Carbon-carbon composite is emerged as a strong aircraft brake (rotator and stator) material due to its low density, excellent thermal and mechanical properties, self lubricating and low wear capability. Compared to conventional steel/ceramet brakes, carbon-carbon composites apparently performed better in weight saving and brake life. The carbon-carbon composites currently used as aircraft brake discs are either polyacrylonitrile (PAN)/chemical vapour infiltrated (CVI) or pitch/resin/CVI-based composites. Recently, the friction and wear performance of a series of two-dimensional PAN/pitch composites has been evaluated under low and medium-energy conditions. The preliminary results indicated that the PAN/pitch composite might also be promising for use as brake material. However, friction and wear behaviour of carbon-carbon brake disc depends upon many parameters, such as fibre and matrix types, fibre angles, load, speed, temperature and humidity.
Wear behaviour of C/C-SiC composites
Verschleißverhalten von C/C-SiC-Verbundstoffen
Tribology 2000 - Plus, International Colloquium, 12 ; 3 ; 1671-1674
2000
4 Seiten, 5 Bilder, 7 Quellen
Aufsatz (Konferenz)
Englisch
Study of Wear Behaviour of POM/Graphite and POM/MoS2 Composites
SAE Technical Papers | 2017
|Wear behaviour of plastics on plastics
Kraftfahrwesen | 1981
|Wear of Tire Tread/Carcass Composites
SAE Technical Papers | 1995
|The effect of reinforcement volume fraction and size on the wear behaviour of Al-matrix composites
British Library Conference Proceedings | 1992
|