Dissolution in chloroform. (e) Precipitation in methanol. (f) Vacuum filtration result. (g) Dried high-molecular-weight PDLLA.
Figure 4.
FTIR spectrum of standard PDLLA.
Figure 4.
FTIR spectrum of standard PDLLA.
Figure 5.
FTIR spectrum of PDLLA samples.
Figure 5.
FTIR spectrum of PDLLA samples.
Figure 6.
The 1H-NMR spectrum of PLA-7 sample recorded at 500 MHz in CDCl3 at 25 °C. The characteristic signals observed include: (a) methine protons (CH) of the polymer backbone at 5.18 ppm, (b) methyl protons (CH3) of the repeating units at 1.58 ppm, (c) methine proton (CH) of the terminal group at 4.38 ppm, and (d) methyl protons (CH3) of the terminal group at 1.47 ppm.
Figure 6.
The 1H-NMR spectrum of PLA-7 sample recorded at 500 MHz in CDCl3 at 25 °C. The characteristic signals observed include: (a) methine protons (CH) of the polymer backbone at 5.18 ppm, (b) methyl protons (CH3) of the repeating units at 1.58 ppm, (c) methine proton (CH) of the terminal group at 4.38 ppm, and (d) methyl protons (CH3) of the terminal group at 1.47 ppm.
Figure 7.
TGA diagrams. (a) Experiment #1. (b) Experiment #2. (c) Experiment #3.
Figure 7.
TGA diagrams. (a) Experiment #1. (b) Experiment #2. (c) Experiment #3.
Figure 8.
Residual plot for molecular weight. The figure displays three diagnostic plots used to evaluate the assumptions of ANOVA: (a) normal probability plot, where each dot represents a standardized residual; (b) residuals versus fitted values, showing the spread of residuals relative to predicted values; and (c) residuals versus observation order, where each point corresponds to a residual plotted in the sequence in which the data were collected. These plots are used to assess normality, homoscedasticity, and independence of residuals, respectively.
Figure 8.
Residual plot for molecular weight. The figure displays three diagnostic plots used to evaluate the assumptions of ANOVA: (a) normal probability plot, where each dot represents a standardized residual; (b) residuals versus fitted values, showing the spread of residuals relative to predicted values; and (c) residuals versus observation order, where each point corresponds to a residual plotted in the sequence in which the data were collected. These plots are used to assess normality, homoscedasticity, and independence of residuals, respectively.
Figure 9.
Main effects and interaction plot for molecular weight, where the dots represent the average molecular weight of PDLLA obtained under each experimental condition. The slope and direction of the lines indicate how each factor and their combination influence the molecular weight of the synthesized polymer.
Figure 9.
Main effects and interaction plot for molecular weight, where the dots represent the average molecular weight of PDLLA obtained under each experimental condition. The slope and direction of the lines indicate how each factor and their combination influence the molecular weight of the synthesized polymer.
Figure 10.
Pareto chart of standardized effects for molecular weight.
Figure 10.
Pareto chart of standardized effects for molecular weight.
Figure 12.
Molecular weight variation as a function of time at different reaction temperatures.
Figure 12.
Molecular weight variation as a function of time at different reaction temperatures.
Figure 13.
First-order kinetic plot for PLA polymerization: linear representation of Ln(Mt/(M − Mt)) as a function of time.
Figure 13.
First-order kinetic plot for PLA polymerization: linear representation of Ln(Mt/(M − Mt)) as a function of time.
Figure 14.
Arrhenius plot for the polymerization of PLA, showing the linear relationship between Ln(kp) and 1/T. The activation energy (Ea) and pre-exponential factor (A) were determined from the slope and intercept, respectively.
Figure 14.
Arrhenius plot for the polymerization of PLA, showing the linear relationship between Ln(kp) and 1/T. The activation energy (Ea) and pre-exponential factor (A) were determined from the slope and intercept, respectively.
Figure 15.
Scaffold. (a) Design using OpenSCAD software. (b) Segmentation using Cura software.
Figure 15.
Scaffold. (a) Design using OpenSCAD software. (b) Segmentation using Cura software.
Figure 16.
Three-dimensional printing tests.
Figure 16.
Three-dimensional printing tests.
Figure 17.
Three-dimension-printed PDLLA scaffold under the best-performing parameters.
Figure 17.
Three-dimension-printed PDLLA scaffold under the best-performing parameters.
Figure 18.
SEM images. (a) S01. (b) S02. (c) S03.
Figure 18.
SEM images. (a) S01. (b) S02. (c) S03.
Figure 19.
Force vs. strain curves for the scaffolds.
Figure 19.
Force vs. strain curves for the scaffolds.
Table 1.
Quantities of components used in the synthesis.
Table 1.
Quantities of components used in the synthesis.
Sample Code | Oligomerization Time (h) | ROP Time (h) | % by Weight of Tin Octoate Catalyst |
---|
PLA-1 | 4 | 4 | 1 |
PLA-2 | 4 | 4 | 2 |
PLA-3 | 4 | 6 | 1 |
PLA-4 | 4 | 6 | 2 |
PLA-5 | 6 | 4 | 1 |
PLA-6 | 6 | 4 | 2 |
PLA-7 | 6 | 6 | 1 |
PLA-8 | 6 | 6 | 2 |
Table 2.
Weights of lactic acid used at the beginning of the synthesis and of the products at the end of each stage.
Table 2.
Weights of lactic acid used at the beginning of the synthesis and of the products at the end of each stage.
Sample Code | Experiment Number | Lactic Acid Weight (g) | Dried Low-Molecular-Weight PDLLA Weight (g) | Dried Lactide Weight (g) | Dried High-Molecular-Weight PDLLA Weight (g) |
---|
PLA-1 | 1 | 60.543 | 11.298 | 2.272 | - |
2 | 60.478 | 11.243 | 2.165 | - |
3 | 60.450 | 11.145 | 2.122 | - |
PLA-2 | 1 | 60.456 | 11.221 | 2.140 | - |
2 | 60.498 | 11.186 | 2.129 | - |
3 | 60.470 | 11.200 | 2.137 | - |
PLA-3 | 1 | 60.557 | 11.320 | 2.251 | - |
2 | 60.469 | 11.238 | 2.153 | - |
3 | 60.478 | 11.239 | 2.159 | - |
PLA-4 | 1 | 60.502 | 11.189 | 2.128 | - |
2 | 60.499 | 11.191 | 2.130 | - |
3 | 60.489 | 11.187 | 2.128 | - |
PLA-5 | 1 | 60.449 | 38.440 | 15.716 | 4.964 |
2 | 60.572 | 38.789 | 16.023 | 5.159 |
3 | 60.461 | 38.549 | 16.234 | 5.767 |
PLA-6 | 1 | 60.448 | 38.096 | 15.844 | 4.427 |
2 | 60.603 | 38.980 | 16.427 | 4.842 |
3 | 60.588 | 39.097 | 16.234 | 4.631 |
PLA-7 | 1 | 60.462 | 38.773 | 16.126 | 10.503 |
2 | 60.466 | 38.794 | 16.423 | 10.984 |
3 | 60.453 | 38.726 | 16.121 | 10.558 |
PLA-8 | 1 | 60.557 | 39.350 | 16.387 | 7.837 |
2 | 60.669 | 39.144 | 16.209 | 7.435 |
3 | 60.477 | 38.143 | 15.987 | 7.234 |
Table 3.
Average molecular weight per sample code.
Table 3.
Average molecular weight per sample code.
Sample Code | Molecular Weight (g/mol) | Coefficient of Variation (%) | Average Molecular Weight (g/mol) |
---|
Experiment #1 | Experiment #2 | Experiment #3 |
---|
PLA-5 | 26,781.24 | 26,944.24 | 28,958.42 | 4.4 | 27,561.30 |
PLA-6 | 14,386.82 | 14,211.91 | 14,814.55 | 2.1 | 14,471.10 |
PLA-7 | 120,457.89 | 117,452.10 | 119,331.80 | 1.3 | 119,080.60 |
PLA-8 | 44,563.81 | 45,142.18 | 43,370.76 | 2.0 | 44,358.92 |
Table 4.
Thermal properties for each sample code concerning its molecular weight.
Table 4.
Thermal properties for each sample code concerning its molecular weight.
Sample Code | Molecular Weight (g/mol) | Tg (°C) | Tm (°C) | ΔHm (J/g) | χ (%) |
---|
PLA-5 | 27,561.30 | 50.16 | 136.89 | 43.73 | 46.67 |
PLA-6 | 14,471.10 | 49.16 | 133.45 | 41.80 | 44.61 |
PLA-7 | 119,080.60 | 52.77 | 143.57 | 44.87 | 47.88 |
PLA-8 | 44,358.92 | 52.26 | 143.28 | 44.37 | 47.35 |
Table 5.
PDLLA degradation temperature.
Table 5.
PDLLA degradation temperature.
Sample Code | Experiment Number | Degradation Temperature (°C) |
---|
PLA-5 | 1 | 263.23 |
2 | 259.71 |
3 | 263.52 |
PLA-6 | 1 | 266.50 |
2 | 278.92 |
3 | 264.22 |
PLA-7 | 1 | 251.79 |
2 | 253.81 |
3 | 254.65 |
PLA-8 | 1 | 271.98 |
2 | 274.53 |
3 | 267.67 |
Table 6.
ANOVA for molecular weight.
Table 6.
ANOVA for molecular weight.
Source | DF | Adjusted SS | Adjusted MS | F-Value | p-Value |
---|
Model | 3 | 19,686,791,944 | 6,562,263,981 | 5598.35 | 0.000 |
ROP time | 1 | 11,054,767,100 | 11,054,767,100 | 9430.95 | 0.000 |
Catalyst concentration | 1 | 5,783,195,404 | 5,783,195,404 | 4933.71 | 0.000 |
ROP time × catalyst concentration | 1 | 2,848,829,440 | 2,848,829,440 | 2430.37 | 0.000 |
Error | 8 | 9,377,433 | 1,172,179 | | |
Total | 11 | 19,696,169,377 | | | |
Table 7.
Evolution of molecular weight over time at different reaction temperatures.
Table 7.
Evolution of molecular weight over time at different reaction temperatures.
| Temperature (°C) |
---|
Time (min) | 150 °C | 160 °C | 170 °C | 180 °C |
---|
0 | 0 | 0 | 0 | 0 |
20 | 19.09 | 27.06 | 39.73 | 63.36 |
40 | 22.34 | 37.44 | 55.97 | 94.35 |
60 | 23.92 | 43.91 | 70.89 | 118.92 |
80 | 29.31 | 48.32 | 80.30 | 130.30 |
100 | 34.67 | 52.63 | 89.97 | 138.13 |
120 | 35.94 | 59.03 | 94.83 | 142.83 |
140 | 38.92 | 65.74 | 97.74 | 144.14 |
160 | 39.14 | 66.14 | 98.94 | 144.66 |
180 | 42.57 | 68.77 | 99.74 | 144.88 |
200 | 43.94 | 69.64 | 100.20 | 144.91 |
220 | 45.10 | 69.99 | 100.34 | 144.92 |
240 | 49.83 | 72.13 | 100.44 | 144.93 |
Table 8.
Reaction rate constants (kp) determined for different temperatures.
Table 8.
Reaction rate constants (kp) determined for different temperatures.
Temperature (°C) | kp (min−1) |
---|
150 | 0.0138 |
160 | 0.0207 |
170 | 0.0362 |
180 | 0.0500 |
Table 9.
Three-dimensional printing parameters.
Table 9.
Three-dimensional printing parameters.
Quality |
Layer height (mm) | 0.04 |
Initial layer height (mm) | 0.32 |
Line width (mm) | 0.44 |
Top/bottom |
Top layers | 8 |
Bottom layers | 10 |
Top/bottom pattern | Lines |
Infill | |
Infill density (%) | 60 |
Infill pattern | Trihexagonal |
Connect infill lines | Yes |
Material | |
Printing temperature (°C) | 218 |
Initial layer printing temperature (°C) | 218 |
Build plate temperature (°C) | 60 |
Flow (%) | 100 |
Speed | |
Print speed (mm/s) | 60 |
Outer wall speed (mm/s) | 30 |
Inner wall speed (mm/s) | 30 |
Travel speed (mm/s) | 150 |
Initial layer speed (mm/s) | 20 |
Retraction | |
Retraction distance (mm) | 1 |
Retraction speed (mm/s) | 40 |
Z-hop height (mm) | 0.08 |
Cooling | |
Fan speed (%) | 100 |
Regular fan speed at height (mm) | 0.4 |
Table 10.
Data for the calculation of scaffold porosity.
Table 10.
Data for the calculation of scaffold porosity.
| S-01 | S-02 | S-03 |
---|
Dry scaffold mass (g) | 0.506 | 0.516 | 0.498 |
Saturated scaffold mass (g) | 0.800 | 0.820 | 0.790 |
Pore volume (cm3) | 0.294 | 0.303 | 0.292 |
Apparent volume (cm3) | 0.413 | 0.422 | 0.407 |
Porosity (%) | 71.2 | 72.0 | 71.7 |
Average porosity (%) | 71.6 |
Table 11.
Mechanical properties of the printed scaffolds.
Table 11.
Mechanical properties of the printed scaffolds.
| Area (mm2) | Thickness (mm) | Maximum Force (kN) | Maximum Stress (MPa) | Nominal Strain at Fmax (mm) | Nominal Strain at Fmax (%) | Elastic Modulus (MPa) |
---|
S01 | 591.8 | 2.20 | 2.50 | 4.23 | 0.324 | 14.7 | 45.7 |
S02 | 590.5 | 2.20 | 2.50 | 4.24 | 0.331 | 15.0 | 51.7 |
S03 | 594.4 | 2.20 | 2.50 | 4.21 | 0.393 | 17.9 | 43.4 |
Average | 4.23 | 0.349 | 15.9 | 46.9 |
Table 12.
Contact angles of the scaffolds.
Table 12.
Contact angles of the scaffolds.
Sample | Position 1 | Position 2 | Position 3 | Average | Standard Deviation |
---|
S01 | 88.7° | 86.4° | 91.7° | 88.93° | 2.66° |
S02 | 86.5° | 79.2° | 86.0° | 83.90° | 4.08° |
S03 | 82.2° | 86.5° | 86.5° | 85.07° | 2.48° |
Total average | 85.97° | 3.56° |