Overview
ABSTRACT
Ceramic matrix composites (CMCs) are made of long silicon carbide or carbon fibres embedded in a ceramic matrix. They were developed for extreme operating environments: high temperatures, oxidising atmospheres, under mechanical stress or under irradiation. Though composed of brittle ceramic materials, the composite is tough, and so can be used in aircraft, spacecraft or nuclear applications. This article describes the main components of the composite and the associated fabrication processes. Their mechanical and thermal behaviours, and the influence of oxidative atmospheres or irradiation are described. Examples of CMC parts are lastly shown.
Read this article from a comprehensive knowledge base, updated and supplemented with articles reviewed by scientific committees.
Read the articleAUTHORS
-
Gérald CAMUS: CNRS Researcher, Thermostructural Composites Laboratory (LCTS), Pessac, France
-
Christophe LORRETTE: Research Engineer, CEA, Director of Nuclear Energy, Saclay, France
-
René PAILLER: CNRS Research Engineer, LCTS, Pessac, France
-
Francis REBILLAT: Professor, University of Bordeaux, LCTS, Pessac, France
-
Bernard REIGNIER: Herakles research engineer, SAFRAN Group, LCTS, Pessac, France
-
Francis TEYSSANDIER: CNRS Researcher, LCTS, Pessac, France
INTRODUCTION
Ceramic materials are hard but brittle. A great deal of work has been devoted to improving the toughness of ceramics, notably by dispersing particles or short fibers in the ceramic to deflect cracks or split them. It is also possible to produce tough ceramic materials by manufacturing composite materials with a ceramic matrix (CMC) and long fibers. The reinforcement provided by these fibers ensures the material's mechanical properties, while the ceramic matrix protects them from the environment. The various CMCs are designated by two headings separated by a slash (C/C, C/SiC, SiC/SiC...), the first designating the fiber material/the second that of the matrix. When the matrix includes additional phases, the main component of the matrix is mentioned.
These composites, which are mainly used in applications involving extreme conditions, are known as "thermostructural", meaning that they can be used as structural materials at high temperatures, and must therefore retain their mechanical properties under operating conditions. They are currently used mainly in the aerospace and nuclear industries. Depending on the application, they are subjected to operating temperatures ranging from 400 to over 2,000°C in oxidizing atmospheres (air, reactor combustion gases, etc.). They can be subjected to stresses ranging from simple vibrations to multiaxial stresses. Finally, in the nuclear field, they can be subjected to irradiation. The fibers, which are essentially made of carbon, silicon carbide or oxides (alumina, basalt, mullite), bear most of the applied load. They must therefore have the highest possible breaking strength and elastic modulus, combined with good fatigue resistance and low density (for aerospace applications). Depending on the type of application, they must also have good resistance to oxidation, creep and critical cracking (propagation of a crack, usually by corrosion, for applied stress intensity factors lower than the macroscopic stresses that trigger damage), high thermal conductivity and be compatible with the interphase or matrix, during processing or use. They can be woven, braided or assembled in the form of semi-finished products (felts, unidirectional webs, etc.), which constitute a preform for the final part. This preform is densified by a ceramic matrix, making the part dense and protecting the fibers from environmental aggression. Unlike conventional composites (organic or metal matrix CMO or CMM), in CMC the modulus of elasticity of the matrix is greater than or equal to that of the fiber, and the strain at break of the matrix is less than the strain at break of the fiber.
Ceramic materials are brittle, however, and a third component is introduced into these composites to "defragilize" them. This is a thin, easily-cleavable interphase between the...
Exclusive to subscribers. 97% yet to be discovered!
You do not have access to this resource.
Click here to request your free trial access!
Already subscribed? Log in!
The Ultimate Scientific and Technical Reference
KEYWORDS
aeronautics | composites | spatial | ceramic materials | Chemical Vapor Infiltration
This article is included in
Glasses and ceramics
This offer includes:
Knowledge Base
Updated and enriched with articles validated by our scientific committees
Services
A set of exclusive tools to complement the resources
Practical Path
Operational and didactic, to guarantee the acquisition of transversal skills
Doc & Quiz
Interactive articles with quizzes, for constructive reading
Long fiber-reinforced ceramic matrix composites
Bibliography
Websites
Thermostructural Composites Laboratory http://www.lcts.u-bordeaux1.fr/
Thermostructural composites: exceptional materials http://www.herakles.com/innovation/composites-thermosructuraux/? lang=fr
...Events
HTCMC, International Conference on High Temperature Ceramic Matrix Composites http://ceramics.org/meetings/9th-international-conference-on-high- temperature-ceramic-matrix-composites-and-global-forum-on-...
Standards and norms
- Test method for tensible stress-strain behaviour of continuous fibre reinforced composites at room temperature - ISO 15733 - 2014
- Mechanical properties of ceramic composites at high temperature – Determination of compression properties - ISO 14544 - 2012
- Ceramic composites – Thermophysical properties: Determination of thermal diffusivity (Based on EN 1159-3:2003) - ISO 19629 - 2013
- Advanced technical...
Patents
HERAUD (L.), COTTERET (J.), BONNET (C.), CHRISTIN (F.), NASLAIN (R.), HAGENMULLER (P.), Porous carbonaceous part densified in situ by chemical vapor deposition of refractory materials other than carbon, and method of manufacture, Patent FR2401888A1 (March 30, 1979).
MAISTRE (M.), Nouvelle structure composite, et procédé et matrice destinés à la fabrication d'une telle structure, Patent FR2498733A1 (July...
Exclusive to subscribers. 97% yet to be discovered!
You do not have access to this resource.
Click here to request your free trial access!
Already subscribed? Log in!
The Ultimate Scientific and Technical Reference