Français
3. Protection against damage during use
Resistance to oxidation and the stability and maintenance of mechanical properties at temperature are critical for CMC applications in the aerospace sector . In some applications, temperatures can reach up to 1,600°C, in air or under the high pressure of gas mixtures containing oxidizing species. The use of materials capable of raising the operating temperatures of aircraft engine parts such as turbine blades would eliminate the need for cooling, improve engine efficiency and reduce fuel consumption and NOx emissions . The service life of CMCs for these...
The Ultimate Scientific and Technical Reference
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
Protection against damage during use
Applications
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...
The Ultimate Scientific and Technical Reference
