| Literature DB >> 28772411 |
Xiang-Yu Zhang1, Gang Fang2,3, Jie Zhou4.
Abstract
Additive manufacturing (AM), nowadays commonly known as 3D printing, is a revolutionary materials processing technology, particularly suitable for the production of low-volume parts with high shape complexities and often with multiple functions. As such, it holds great promise for the fabrication of patient-specific implants. In recent years, remarkable progress has been made in implementing AM in the bio-fabrication field. This paper presents an overview on the state-of-the-art AM technology for bone tissue engineering (BTE) scaffolds, with a particular focus on the AM scaffolds made of metallic biomaterials. It starts with a brief description of architecture design strategies to meet the biological and mechanical property requirements of scaffolds. Then, it summarizes the working principles, advantages and limitations of each of AM methods suitable for creating porous structures and manufacturing scaffolds from powdered materials. It elaborates on the finite-element (FE) analysis applied to predict the mechanical behavior of AM scaffolds, as well as the effect of the architectural design of porous structure on its mechanical properties. The review ends up with the authors' view on the current challenges and further research directions.Entities:
Keywords: additive manufacturing; biomaterial; finite element modeling; geometric design; mechanical property; scaffold
Year: 2017 PMID: 28772411 PMCID: PMC5344607 DOI: 10.3390/ma10010050
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Figure 1Procedure of design, fabrication and evaluation of BTE scaffolds. μCT, micro-computed tomography.
Additive manufacturing (AM) technologies, their features and applications.
| Method | Process Characteristics | Applicable Metallic Materials for Bone Tissue Engineering | Advantages (+) and Disadvantages (−) | Category | Manufacturer |
|---|---|---|---|---|---|
| Powder bed and inkjet 3D printing (3DP) [ | Depositing binder on metal powder Curing the binder to hold the powder together Sintering or consolidating the bound powder Infiltrating with a second metal (optionally) | Stainless steel, iron, cobalt-chromium alloy, zirconium, tungsten, etc. | Ability to create shapes that are difficult or impossible for traditional methods (+) No need for potentially extensive laser optimization experimentation (+) No heat source is used during the processing (+) No need for a build plate (+) Need post-processing (−) Considerable porosity exists (−) Not available for part reparation (−) | Binder jetting | ExOne, 3D System |
| Selective laser sintering (SLS) [ | Preparing the powder bed Layer by layer addition of powder Sintering each layer according to the CAD file, using laser source | Stainless steel, cobalt-chromium alloy, titanium, etc. |
No need for support (+) No post-processing is needed (+) Need heat treatment and material infiltration (−) Porous part and rough surface (−) Thermal distortion (−) Not available for part reparation (−) | Powder bed fusion | EOS |
| Selective laser melting (SLM) [ |
Thin layers (20–100 μm) of atomized fine metal powder are evenly distributed using a coating mechanism onto a substrate plate, usually metal Each 2D slice of the part geometry is fused by selectively melting the powder The process is repeated layer after layer until the part is complete | Stainless steel, iron based alloys, titanium, gold, silver, etc. |
Capable of fully melting the powder material, producing fully dense near net-shape components without the need for post-processing (+) High processing precision (≤10 μm) (+) Support needed where necessary (−) High quality demands for metal powders and limited part size (−) Distortion caused by residual thermal stress (−) Not available for part reparation (−) | Powder bed fusion | SLM Solutions |
| Electron beam melting (EBM) [ | The EBM machine reads data from a 3D CAD model and lays down successive layers of powder These layers are melted, utilizing a computer controlled electron beam under vacuum | Titanium alloys, cobalt chromium alloy | Kinetic energy transfer and preheating the powder result in lower thermal stresses (+) Vacuum environment; metal does not oxidize easily (+) No support needed (+) Complex internal cavities not possible due to preheating/sintering process (−) Rougher texture and less precise than laser beam manufacturing (−) | Powder bed fusion | Arcam |
| Direct metal laser sintering (DMLS) [ | Spreading a very thin layer of metal powder across the surface that is to be printed Laser slowly and steadily moves across the surface to sinter powder Additional layers of powder are then applied and sintered | Stainless steel, titanium, etc. | Parts free from residual stresses and internal defects (+) Expensive; limited its use to high-end applications (−) Not suitable for low ductility materials (−) Heating stage needed for low ductility materials (−) | Powder bed fusion | Stratasys |
| Direct metal deposition (DMD) [ | Powder is melted using laser or other kind of energy at the nozzle and then deposited layer by layer | Iron, titanium, etc. | Part size is not limited to bed size; large metal parts (+) No limitation in processing space (+) Available for part reparation (+) Poor surface finish (−) | Direct energy deposition | Optomec, TWI |
| Electron beam additive manufacturing (EBAM) [ | Convert CAD model to CNC code Electron beam gun deposits metal, via a powder or wire feedstock, layer by layer, until the part reaches the near-net shape Finish heat treatment and machining | Titanium, stainless steels, zinc alloy, tantalum, tungsten, etc. | Part size is not limited to bed size; large metal parts (+) Good material utilization (+) Multiple wire feed nozzles can be utilized with a single EB gun (+) Lower processing accuracy than powder bed AM and poor surface finish (−) | Direct energy deposition | Sciaky, Efesto |
Qualitative comparison between different AM processes.
| AM Process | Resolution | Build Speed | Surface Roughness | Power Efficiency | Build Volume | Residual Stress | Cost |
|---|---|---|---|---|---|---|---|
| 3DP | Poor | Fast | Poor | - | Big | Low | Low |
| SLS | Good | Slow | Excellent | Poor | Small | High | High |
| SLM | Good | Slow | Excellent | Poor | Small | High | High |
| EBM | Moderate | Fast | Good | Good | Small | Moderate | High |
| DMLS | Good | Slow | Excellent | Poor | Small | Low | High |
| DMD | Poor | Fast | Poor | Poor | Big | High | Moderate |
| EBAM | Moderate | Moderate | Good | Good | Small | Moderate | High |
Figure 2Scaffold designs based on different types of unit cells.
Figure 3Failure mechanisms of (a) the diamond lattice structure at a 22% volume fraction; continuous shearing band of 45°, owing to crushing diagonal layers, is observed. Shearing of layers is accompanied by the bending failure of tying struts perpendicular to the diagonal plates; and (b) the cubic lattice structure; layer-by-layer deformation mechanism is confirmed by stretch-dominated deformation in scaling law analysis [98].
Figure 4Distribution of the strut diameter of the 17 sections for the biomechanically optimized scaffolds with diagonal design (a); results in terms of strut diameter (b); and pore size (c) of each section for all the three investigated scaffold designs [100].
Figure 5Patterns of bony tissue (3D view and frontal view) predicted by the optimization algorithm in the case of (A) square pores, under a pressure of 1 MPa and with a scaffold Young’s modulus of 1000 MPa; and (B) circular pores, under a pressure of 1 MPa and with a scaffold Young’s modulus of 1000 MPa; (C) a detailed view of the pattern of bony tissue predicted to form in an elliptic pore. The gray elements represent the volume within the scaffold where bone formation is predicted to occur [101].
Figure 6Compressive stress-strain curves of the specimens based on the cube unit cell and with porosity of (a) 88%; (b)78%; (c) 74%; (d) 66% [39].
Figure 7Comparison between the mechanical properties of different types of porous structures based on the six different unit cells: (a) elastic gradient; (b) first maximum stress; (c) plateau stress; (d) yield stress; (e) energy absorption. In these figures, the exponents of the power law fitted to the experimental data points, but not the experimental data points themselves, are compared with each other [39].
Mechanical properties of scaffolds made of different types of unit cells.
| Unit Cell | Material | Pore Size (μm) | Strut Diameter (μm) | Porosity (%) | Young’s Modulus (GPa) | Yield Stress (MPa) | References | |||
|---|---|---|---|---|---|---|---|---|---|---|
| Nominal | Measured | Nominal | Measured | Nominal | Measured | |||||
| Cube | Ti-6Al-4V | 348~720 | 451~823 | 1452~1080 | 1413~1020 | 65~90 | 63~87 | 1.76~4.62 | 29~110 | [ |
| Ti-6Al-4V | 550, 800 | - | 300, 400 | - | 70.3~70.7 | 70.2~68.7 | 5.10~6.70 | 155~164 (UCS) | [ | |
| Ti-6Al-4V | 1000~2040 | 765~1020 | 450, 800 | 466~941 | 60.91~75.83 | 49.75~59.32 | 0.57~2.92 | 7.28~163.02 | [ | |
| Diamond | Ti-6Al-4V | 277~600 | 240~564 | 923~600 | 958~641 | 89~63 | 89~64 | 0.39~3.30 | 7~70 | [ |
| Ti-6Al-4V | - | 670~1820 | - | 420~540 | - | 87~60 | 0.4~6.5 | 11.4~99.7 | [ | |
| Truncated cube | Ti-6Al-4V | 1720~1370 | 1625~1426 | 180~530 | 331~620 | 94~76 | 91~80 | 0.99~3.19 | 10~40 | [ |
| Truncated cuboctahedron | Ti-6Al-4V | 876~807 | 862~1049 | 324~564 | 862~1049 | 82~64 | 81~64 | 2.37~4.62 | 25~100 | [ |
| Rhombic dodecahedron | Ti-6Al-4V | 1250~950 | 1299~1058 | 250~550 | 246~506 | 90~66 | 89~68 | 0.22~2.97 | 7~88 | [ |
| Ti-6Al-4V | - | - | - | 67~129 | - | 84~67 | 0.55 | - | [ | |
| Rhombicuboctahedron | Ti-6Al-4V | 820~670 | 877~794 | 380~530 | 348~438 | 84~64 | 89~68 | 2.23~4.40 | 39~93 | [ |
| Dodecahedron | Ti-6Al-4V | ~ | 150 | ~ | 500 | - | 80 | 1.22 | 12.7 | [ |
| CP-Ti | 450, 500 | ~ | 120, 170, 230 | - | - | 66~82 | 0.58~2.61 | 8.6~36.5 | [ | |
| Ti6-Al-4V | 500, 450 | 560, 486 | 120, 170 | 140, 216 | - | 68~84 | 0.55~3.49 | 15.8~91.8 | [ | |
| Tetrahedron | Ti-6Al-4V | 500 | - | 0.2~0.39 | - | 50~75 | - | 4.3~1.9 | 57~156 | [ |
| Octet truss | Ti-6Al-4V | 770 | - | 0.2~0.4 | - | 50~75 | - | 4.6~1.2 | 34~172 | [ |
| Twist struts | Ti-6Al-4V | - | - | 0.90, 1.10 | - | 55~60 | 55~61 | 3.4~26.3 | 103~402 | [ |
| Gyriod TPMS | Ti-6Al-4V | - | 560~1600 | - | - | - | 80~95 | 0.13~1.25 | 6.50~81.30 | [ |
| Diamond TPMS | Ti-6Al-4V | - | 480~1450 | - | - | - | 80~95 | 0.12~1.25 | 4.66~69.21 | [ |