CERAMIC COMPOSITE MATERIAL Russian patent published in 2014 - IPC C04B35/565 

Abstract RU 2530802 C1

FIELD: machine building.

SUBSTANCE: invention can be used at manufacturing of parts and units of uncooled structures in aircraft gas turbine engines of new generation with improved characteristics of specific power and fuel efficiency which are operated under the temperatures of up to 1750°C in oxidizing media environment. Ceramic composite material contains silicon, carbon, silicon carbide and oxide system ZrO2-HfO2-Y2O3 with the following ratio of components, wt %: Si - 15-30; C - 20-40; oxide system ZrO2-HfO2-Y2O3 - 3-15; SiC - the rest. The oxide system ZrO2-HfO2-Y2O3 is of the following chemical composition, wt %: ZrO2 - 55-80; HfO2 - 15-30; Y2O3 - 3-15.

EFFECT: increased heat resistance of items.

2 tbl

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RU 2 530 802 C1

Authors

Vaganova Marija Leonidovna

Grashchenkov Denis Vjacheslavovich

Ermakova Galina Vladimirovna

Solntsev Sergej Stanislavovich

Dates

2014-10-10Published

2013-10-03Filed