FIELD: chemistry.
SUBSTANCE: invention relates to glass-ceramic composite materials based on nanostructured glass-ceramic matrices which are reinforced with carbon filler, for making annular elements and components for future aerospace equipment with working temperature of up to 1300°C, used in oxidative and other aggressive media and working under heavy mechanical loads. The material can be used in ground-based, power generating, oil and gas pumping and transportation systems an in new fields of general and special machine building. The invention discloses glass-ceramic composite material which contains a glass matrix and carbon fibre filler in the following ratio, wt %: glass matrix 55.5-75.5, carbon fibre filler 24.5-44.5. The glass matrix is crystallised in high-temperature phase of cordierite and has the following chemical composition, wt %: Al2O3 33-38, MgO 11-15, SiO2 - the rest.
EFFECT: high impact viscosity and fire resistance of the glass-ceramic composite material at working temperatures of up to 1300°C.
4 ex, 2 tbl
| Title | Year | Author | Number | 
|---|---|---|---|
| CERAMIC COMPOSITE MATERIAL | 2007 | 
 | RU2359927C1 | 
| COMPOSITE MATERIAL AND DEVICE MADE FROM THIS MATERIAL | 2006 | 
 | RU2310628C1 | 
| CERAMIC COMPOSITE MATERIAL | 2008 | 
 | RU2388727C1 | 
| COMPOSITE MATERIAL AND THE ITEM MADE OUT OF IT | 2004 | 
 | RU2273617C1 | 
| COMPOSITE MATERIAL | 2003 | 
 | RU2257362C1 | 
| CERAMIC COMPOSITE MATERIAL | 2006 | 
 | RU2347771C2 | 
| COMPOSITE | 2001 | 
 | RU2193539C2 | 
| CERAMIC COMPOSITE MATERIAL | 2009 | 
 | RU2392250C1 | 
| CERAMIC COMPOSITE MATERIAL | 2010 | 
 | RU2447039C1 | 
| CERAMIC COMPOSITE MATERIAL | 2009 | 
 | RU2397969C1 | 
Authors
Dates
2011-02-20—Published
2009-04-29—Filed