DESIGN, ASSEMBLY AND CHARACTERIZATION OF COMPOSITE ...

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e) Figure 3.11 a) Non-space filling frame lattice printed with BT and carbon black inks; b) BT structure after burnout of carbonaceous content; c) sintered BT structures positioned against each other; d) a sintered non-space filling frame HA lattice, and e) a periodic BT structure after burnout of carbonaceous content. Three important features of the carbon black ink can be stated from observation of these results. First, the carbon black ink prints easily alongside the ceramic inks and acts as a sufficient support material in the wet printing state. Second, co-drying of the ceramic and carbon black inks did not cause cracking of the main structure; an indication that drying shrinkage is comparable in each. Third, the burnout stage did not cause cracking or destruction of the ceramic structure and resulted in good shape retention of the ceramic structure. This compatibility of carbon black ink with these ceramic inks suggests that it may also be used as fugitive support material for other ceramic compositions. 110
3.4 Conclusion A fugitive support material for Robocasting process was successfully developed using carbon black and polymer additives to form a non-ionic gel network in an aqueous medium. A type of carbon black powder Monarch 120A58 is first dispersed in water with the use of nonylphenol ethoxylate surfactant, and then gelled through interactions with non-ionic polymer additives Pluronic F-127 and Methocel F4M. The dispersion step requires a lower concentration of carbon black dispersion followed by concentration through a centrifugation process. Careful study of surfactant and polymeric additive effects on the rheology of carbon black suspensions resulted in colloidal gels with elastic and flow properties comparable to those observed in ceramic-based printing inks. The carbon black gel maintains its shape upon extrusion through the deposition nozzle, has negligible shrinkage after drying, and leaves only negligible ash content after burnout in air. The compatibility with BT and HA inks suggests that the carbon black ink may be compatible with other ceramic compositions. For ceramics, burnout in an oxidizing atmosphere is acceptable and one may expect that the carbon black will be removed by about 650 o C. For materials such as metals that require a non-oxidizing atmosphere, removal of the carbon black support material could be achieved; however, its feasibility depends on material chemistries and process variables involved. The development of this support material is expected to benefit the practitioners of aqueous colloidal gel solid freeform fabrication processes by allowing for a wider range of shapes to be printed, including those with large spans and cantilevered elements. 111
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DESIGN, ASSEMBLY AND CHARACTERIZATI
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ACKNOWLEDGEMENTS First and foremost
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CHAPTER 5 BARIUM TITANATE NICKEL CO
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Table 6.1 Formulations of aqueous c
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Figure 2.12 Schematic illustrations
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Figure 2.35 Schematic of the SHS pr
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Figure 4.9 Sintered nickel lattices
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Figure 6.12 Optical image of the cr
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1.1. Motivation CHAPTER 1 INTRODUCT
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and characterizing rheological prop
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2.1. Materials System CHAPTER 2 BAC
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2.2. Reentrant Structures and Ceram
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devices would provide self-sustaini
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a) b) Figure 2.4 Schematic illustra
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production of concept models, injec
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Fused Deposition Modeling (FDM) was
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Laser Engineered Net Shaping (LENS)
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Inkjet printing (IP) 27 is based on
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Table 2.1 Comparisons of various SF
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Figure 2.11 Processing steps involv
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2.4.1 Colloidal Inks The printing i
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Robocasting has lacked a well-desig
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Table 2.2 Example polymers that dep
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2.6. Sintering In robocasting, sint
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Figure 2.15 Sphere and plate model
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where
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2.5.3 Solid State Sintering In this
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Figure 2.18 Illustration of neck gr
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2.5.3.4 Final Stage During this sta
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Figure 2.23 Schematic diagram of th
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2.5.4.2 Rearrangement With the form
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2.5.4.6 Spreading of Sintering Aid
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Driven by reduction of free energy,
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2.5.5 Sintering Atmosphere Sinterin
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2.7. Composite Materials In this re
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Figure 2.29 Types of composite mate
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Table 2.6 Examples of composite mat
Page 75 and 76: Table 2.7 Examples of FGM applicati
Page 77 and 78: 2.7.3 Processing For the fabricatio
Page 79 and 80: prepared discrete layers of uniform
Page 81 and 82: Powder densification processes gene
Page 83 and 84: The specific volume fraction beyond
Page 85 and 86: a) b) Figure 2.34 a) Volume fractio
Page 87 and 88: When the powders are densified in s
Page 89 and 90: Various FGM coating processes are a
Page 91 and 92: of FGMs, such as partially reactive
Page 93 and 94: leading to a characteristic time τ
Page 95 and 96: 3.1 Introduction CHAPTER 3 AQUEOUS
Page 97 and 98: occurs in a multi-step process: fir
Page 99 and 100: a) b) Figure 3.1 a) SEM image of as
Page 101 and 102: 3.2.3 Preparation of Carbon Black C
Page 103 and 104: 3.2.5 Drying Shrinkage Characteriza
Page 105 and 106: the optimized surfactant concentrat
Page 107 and 108: The storage modulus of a colloidal
Page 109 and 110: For HA ink, yield stress
Page 111 and 112: In the case of the aqueous carbon b
Page 113 and 114: PPO units of Pluronic F-127 may ads
Page 115 and 116: a) b) Figure 3.6 A carbon black lat
Page 117 and 118: a) b) Figure 3.7 SEM images of a) c
Page 119 and 120: TGA plot is in agreement with previ
Page 121 and 122: a) b) Figure 3.9 Thermogravimetric
Page 123 and 124: 3.3.8 Fabrication of Complex Cerami
Page 125: c) d) 109
Page 129 and 130: metal inks have been reported for R
Page 131 and 132: Midland, MI) 5% by weight stock sol
Page 133 and 134: 4.2.5. Thermal Degradation of Binde
Page 135 and 136: 4.3. Results and Discussion 4.3.1.
Page 137 and 138: 4.3.2. Preparation of Nickel Ink Su
Page 139 and 140: 260 °C for 8 hours, the residual c
Page 141 and 142: Table 4.1 Calculated residual carbo
Page 143 and 144: a) b) Figure 4.6 Sintered Ni struct
Page 145 and 146: temperature 138, 139 lead to 92-95%
Page 147 and 148: Figure 4.8 Scanning electron microg
Page 149 and 150: c) Figure 4.9 Sintered nickel latti
Page 151 and 152: 5.1. Introduction CHAPTER 5 BARIUM
Page 153 and 154: materials within the overall struct
Page 155 and 156: 40:60, 60:40, 80:20 are separately
Page 157 and 158: 5.2.3. Rheological Characterization
Page 159 and 160: 5.2.5. Co-sintering and Re-oxidatio
Page 161 and 162: mixing, BT and Ni phases appear uni
Page 163 and 164: The combined use of PAA and PAA-90K
Page 165 and 166: To quantify this difference in sint
Page 167 and 168: As the BT and Ni particles used in
Page 169 and 170: The reducing atmosphere used in the
Page 171 and 172: Figure 5.7 Vickers hardness number
Page 173 and 174: 5.3.6. Fabrication of BT-Ni composi
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a) b) Figure 5.10 Co-sintered compo
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5.4. Conclusions Freeform fabricati
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Liquid phase sintering involves usi
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(pH=4.4, 31.5% by weight) (Adva Flo
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concentration of 7 mg/mL in the aqu
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Table 6.1 Formulations of aqueous c
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thickness. Each layer of the struct
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6.2.6. Hardness Test Microindentati
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micrographs for these two powders.
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Second, the added LiAC∙2H2O is am
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Figure 6.3 Oscillatory behavior for
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a) b) Figure 6.4 Sintering strain c
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mass transport in LFBT network. 167
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The above discussion is mainly focu
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Figure 6.8 shows the bowtie-shaped
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Figure 6.10 A NPR composite of para
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etween BT and Ni phases. But Zn ele
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Figure 6.13 Scanning electron micro
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Figure 6.15 shows the mapping of Ti
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Figure 6.17 and Figure 6.18 show el
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Figure 6.19 shows element mapping f
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6.3.7. Piezoelectricity and Dielect
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6.4. Conclusions Aqueous colloidal
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geometric features, including non-s
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3. Development of aqueous colloidal
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7.2. Recommendations In the context
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gelation behavior. κ-carrageenan i
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REFERENCES 1. Larsson 9301647, 1993
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29. Simchi, A.; Petzoldt, F.; Pohl,
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61. Bouvard, D., Acta Metallurgica
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92. Morissette, S. L.; Lewis, J. A.
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120. Boehm, H. P., Some Aspects of
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150. Atkinson, A., Growth of Nio an
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APPENDICES A. Mathematical Modeling
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and
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conditions: Equation A.12 is solved
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and with
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a) b) Figure B.1 a) Freeze-dried st
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a) Figure C.1 Cr-Ni lattices of 5Cr
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E. Binary Phase Diagram of ZnO-B2O3
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References A.1. Du, Z., Sarofim, A.
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Name: Jian Xu Date of Degree: May,
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