Advances in Bioceramics and Porous Ceramics · Apatite-Polyglutamic Acid Composites Prepared...

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Advances in Bioceramics and Porous Ceramics A CoNection of Papers Presented at the 32nd International Conference on Advanced Ceramics and Composites January 27-February I, 2008 Daytona Beach, Florida Editors Roger Narayan Paolo Colombo Volume Editors Tatsuki Ohji Andrew Wereszczak A John Wiley & Sons, Inc., Publication

Transcript of Advances in Bioceramics and Porous Ceramics · Apatite-Polyglutamic Acid Composites Prepared...

  • Advances in Bioceramics and Porous Ceramics

    A CoNection of Papers Presented at the 32nd International Conference on Advanced

    Ceramics and Composites January 27-February I , 2008

    Daytona Beach, Florida

    Editors Roger Narayan Paolo Colombo

    Volume Editors Tatsuki Ohji

    Andrew Wereszczak

    A John Wiley & Sons, Inc., Publication

    dcd-wgc1.jpg

  • This Page Intentionally Left Blank

  • Advances in Bioceramics and Porous Ceramics

  • This Page Intentionally Left Blank

  • Advances in Bioceramics and Porous Ceramics

    A CoNection of Papers Presented at the 32nd International Conference on Advanced

    Ceramics and Composites January 27-February I , 2008

    Daytona Beach, Florida

    Editors Roger Narayan Paolo Colombo

    Volume Editors Tatsuki Ohji

    Andrew Wereszczak

    A John Wiley & Sons, Inc., Publication

  • Copyright 0 2009 by The American Ceramic Society. All rights reserved

    Published by John Wiley & Sons, Inc., Hoboken, New Jersey. Published simultaneously in Canada.

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  • Contents

    Preface

    Introduction

    BIOCERAMICS

    Thermal Interface Stresses Including 3D Microstructures in Layered Free-Form Ceramics

    Hrishikesh Bale, Jay C. Hanan, and James E. Smay

    Preparation and Biomineralization of Silica-Based Organic-Inorganic Hybrid Hollow Nanoparticles for Bone Tissue Generation

    Song Chen, Akiyoshi Osaka, Kanji Tsuru, and Satoshi Hayakawa

    Effect of Wollastonite on the In Vitro Bioactivity and Mechanical Properties of PMMA Bone Cements

    Dora A. Cortes, David Renteria, M. Isabel Villarreal, Sergio Escobedo, J.M. Alrnanza, and Jose C. Escobedo

    Titanium Surface Modification to Titania Nanotube for Next Generation Orthopedic Applications

    Kakoli Das, Susmita Bose, and Amit Bandyopadhyay

    Calcium Phosphate Nanocarrier in BSA Delivery Sudip Dasgupta, Amit Bandyopadhyay and Susmita Bose

    Machinable Tricalcium Phosphate/Lanthanum Phosphate Composites

    Celaletdin Ergun

    Location of Carbonate Ions in Structure of Biological Apatite Michael E. Fleet and Xi Liu

    ix

    xi

    3

    19

    27

    37

    43

    53

    63

    V

  • Nanoindentation of Yttria Doped Zirconia Under Hydrothermal 77 Degradation

    Y. Gaillard, E. Jirnenez-Pique, J. A. Muiioz, J. Valle, and M. Anglada

    Influence of Sintering Conditions on the Microstructure of Chemically Precipitated Hydroxyapatite Nanopowder

    93

    Hoda Arnani Harnedani, Hiva Baradari, Sara Karimi, Harnidreza Rezaie, and Jafar Javadpour

    Hydrothermal Treatment of Alpha Tricalcium Phosphate Porous Ceramics in Various Aqueous Solutions

    103

    Masanobu Karnitakahara, Koji loku, Giichiro Kawachi, and Chikara Ohtsuki

    Electrochemical Deposition of Hydroxyapatite on Titanium Substrates in Metastable Calcium Phosphate Solution under Pulse Current

    M. Kawashita, T. Hayakawa, and G.H. Takaoka

    Hydroxyapatite/GEMOSIL Nanocomposite Ching-Chang KO, Tzy-Jiun Mark Luo, Lu Chi, and Alice Ma

    113

    123

    Challenge Toward Microstructure Optimization of Irregular Porous Materials by Three-Dimentional Porous Structure Simulator

    135

    Michihisa Koyarna, Hiroshi Fukunaga, Kei Ogiya, Tatsuya Hattori, Ai Suzuki, Riadh Sahnoun, Hideyuki Tsuboi, Nozornu Hatakeyarna, Akira Endou, Hirornitsu Takaba, Carlos A. Del Carpio, Rarnesh C. Deka, Mornoji Kubo, and Akira Miyamoto

    Synthesis of Rhenanite (p-NaCaP0,)-Apatitic Calcium Phosphate Biphasics for Skeletal Repair

    151

    R.M. Knotts, S. Jalota, S.B. Bhaduri, and A.C. Tas

    Nanomaterials as Improved Implants: A Review of Recent Studies 165 Huinan Liu and Thomas J. Webster

    Apatite-Polyglutamic Acid Composites Prepared Through Biomimetic Process

    181

    Toshiki Miyazaki, Atsushi Sugino, and Chikara Ohtsuki

    Formation of Bone-Like Apatite on Tricalcium Phosphate Ceramics in a Solution Mimicking Body Fluid

    Chikara Ohtsuki, Kohei Yarnaguchi, Tornohiro Uchino, Giichiro Kawachi, Koichi Kikuta, and Masanobu Karnitakahara

    189

    Ultraviolet Irradiation Had Limited Effects on Enhancing In Vitro Apatite Formation on Sol-Gel Derived Titania Films

    Akiyoshi Osaka, Tetsuya Shozui, Kanji Tsuru, and Satoshi Hayakawa

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    vi . Advances in Biocerarnics and Porous Ceramics

  • Nanostructured Bioactive Glass Scaffolds for Bone Repair Mohamed N. Rahaman, Delbert E. Day, Roger F. Brown, Qiang Fu, and Steven B. Jung

    Development of Novel Biocompatible Hydroxyapatite Coated Nanotubular Titania for Implant Application

    K. S. Raja, G.L. Craviso, M. Misra, A.M. Raichur, and A. Kar

    Low Temperature Degradation and Biomedical Properties of Y-TZP Ceramics

    Yumi Tanaka, Nami Ukai, Keishi Nishio, and Kimihiro Yamashita

    Nanoscale Hydroxyapatite for Bioceramic Applications Tien B. Tran, Joanna R. Groza, and James F. Shackelford

    Rheology and Properties of Bioactive Orthopedic Cement Noah Wiese, Stanley D. Wagner, and Thomas D. McGee

    POROUS CERAMICS

    Cellular Ceramics Made of Silicon Carbide Ceramics for Burner Technology

    J. Adler, G. Standke, M. Jahn, and F. Marschallek

    A Modified Gelcasting Procedure to Prepare Alumina Porous Components: Process Optimization and Preliminary Mechanical Tests

    Mariangela Lombardi, Laura Montanaro, Laurent Gremillard, and J e r h e Chevalier

    Experimental Investigation of the Oxidation Behavior of SiSiC Foams

    F.R.A. Mach, F.V. Issendorff, A. Delgado

    New Technology with Porous Materials: Progress in the Development of the Diesel Vehicle Business

    Kazushige Ohno

    Porous Alumina and Zirconia Bodies Obtained by a Novel Gel Casting Process

    Jean-Marc Tulliani, Valentina Naglieri, Mariangela Lombardi, and Laura Montanaro

    R-Curve Behavior in Porous Cordierite Honeycombs James E. Webb and Sujanto Widjaja

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    227

    239

    249

    259

    271

    287

    299

    31 3

    327

    339

    Advances in Bioceramics and Porous Ceramics . vii

  • Fabrication of Porous Silicon Nitride Ceramics with Gradient Microstructure

    Xiaowei Yin, Xiangming Li, Litong Zhang, Laifei Cheng, Yongsheng Liu, and Tianhao Pan

    Author Index

    349

    359

    viii . Advances in Bioceramics and Porous Ceramics

  • Preface

    This issue contains the proceedings of the “Porous Ceramics: Novel Developments and Applications” and “Next Generation Bioceramics” symposia, which were held on January 27-February 1, 2008 at the Hilton Daytona Beach Hotel in Daytona Beach, FL, USA.

    The interaction between ceramic materials and living organisms is emerging as a new frontier in materials research. Novel techniques for processing ceramic materi- als are being developed that will provide improvements in the diagnosis and treat- ment of medical conditions. This symposium allowed for discussion among the many groups involved in the development and use of bioceramics, including ceram- ic researchers, medical device manufacturers, and clinicians. This symposium ad- dressed several leading areas in the use of bioceramics, including rapid prototyping of bioceramics; advanced processing of bioceramics; biomimetic ceramics and bio- mineralization; in vitro and in vivo characterization of bioceramics; nanostructured bioceramics; and porous bioceramics (joint with the Porous Ceramics: Novel De- velopments and Applications symposium)

    Porous ceramics components are an essential part of numerous components in various enabling engineering applications. This symposium brought together engi- neers and scientists in the area of ceramics with porosity ranging from nano- to mil- li-meters (thus including foams, honeycombs, 3D scaffolds, interconnected fibers, sintered hollow spheres, meso-porous materials and aerogels). The basic aspects of processing, characterization, modeling, properties evaluation and applications of these materials, including processing methods for porous ceramics, structure and properties of porous ceramics, mesoporous ceramics, applications of porous ceram- ics, filtration and purification with porous ceramics, lightweight structural compos- ites with a porous matrix, gas-solid electrodes from porous ceramics, porous ceram- ics for hydrogen and energy-related applications, and porous bioceramics, were addressed.

    We would like to thank the staff of The American Ceramic Society for making this proceedings volume possible. We also give thanks to the authors, participants,

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  • and reviewers of the proceedings issue. We hope that this issue becomes a signifi- cant resource in the area of porous ceramics and bioceramics research that not only contributes to the overall advancement of this field but also signifies the growing role of The American Ceramic Society in these rapidly developing areas.

    Paolo Colombo Universita di Padova, Italy

    Roger Jagdish Narayan University of North Carolina and North Carolina State University

    x . Advances in Bioceramics and Porous Ceramics

  • Introduction

    Organized by the Engineering Ceramics Division (ECD) in conjunction with the Basic Science Division (BSD) of The American Ceramic Society (ACerS), the 32nd International Conference on Advanced Ceramics and Composites (ICACC) was held on January 27 to February 1, 2008, in Daytona Beach, Florida. 2008 was the second year that the meeting venue changed from Cocoa Beach, where ICACC was originated in January 1977 and was fostered to establish a meeting that is today the most preeminent international conference on advanced ceramics and composites

    The 32nd ICACC hosted 1,247 attendees from 40 countries and 724 presenta- tions on topics ranging from ceramic nanomaterials to structural reliability of ce- ramic components, demonstrating the linkage between materials science develop- ments at the atomic level and macro level structural applications. The conference was organized into the following symposia and focused sessions:

    Symposium 1

    Symposium 2

    Symposium 3

    Symposium 4 Symposium 5 Symposium 6

    Symposium 7

    Symposium 8

    Symposium 9

    Mechanical Behavior and Structural Design of Monolithic and Composite Ceramics Advanced Ceramic Coatings for structural, Environmental, and Functional Applications 5th International Symposium on Solid Oxide Fuel Cells (SOFC): Materials, Science, and Technology Ceramic Armor Next Generation Bioceramics 2nd International Symposium on Thermoelectric Materials for Power Conversion Applications 2nd International Symposium on Nanostructured Materials and Nanotechnology: Development and Applications Advanced Processing & Manufacturing Technologies for Structural & Multifunctional Materials and Systems (APMT): An International Symposium in Honor of Prof. Yoshinari Miyamoto Porous Ceramics: Novel Developments and Applications

    xi

  • Symposium 10 Symposium 1 1

    Focused Session 1 Geopolymers Focused Session 2

    Basic Science of Multifunctional Ceramics Science of Ceramic Interfaces: An International Symposium Memorializing Dr. Rowland M. Cannon

    Materials for Solid State Lighting

    Peer reviewed papers were divided into nine issues of the 2008 Ceramic Engi- neering & Science Proceedings (CESP); Volume 29, Issues 2-10, as outlined be- low:

    Mechanical Properties and Processing of Ceramic Binary, Ternary and Com- posite Systems, Vol. 29, Is 2 (includes papers from symposium 1) Corrosion, Wear, Fatigue, and Reliability of Ceramics, Vol. 29, Is 3 (includes papers from symposium 1) Advanced Ceramic Coatings and Interfaces 111, Vol. 29, Is 4 (includes papers from symposium 2) Advances in Solid Oxide Fuel Cells IV, Vol. 29, Is 5 (includes papers from symposium 3) Advances in Ceramic Armor IV, Vol. 29, Is 6 (includes papers from sympo- sium 4) Advances in Bioceramics and Porous Ceramics, Vol. 29, Is 7 (includes papers from symposia 5 and 9) Nanostructured Materials and Nanotechnology 11, Vol. 29, Is 8 (includes pa- pers from symposium 7) Advanced Processing and Manufacturing Technologies for Structural and Multifunctional Materials 11, Vol. 29, Is 9 (includes papers from symposium 8) Developments in Strategic Materials, Vol. 29, Is 10 (includes papers from symposia 6, 10, and 1 1, and focused sessions 1 and 2)

    The organization of the Daytona Beach meeting and the publication of these pro- ceedings were possible thanks to the professional staff of ACerS and the tireless dedication of many ECD and BSD members. We would especially like to express our sincere thanks to the symposia organizers, session chairs, presenters and confer- ence attendees, for their efforts and enthusiastic participation in the vibrant and cut- ting-edge conference.

    ACerS and the ECD invite you to attend the 33rd International Conference on Advanced Ceramics and Composites (http://www.ceramics.org/daytona2009) Janu- ary 18-23,2009 in Daytona Beach, Florida.

    TATSUKI OHJI and ANDREW A. WERESZCZAK, Volume Editors July 2008

    xii . Advances in Bioceramics and Porous Ceramics

  • Bioceramics

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  • THERMAL INTERFACE STRESSES INCLUDING 3D MICROSTRUCTURES IN LAYERED FREE-FORM CERAMICS

    Hrishikesh Bale: Jay C. Hanan," James E. Smayh 'Mechanical and Aerospace Engineering. hChemical Engineering: Oklahoma State University, Stillwater. OK, USA

    ABSTRACT Processing of complex ceramic parts such as a dental restorations involves sintering of ceramic

    performs. Intended and unintended microstructures such as voids, cracks and, interfaces exist in these parts. These microstructures contribute to the mechanical response and ultimate life. A combined X- ray computed micro-tomography and X-ray micro-diffraction experiment was implemented on an alumina-zirconia layered free-form fabricated composite. The composite serves as a model for examining the mechanics and material characteristics of ceramic dental restorations. The current in- situ X-ray technique is capable of determining the strain values at prescribed spatial locations on the micron scale using high-energy synchrotron radiation and refractive focusing optics.

    In coordination with the experimental work, a finite element analysis of the volume generated by micro-tomography was developed. This required implementing a non-trivial procedure of converting the tomograph into a 3D finite element model. Simulation of sintering on this real geometry is compared with the experimental strain results for validation of the model. Once validated, the simulation offers more detailed insight to mechanical properties than experimental measurements offer on their own. This comprehensive procedure of modeling and experimentation including microtomography combined with diffraction offers a powerful method to quantify damage evolution and strain in ceramic layered composites-first intended for dental applications. yet broadly applicable as structural materials.

    INTRODUCTION Two of the ceramics commonly used for dental restorations are alumina and zirconia.

    Typically they are used independently, but their common sintering temperatures allow combination as laminates or as mixtures. Considerations for choosing these ceramics include fracture toughness, strength, cost. and their aesthetically pleasing color resembling natural teeth. In general, these high- performance ceramics are used as structural members in crowns or bridges and are overlaid with porcelain giving translucence, final color. and texture to the restoration. While they may be sintered together, alumina and zirconia have different mechanical properties such as their elastic moduli and thermal expansion coefficients. These differences in properties provide a source for residual stresses when the two materials are sintered as mixtures or laminates. They superimpose over applied stresses and can accelerate or retard cracking and failure. Under the prolonged or cyclic influence of loads, small cracks grow into larger cracks which are detrimental to the life of the part.' This is a serious problem for all bio-material applications whether considering dental restorations or implants and joint replacement prosthesis. Alternatively. the interface layer where the residual stresses exist can be tailored as a low fracture energy region to deflect cracks and induce toughening mechanisms.2 Determination of the residual stresses in such composites and laminates has been a challenging problem. The situation becomes more complicated when intricate geometries are involved, for instance a dental crown.

    While experiments providing bulk properties have been extensive, there is a lack of such understanding with composites. This is further complicated by the contribution of micro-scale features such as stress concentrators like pores and facets. Visualization of these defect zones in 3D is possible

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  • Thermal Interface Stresses Including 3D Microstructures in Layered Free-Form Ceramics

    using X-ray micro-tomography (p-CT). Experiments using CT to visualize microstructure and monitor the evolution of the structure have been carried '," Such experiments are able to probe in-situ material characteristics and monitor the gradual developments in phase change. pore distribution and. fluid uptake. In addition, efforts to analyze quantitatively properties such as elastic modulus, fiacture toughness, and the nature of stresses using X-ray diffraction measurenients are o n g ~ i n g . * ~ ~ ~ ' ~ * " Both these methods, X-ray micro-diffraction and X-ray micro-tomography, when combined together provide valuable information pertaining to the microstructure and material properties. Some of the preliminary work on the combined experimentation has produced results which evaluate strains from positions which can be tracked by tomography.12 This gives comprehensive 3D information including spatial coordinates where the particular material property is evaluated.

    Pin-pointing stress to a specific location within a 3D volume is important and has been ~hallenging.'~ Finite element simulations are generally utilized in such scenarios, where a model is generated as close as reasonable to the actual geometry. Many times this leads to approximations from the actual result. However, finite element simulations are advantageous since results from any location throughout the sample volume can be observed. The present work refers to an experimental and computational evaluation of alumina-zirconia composites and aims to validate a finite element model which was modeled with actual $ample dimensions using tomography as input for comtructing the mesh. A comparison of the experimental results and simulations will confirm the effectiveness of both the experimental technique and the simulations.

    METHOD Sample Preparation

    The experiment consists of sintered samples produced using a novel solid free form fabrication technique called Robo-casting to assemble layers of alumina and zirconia. Freeform fabrication involves printing colloidal inks of the two ceramics using fine printing tips or nozzles. The 3-D tool path print design is fed to a computer numeric control system to obtain the desired geometry. Following earlier work," the starting inks consisted of alumina. A1103 ( aA1?()3= 5.5 pmini-"C at 25 "C, 10.1 pdm-"C at 1127 "C )Is and Yttria stabilized tetrayonal Zircoina, ZrO2 (CTE,azlo2=10.9 at 25 T)". Mixtures of the two inks can also be printed. The colloid volume fraction in the inks was &(>I(& = 0.47 for A1203 and ZrOz. The green bodies were first bisque fired at 1IOO"C then sintered at 1150 "C.

    Figure I Schematic ofrobocasting used to fabricate the layered composites. 3-D printing is performed with ink nozzles. One nozzle dedicated to an alumina ink and the other to zirconia. (see also ').

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  • Thermal Interface Stresses Including 3D Microstructures in Layered Free-Form Ceramics

    Combined In-Sitic X-Ray Micro-Diffraction and Micro Computed Tomography The Advanced Photon Source X-ray synchrotron facility at Argonne National Laboratory.

    Chicago was utilized to conduct the X-ray diffraction and imaging experiments on the abocementioned samples. The beamline ID-2-BM m-as modified so both high-resolution tomography and micro diffraction could be conducted in-situ on the composite. The diffraction CCD (Charged Coupled Device), the tomography camera and the sample stage straddles a plane including the X-ray beam. The diffraction CCD is oriented at a 28 angle of 30" to the beam. The camera used for tomography is mounted with a scintillator plate that fluoresces X-rays as visible light. A high-precision translation stage was used to position the sample with respect to the X-ray beam.

    Micro-diffraction is sensitive to lattice distortion. such as those which are majorly present in the vicinity of the interface. Due to this sensitibity it has the ability to measure the residual strain in the interface zone formed between the alumina and zirconia phase. This micro-residual strain is an indication of the advantage in using a mixture for the second phase. Since the two phases do not mix, some accommodation of each of the constituents properties, such as CTE, results. The residual strain at the interface is identified from line scans which observe the strain at points following the path of the line across the interface. These diffraction measurements are based on elastic displacements of atoms, d, from their equilibrium strain free lattice positions. d(,. according to Brag ' s law. At room temperature ceramics deform elastically. Ad = d - do. rather than with elastic and plastic flow commonly observed in metals. Diffraction directly observes the total strain, E = Ad / do, in these materials up until failure. In addition. diffraction measurements average over the diffracting grains in an irradiated volume. For materials such as dental ceramics. the grain size (less than I pni) is small relative to the beam allowing micro-diffraction measurements to be representative of an isotropic continuum rather than being heavily intluenced by individual grains whose grain-to-grain stress'' may significantly deviate from the local average.

    Figure 2 Left schematic of tlie diffractometer stage. It and tlie labeled photograph (right) show tlie arrangement o f the diffraction and toniograpliy canieras niounted with relation to the incident beam.

    Sample alignment and stability is very important since micro-diffraction measurements are sensitive to sample displacement. The error in the measured inter-planar spacing as a result of displacement 6 is given by the following equetion."

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    where, 8 i s the Bragg angle, R is the Radius of the goniometer. For example, a sample displacement of 100 Fm along the beam (as shown in Figure 3) causes an error of 1 0 0 ~ 1 0 ~ in 820. assuming a 100 mm goniometer radius and a 28 of 30'. This is equivalent to a 20 MPa error in alumina stress. Thus from the equation it is evident that displacement errors can be large.

    Figure 3 Schematic of displacement error caused when sample is moved with respect to the beam. Reproducibility of the translation stage and alignment of the sample when moving, such as for line scans or do measurements depend on this error being small.

    To avoid translation errors in tl-spacing. the composite sample and its two strain-free references. one for each layer type. were positioned in-line and checked with 90" in plane. 4, rotations to verify alignment. In addition the translations were checked by live radiographs. Periodic recordings of the beam spot and monitoring of the system alignment were documented. To within the resolution ofthe measurements. translation errors of the entire system were maintained below 10 pm with typical errors for any one exposure much less than 1 pm.

    The composite and strain-free reference samples were mounted together and sample switching was done with the use of lateral translation. Monitoring the d-spacing of the strain free references allows corrections for d-spacing changes in the ceramic which are not due to layering in the composite. For example. Yttria stabilization in zirconia or low concentration contaminates in the alumina powder. Keeping these references in the same environment as the composite ensures even the sanie thermal conditions are maintained for the references. All processing and experimental conditions were maintained identically for these specimens.

    Experimental geometry The diffraction exposures were recorded onto a diffraction CCD (QUANTIX 6303e). oriented

    at an angle of 8 to the incident beam. Since only a small arc (1.2' of the entire diffraction cone) is recorded, only one component of the strain tensor is observed. Precision in 8 is paramount. A compromise is required such that the brightest peaks are captured in order to have higher strain accuracies, yet the peaks are clearly resolved to a resolution within i0.0001" @(which corresponds to a strain of 10x106). A careful choice of the diffraction cone area is made with considerations of low background and interference from other diffracting phases, within the limitations of shadowing from goniometer components 'and other hardware.

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    2.0

    E E

    1.5 .-

    0 5 10 15 20 25 X-ray energy keV

    Figure 4 Plot of X-ray attenuation as a function of Energy." The inset shows a typical radiograph and illustrates the difference in X-ray attenuation for the two phases at 21 keV.

    It is important to note that the diffracted intensity recorded on the CCD is the result of diffraction from many grains in the sample that lie along the beam path. High-energy synchrotron X- rays, 21 keV. were obtained using the double crystal nionocluoniater. Figure 4 shows the level of attenuation oftlie beam, caused by alumina and zirconia. With an absorption edge at 18 keV. zirconia absorbs most of the beam. The diffraction signal obtained in the zirconia region is limited to the surface. For transmission, the signal is less than 1"/0 in the zirconia region as is evident from the intensity plot and the tomographic section shown i i i Figure 5 .

    Figure 5 Bi-layer ceramic with alumina on top and zirconia at the bottom (lett), Toinographed w h i n e showiiig detailed features ii i the cross section

    For micro-diffraction. the X-ray beam is focused through a series of compound refractive lenses to a diameter of 14 pm x 7 p i as measured by a radiograph.'" The lenses were placed several

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  • Thermal Interface Stresses Including 3D Microstructures in Layered Free-Form Ceramics

    meters upstream of the center of diffraction. To switch between micro-diffraction and imaging, the compound refractive lenses were translated out of the beam path. This allows the parallel beam through for imaging. Further ad,justment of the imaging beam was done with slits. The tomographs were taken with this larger parallel beam which can be adjusted from 2 to 4 mm across.

    Diffraction exposures were obtained for each scan point along the dashed line shown in Figure 5. A Lorentzian profile algorithm was used to fit the peaks obtained by binning and integrating the rings. The residual strains were calculated by comparing these peak positions with the value obtained from the strain-tiee references. The two alumina peaks namely (3 0 0), (2 1 4) which have the strongest signal are used for the strain calculation. Figure 6 shows an example of the CCD exposure giving sections of the rings. The CCD was corrected for distortion by calibrating with a CeOz standard powder. For the plot on the right. a series of integrated patterns of ceramic peaks show the change in composition proportional to the change in peak areas as the line sc'an progresses from the alumina phase to the zirconia phase.

    High resolution tomographs consist of a sequence of radiographs taken for 0.25'$ steps of the sample about its central axis. The 3D reconstructions were analyzed with various slice orientations (AMIRA 3.1.1 a 3D visualization software). Features like cracks, pores. discontinuities and different phases were observed. The entire tomograph consists of 1024 slices. the total assemblage of all the slices requires 4Gb of memory. Each slice includes 1024 x 1024 pixels. The images were converted to %bit TIFF format suitably rescaling the intensity ranges to maintain the contrast between the alumina phase. zirconia phase, the pores, and the crack.

    Figure 6 Indexed alumina peaks in the alumina phase. The image on the left is from a scan point close to the interface. hence the ZrO2 peaks are visible. The plot on the right shows peak profiles approaching the interface.

    Tomography to Finite Element Model An important aim of this experiment was to determine the ability to generate a computational

    model of the complex geometry of the freeform fabricated sample and simulate the sintering process that results in residual stresses and cracking. Reconstructed data obtained from tomography was digitilly visualized in 3D. The different phases can be distinctly seen by the contrast. The material coordinates were registered into a model including the material properties before submitting to finite element analysis. The process of differentiating the constituent phases of the tomography is called segmentation. Segmentation involves a detailed procedure of image processing to reduce noise. and enhance key features like voids, pores. and cracks. Followed by the initial image processing. each

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    slice was recast. using a threshold to extract basic features on a broader scale. Some low contrast features such as. interface delineations between two phases (as seen in Figure 5 ) were difficult to segment using the automatic tools. and were selected manually.

    Figure 7 Segmentatioii of the sample volume based on contrast and threshold intensity. Bottom figures show orthogonal slices moving from the zirconia to the alumina region. Features in the alumina region are clearly seen compared to the zirconia region due to high transmission in the alumina region

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    Sequence d segmentation and conversiar 40 FE input model.

    Figure 8 Example images representing steps showing implementation of segmentation. surface, and Lolume meshing for input to finite element modeling.

    The volume is segmented by labeling phases according to the material density. The volume was reconstructed from a subset of 800 slices out of a total of 1024 orthogonal slices. Each slice was segmented based on intensity threshold and contrast. Some example frames are described in Figure 7. Following segmentation, a surface mesh is generated on the material boundaries. The surface mesh creates a well defined closed boundary for the entire sample volume including pores. This is an important step since quality of the surface mesh dictates the quality of the volume mesh generated in the succeeding step. Surface mesh generation is done in steps of gradually decreasing surface elements. The primary goal is to reduce the total surface elements while maintaining the surface geometry. Reduced facets leads to fewer volumetric tetrahedrons generated which reduces demand on computational resources. For example, 1021692 tetrahedrons were employed in our calculations. Reduction from 1,739,702 facets to 50,000 facets was typical. After a successful surface mesh is generated. the marching algorithm*" fills the volume with tetrahedral of nodal properties corresponding to the material it contains.

    FE Analysis After the volumetric tetrahedral mesh was generated (Amira) the model was exported for post-

    processing (Hypermesh v7) where mesh validation and refinement operations were done and finally converted to an input format for Finite Element Modeling (FEM), (Abaqus v6.6). The input file has details of nodal properties. interface contact nodes, and spatial information. Figure 9 shows a comparison of the radiograph of the composite and the finite element mesh generated from the tomograph. The region where the diffraction line scan was recorded is depicted. Model orientation with respect to the co-ordinate system was established before the nodal path was assigned. The orientation with reference to the beam was digitally fixed by hand using visual feedback comparing the

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  • Thermal Interface Stresses Including 3D Microstructures in Layered Free-Form Ceramics

    oriented mesh with the radiograph. As seen in the Figure 8. a sniall error in the rotational orientation is possible. Howeber. this has minimal impact on the results Since the sample is generally axially sqninietric. Automating this step could iinpro\e the alignment.

    Figure 9 A Comparison of the real sample and the real fuiite rlenient geometry generated to model residual stress. Left top: Radiograph indicates the position of the X-ray exposures on the sample with respect to the niicrobearn. Left, bottom: Side view of tetra mesh for FEM. This orientation was used to simulate the strains observed by diffraction. Right: Top view of tetra mesh. This orientation more clearly shows the path of the X-ray beam iised for strain measurements.

    The FEM code’s primarq purpose Has to conduct the simulation of thermal residual stesses in the composites. The thermal residual stress was simulated in a static general step with 10 incremental steps. The temperature dependant theimal coefficient of expansion for alumina and zirconia is utilized for this analysisf5. For comparison, an ideal cylindrical Bi-laler composite was also modeled. Material properties corresponding to alumina and alumina-zirconia were initialized at the nodes using region partitioning. The temperature step was applied by defining an initial. 1000°C, and final. 25°C. temperature field around the sample. Aberage computation time for the complex tomography model and the ideal cylinder model are 12 hours and I hour respectitely on an Intel Pentium-4 3.2GHz. machine.

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    RESULTS The residual strains in the alumina region are compressive as compared to the zirconia region.

    For the lane parallel to the interface, the X-ray integrated residual strain reaches a maximum of -275 1 0 at the interface. Far from the interface, the residual strain relaxes to the strain-free value. The strain falls to half its maximum, 100 pm froin the interface. Figure 10 plots these strains as a function o f distance from the interface. A radiograph showing the path of the X-ray line scan is also shown. The figure shows registration of the strain data on the corresponding radiograph. The position accuracy is maintained by tracking the coordinates of the micro-beam spot and overlapping the two frames.

    f!

    0 . - Tonwaiaphy m e 1 PiediCLkx

    -&- Slrpla Cylinder model predlcmn I -

    -1 -0.8 -0.6 0 .4 0 . 2 0 0.2

    Figure 10 Top: A plot o f strains from an X-ray line scan across the interface in the zirconia and aluniina layered sample. The plot also consists of the predicted values obtained from FE simulations (ideal cylinder and the real geometry). The measured strains approach zero close to a crack visible in the associated radiograph (bottom). The crack initiates from a notch as a stress concentrator and travels into the alumina phase, terminating within the interior.

    The residual strains also relax near the crack visible in the radiograph. This crack can be clearly observed in Figure 5 which shows an orthogonal section taken from the tomograph. A crack typical for this sample type was observed. The crack originates from the periphery at a region of stress concentration within the alumina layer and then proceeds away from the interface at an angle of about 30". The crack appears in the segmentation process as a low absorption gas phase. This crack region was manually filled-in, with the surrounding material properties in the segmentation module for FE

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    models. Utilizing both the radiograph and the beam-spot position. the line scan region in the FE simulation is also matched to extract results from the same region as done experimentally-an advantage provided by tomography.

    Residual strajn results for the simple cylinder caw are shoun in Figure I I . A maximum compressive strain integrated along a path simulating the X-ray beam reached -320 x 10' at the interface. The strains along the beam path have been integrated to determine a strain value o fa volume comparable to that observed with X-ray diffraction. The contour plot obtained from FEM is overlapped with the paths at which the nodal information was gathered. Determining coordinates for a desired node is easy for the simple cylinder case. but becomes challenging for the more complex freefonn geometry. To avoid complexities in detennining the coordinates of the line scan. a path was defined along a scan point which collects nodal as well as eleniental intersection values along the path. The scan path consists of nodes along a predefined path and hence only a point region. Whereas in the case of the X-ray diffraction measurement averaging of strains takes place at discrete diffracting grains along a beam path over a volume which contains the area of the beam (14 pin x 7 pm) .

    Figure 11 Contour plot showing a section of the ideal cclinder FE simulation of the alumina-zirconia bi-lager composite. The cross-section corresponds to the line scan showing the region through which the strains were integrated. The strains were integrated along the marked paths (white).

    Results of the simulation on the tornograph) based model are shown in Figure 12. A direct comparison between the ideal and the real geometry shows that the real geometry takes into account the voids present as processing defects along with the complex external geometry. I t is observed that the integrated maximum compressive residual strain at the interface region is -24G x l o 6 . which is loner (almost 20%) than the ideal model case.

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    Figure 12 Contour plot showing FE simulation of the alumina-zirconia bilayer composite model based on the real geometry provided from tomography. With the cutaway view, the internal voids and pores in the alumina region are clearly visible.

    DISCUSSION Significant CTE mismatch between the two pure alumina and zirconia layers exists (azd,2=10.9

    at 25°C and C~ZIZO?= S.Symlm-"C at 2S°C, 10.1 pm/m-"C at 1127°C ),Is which often results in cracking due to residual stresses. A combined tomography and diffraction measurement leads to precise registration of the scan points on the sample. which pinpoints the location of the measured strains in the context of the local microstructure. At this scale with the presence of defects, accurate registration of the mapped area becomes increasingly critical compared to volumetric measurements or bulk average measurements. It is seen in Figure 6. that as the sample was scanned in the diffraction mode. along line scans running from the alumina region to the zirconia region. the intensities of the zirconia peaks increase5 and that of alumina decreases gradually. This gradual change is influenced by the integration of the intensities coming from all the grains along a beam path through the sample. Especially at the interface. since the interface is not a flat planar geometry, the beam goes through both the alumina and zirconia grains. However. this X-ray integration of strains across microstructural features is an important aspect regarding interpretation of the residual stress state ofthe composite.

    Without considering the FEM model, the experiments clearly reveal compressive residual stresses exist parallel to the interface in the alumina region and tensile residual stress exist on the zirconia-alumina side of the interface. The highest strain value obtained from the X-ray diffraction mas nearly 300 x 106 at the interface. The compressive strains persist up to 0.2 mm away from the

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    interface. Where the crack is present. as seen in the radiograph. the strain value was observed to relax. As expected, this relaxation contrasts to the finite element model. 'The crack was closed for the model to avoid a singularity in the solution and its inability to model large scale deformation as in case of a crack. Crack initiation might be inferred from the stress values in the model which are greater than the yield stress.

    An important result of this experiment and the corresponding finite element model is the evaluation of strain values obtained through the integrated grain volume. Since the experiment involves the transmission geometry. diffraction patterns consist of intensities from many grains. Hence, results represent average strain values from many grains in the beam path for a particular scan point, and not from a particular grain. The residual strain values from the experiment were closer to the simulation values for the real geometry simulation than the ideal cylinder case. This is due to the fact that the real geometry simulation not only accounts for the surface morphology. but also takes into account the voids and interface shape. unlike the ideal cylinder. This validation of the finite element niodel suggests that the model can be used to generate values for the zirconia region which otherwise are difficult to probe with X-rays due to strong absorption.

    Conversion of the real geometly to the finite element model through tomography was successfully implemented. The original resolution of the images acquired is far higher than that used in the finite element model. This leads to elimination of voids smaller than 10 microns. Use of higher memory and computational power would overcome this limitation.

    CONCLUSION A comprehensive and effective experimental and computational procedure capable o f

    determining computing thermal residual strains Corresponding to pores and phase boundaries such as the layered interface was developed. The computational model generated for an ideal case and a real geometry were validated through experimental results. Generation of the 3D model involved large data volumes. This volume must be carefully reduced without compromising the tine details affecting an analysis. Both the experimental and computational techniques, evaluated a maxinium compressive residual strain in the plane of the interface close to 2 7 5 ~ 1 0 ~ due to the coefficient of thermal expansion mismatch. This compressive stress remained up to 0.2 mm into the Alumina layer falling off to the far-field strain-free value. possibly prematurely due to a crack. Since the morphology is complex. these experimental results are aided by comparison with simulations. The validated simulations for the ceramic composite predict principle stresses in excess of 300 MPa at the interface region.

    It was shown from simulations that including the real sample geometry was significant in understanding the characteristics of the interface and residual strain state around it. The strain results calculated for an ideal cylinder were nearly 20% greater than the results for the real geometry. The real geometry includes features such as the interface shape. external geometry. and interior voids. The standard deviation of the strains evaluated by micro-diffraction is nearly 10x1 0.6 for the alumina region. The zirconia layer, where strain evaluation using X-rays is more difficult. can be simulated with additional confidence due to the validated model.

    ACKNOWLEDGMENTS The authors are grateful to Diane Rekow and Van Thompson at the NYU Dental College for

    their guidance and support. In addition. James Smay at Oklahoma State University provided the samples used in this study. A poition of this work was supported by a grant from the National Institutes of Health (NIH-NIDCR. POI-10976). Yong Chu and Francesco De Carlo provided valuable assistance related to use of the Adkanced Photon source. Use of the Advanced Photon Source was

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  • Thermal Interface Stresses Including 3D Microstructures in Layered Free-Form Ceramics

    supported by the U. S. Department of Energy. Office of Science, Office of Basic Energy Sciences, under Contract No. W-31-109-ENG-38. The authors also acknowledge a portion of the research results discussed in this publication were made possible by the OHRS award for project number HR07- 134, from the Oklahoma Center for the Advancement of Science and Technology.

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