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1Subject: Composite Materials Science and Engineering Subject code: 0210080060 Prof C. H. XUSchool of Materials Science and EngineeringHenan University of Science and TechnologyChapter 8:Ceramic Matrix Composites (CMCs)
2Ceramic Matrix Composites (CMCs) This chapter will coverIntroduction to CMCsFabrication of CMCsReview of selected CMCsToughening mechanisms
3Introduction to Ceramic Matrix Composites (CMCs) Ceramics: high strength, stiffness, and brittleObjective for CMCs is to increase in the toughnessUse and fabricate CMCs at high temperatureLess reinforcements are availableSchematic force-displacement curves for a monolithic and CMCs, illustrating the greater energy of fracture of the CMCs
5Processing Ceramic Matrix Composites (CMCs) Conventional mixing and pressing(a) A powder of the matrix is mixed with reinforcement (particles or whiskers) together with a binder(b) Pressure(c) Fire or hot pressureDifficulty during fabricationDifficult to obtain uniform mixtureDamage to whiskers during mixing and pressing operations
6Processing Ceramic Matrix Composites (CMCs) Slurries (泥浆）Simplified flow sheet (流程图) for mixing (whiskers or chopped fibers) as a slurry prior to shapingThe properties of CMCs produced by slurries is not good because of more porosity in materials
7Processing Ceramic Matrix Composites (CMCs) Slurries: for continuous fibre reinforced composite1）Fibers (glass fibers), impregnated with slurry (powder glass (1-50mm) in water and water soluble resin binder), are wound on to a mandrel to form a tape.2) The tape is cut into pies.3) The types are stacked (lay-up).4) Burnout of the binder5) Heat pressuree.g. glass fiber reinforced glass-ceramic matrix)
8Processing Ceramic Matrix Composites (CMCs) Liquid State ProcessingMatrix transfer molding: glass matrix compositeproduction CMCs with tube shape1): SiC cloth (reinforcement) and glass slug (matrix) plunge in a cylinder2) Heat to melt glass, press liquid and inject in SiC cloth3) Eject the mandrel and cylindere.g. SiC reinforced glass-ceramic (polycrystalline structure) matrix
9Processing Ceramic Matrix Composites (CMCs) Sol-gel (溶胶-凝胶) processingsol: dispersion of small particles of less than 100 nm, obtained by precipitation (沉淀) resulting from a reaction solutionGel: sol lost some liquid to increase viscosityPour sol over perform (reinforcement)Mix sol or gel with reinforcementRepeat infiltration and dry until required densitydryDry solheat to produce required ceramicHot pressFireMixing reinforcement in a sol or a gelInfiltration of a preforme.g. ZrOCl2+NH3+3H2O=2NH4Cl+Zr(OH)4Zr(OH)4 → ZrO2 at 550℃
11Processing Ceramic Matrix Composites (CMCs) Lanxide processFormation of a ceramic matrix by the reaction between a molten metal and a gas (e.g. molten aluminum reacting with oxygen to form alumina)growth rate isparabolic when the diffusion of liquid metal controls the process.linear when chemical reaction at preform and infiltrated preform controls process; In this case, liquid metal diffuses rapidly by a wicking (灯芯的) process along grain boundaries in ceramic matrix when gsv> 2gsL.
12Review of selected CMCs - SiC reinforcement alumina Usually made by slurry method (SiC whisker and polycrystalline a-alumina)
13Review of selected CMCs - SiC reinforcement alumina left fig. showing: Improvement in toughness due to SiC whiskers in alumina matrix at various temperatureRight fig. showing: Log-log plot of strain rate versus stress showing that the creep rate at a given stress is less for the SiC reinforced alumina
14Review of selected CMCs - SiC reinforcement alumina SiC whisker reinforced alumina has good thermal shock (热冲击) resistance. The reasons arelowers the coefficient of thermal expansion;Increase the thermal conductivity;Improves the toughness;Thermal shock behaviors of an alumina-20vol%SiC whisker composite and alumina; cooling materials from high T to room T in water
15Review of selected CMCs - Zirconia-toughened alumina Zirconia, ZrO2, -toughened alumina (ZTA) contains reinforcement (10-20vol% of fine Zirconia) and matrix (alumina).ZrO2 Crystal:Tetragonal (T) at high temperatureMonoclinic (M) at low temperatureT→M transformation during cooling causes an increase in 3% volume, producing microcrack in Al2O3 matrix.Microcracks absorb energy to improve toughness of composite
16Review of selected CMCs - Zirconia-toughened alumina Add stabilizing oxide, such as 3mol.% Y2O3 to ZrO2 suppress t→m transformation during cooing.Fine metastable tetragonal-ZrO2 at room temperature in ZTAZrO2 particles at a crack tip will transfer to monoclinic-ZrO2 under stress, which is called as transformation toughing.
17Review of selected CMCs - Glass-ceramic matrix composites Glass-ceramics: some glass with crystal structureE.g. lithium aluminosilicate (LAS) systemWorking temperature:LAS-I 1000℃;LAS-II 1100℃;LAS-III 1200℃;
18Review of selected CMCs - Glass-ceramic matrix composites Young’s modulus of SiC-LAS composites is larger than monolithic LAS
19Review of selected CMCs - Glass-ceramic matrix composites Composites have higher strength than that of monolithic LASElastic deformation at beginning (linear curves)Matrix plastic deformation and reinforcement elastic deformation.Reinforcements break from point F
20Review of selected CMCs - Glass-SiC reinforcements Room temperature Toughness of LAS-SiC compositeVol% SiCK1C (MPam1/2)LAS1.5LSA-I50 (unidirectional)17LSA-II50 (Cross-plied)10
21Review of selected CMCs - Glass-SiC reinforcements The properties of composite maintained to 1000℃ in inert atmosphere.The properties of composite reduced from 800 ℃ in air. Oxygen diffuses along microcracks in the matrix and reacts with SiC.
22Unidirectional reinforcement -glass matrix composite has better fatigue properties Cross-plied reinforcement glass matrix composite has less fatigue properties.
23Review of selected CMCs - Carbon – Carbon Composites Dense carbon-carbon compositesContinuous fiber materialsthe good mechanical properties of the better quality of fiberProduce a materials with a desired degree of anisotropy (各向异性)Discontinuous fiber materialsBeing used to fabricate large componentsproduce isotropic materials and improve inter-laminar strengthApplications: disc brakes for racing car and aircraft, gas turbine components, nose cones and leading edges for missiles
25Dense carbon-carbon composites -Manufacture a reinforcement preform Continuous and discontinues carbon fibers, matReinforcement preform
26Dense carbon-carbon composites -Manufacture matrix Liquid phase processingRaw materials - thermosetting resins (phenolic, furan, polymide, polyenylene) :Impregnation （注入） thermosetting resins in a reinforcement preform~ Polymerize at 250℃ to form cross-link polymerPyrolysis （高温分解）and carbonization at 600~1000℃ to form amorphous, isotropic carbon (carbon yield about 45~80%)Raw materials - Pitch:Impregnation pitch in a reinforcement preformthermoplastic polymer in naturePyrolysis and carbonize at 600~1000℃ to form a highly orientated mesophase carbon; carbon yield about 50% under normal pressure and up to 90% under high pressureEach cycle needs about 3 days.multiple impregnation and carbonization to obtain high density;
27Dense carbon-carbon composites -Manufacture matrix Chemical vapor infiltration (CVI) , also called as chemical vapor deposition: thermal decomposition of hydrocarbon, such as methane CH4(g) = C(s) + 2H2(g) under suitable temperature and pressureLaminar aromatic (芬芳的)Layered pyrolitic carbonIsotropic sooty (乌黑的)surface nucleated dense pyrolitic graphitecontinuously nucleated graphite
28Dense carbon-carbon composites -Manufacture matrix Isothermal method:The infiltration (渗透): under low pressure of 0.6 ~ 6 MPa at a constant temperature of 1100℃.Problem: form an impermeable crust (外壳)The crust must be removed by a machine to remain continuous infiltration.Thermal gradient method:The infiltration carried out under atmosphere pressure at a inner temperature of 1100℃.The inner of sample was heated by induction coil.Pressure gradient method:Gas is forced into the interior of samples
29Dense carbon-carbon composites - graphitization and coating Graphitization: heat treatment at high temperature up to 1500~2800℃ to obtain graphite matrixcoatingIn order to Improve oxidation resistance of compositeA coating system capable of offering protection up to 1400℃ currently;Coating must be satisfyMechanically, chemically and thermally compatible with the compositeAdhere to the compositePrevent diffusion of oxygen from the environment through to the compositePrevent diffusion of carbon from the composite to the environmentComplex protective systemsLarge differences in the coefficient of thermal expansion (CTE) between coating layer and composite during cooling lead to cracking of coating and loss of oxidation protection.SiC and Si3N4 as primary oxidation barrier coat, based on CTE.Second protective system: add a glass former particles in to matrix to form glass phase or having an additional glass coating.
30Dense carbon-carbon composites - Properties The effects of different carbon matrix on the properties of C-C composite
31Dense carbon-carbon composites - Properties 1-D (one dimensional woven carbon fibre reinforced composite) is strong but brittle.2-D (two dimensional woven carbon fibre reinforced composite) has properties intermediate to those of the 1-D and 3-D3-D (three dimensional woven carbon fibre reinforced composite) has better toughness and less strengthThe low toughness of 1-D composite is attributed to the poor interlaminar propertiesSchematic stress-strain curves illustrating the effects of the form of reinforcement on strength and toughness
32Dense carbon-carbon composites - Properties Comparison of the fatigue performance of carbon fiber reinforced carbon composite and carbon fiber reinforced polymer composite: (a) torsion; (b) flexuralFatigue property of CFRC is similar to CFRP
33Dense carbon-carbon composites - Properties Specific strength versus temperature forACC: made using woven carbon cloth;RCC: produced from low modulus fiber;High strength C-C: made with unidirectional carbon fibers interplied with woven cloth
34Review of selected CMCs - Porous carbon – carbon Composites Porous carbon-carbon composites, also called as carbon bonded carbon fibres (CBCF)Processing:A mixture including carbon fiber, phenolic resin (binder), and water;The mixture pumped into a mould;Water extracted under vacuum and dryCarbonization at ~950℃, carbon yield about 50%,Graphite at high temperature to obtain 99.9% carbon.porosity contents are in the range 70-90%Application of CBCF as insulation at high temperature under vacuum (no oxygen) or at the temperature less than 400℃
35Review of selected CMCs - Porous carbon – carbon Composites Strength related to the densityThe properties are anisotropic.Fiber orientation takes place under vacuum during processingStrength of carbon bonded carbon fiber as a function of density and orientation. Z and X/Y denote the direction of the tensile stress in the bend test
36Toughening mechanisms - Introduction There are many different toughening mechanisms.One or more toughening mechanisms may operative in a composite.The effectiveness of the toughening mechanisms depends on:Size, morphology and volume fraction of the reinforcement;Interfacial bond;Properties (e. g. mechanical, thermal expansion) of the matrix and the reinforcement;Phase transformation……
37Toughening mechanisms - crack bowing (弓) (a) Crack approaches to reinforcements.(b) the crack bowed under stress to form a nonlinear crack front.Decrease in the stress intensity K along the bowed section in the matrixIncrease in the stress intensity K at the reinforcementK reached to the fracture toughness of the reinforcement → the reinforcement breaksBowing needs more energy to increase toughness
38Toughening mechanisms - crack bowing Crack bowing toughing ↑with ↑ the volume fraction of reinforcement (more reinforcements)with ↑ aspect ratio of the reinforcementwith ↑ the properties of reinforcement
39Toughening mechanisms - Crack deflection (偏斜, 偏转) Crack deflects and becomes non-planar, due to interaction between the reinforcement and crack front.(a) Tilt (倾斜)of crack front(b) Twist (扭) of crack frontThere are 3 crack modesFlat crack propagates in mode I.Tilt crack in modes I and IITwist crack in modes I and III
40Toughening mechanisms - Crack deflection Deflection occurs when the interaction of the crack with the residual stress fields due to differences in the thermal expansion coefficients or elastic moduli between the matrix and reinforcement.Deflection toughening ↑:with↑volume fraction of reinforcementWith ↑ aspect ratio of reinforcementDominated by twisting rather than tilting of the crack
41Toughening mechanisms - Debonding toughening Debonding: Reinforcement fibre separates from matrix.Debonding toughening: New surface in the composite require energy in debonding.Debonding toughening ↑Weak interface of matrix and reinforcementStrong reinforcementLarge volume fraction of reinforcement.
42Toughening mechanisms - Pull-out toughening Pull out a fibrePull-outDebondingFibre fracture for long fiberThe normal (法线）frictional forces have to be overcome during pull-out.The maximum pull-out length of a fibre is ½ the critical length (lc).If embedded length is greater than lc. fibre will break.
43Toughening mechanisms - Pull-out toughening Maximum work to pull out a fibre isWhere D, lc and sTf are diameter, critical length and fracture strength of the fibre, respectively.The energy of pull-out is greater than that of debonding.Pulling a fibre out of the matrix
44Toughening mechanisms - Fibre bridging toughening Fibre bridging: some fibres debonds but not break.Fibres carry out stresses under load.Reduce the stresses at crack tip and hinder crack propagation.Toughness-crack extension curve:Toughness increase with crack extension at initial crackingConstant toughness maintains when crack reaches to critical value.
45Toughening mechanisms - Microcrack toughening Thermal stress forms between matrix and reinforcement during cooling, due to difference in coefficient of thermal expansion (a).af>amTangential compressive and a radial tensile stresses in matrixCircumferential crack forms under high tensile stress.Tangential tensile stress in matrix cause radial crack under high tensile stress.Stress distribution and microcrack formation around spherical particles when (a) af>am, (b) af<am,C and T for compressiveand tensile stresses
46Toughening mechanisms - microcrack toughening The toughness of a materials can be enhanced by the presence of microcracks, due to crack blunting, branching and deflection.The microcrack toughening is effective on the limited density and size of cracks.Toughness of materials increases and strength decreases in the microcrack toughening.
47Toughening mechanisms - Transformation toughening Metastable tetragonal-ZrO2 at room temperature in ZTAtransformation toughing: ZrO2 particles at a crack tip will transfer to monoclinic-ZrO2 under stress. Energy is absorbed ahead of the primary crack owing to the transformation.Giving an increase in toughness△KTT = 0.3vzirc △eEmro1/2Where vzirc is the volume fraction of metastable particles; △e is unconstrained strain accompany the transformation; Em is young’s alumina matrix and ro is the width of zone in the crack.Strength and toughness of materials increase at same time.Transformation toughening: transformation of metastable particles at the crack tip gives a Zone, of width ro, of transformed particles
48Further Reading: Text Book: Reference book: Other reference: Composite Materials: Engineering and Science (pages , ).Reference book:Introduction to Materials (page )Other reference:Lecture note 8