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