A platform for research: civil engineering, architecture and urbanism
A platform for research: civil engineering, architecture and urbanism
Continuous fiber-reinforced zirconium carbide based composite material and preparation method thereof
The present invention relates to a continuous fiber-reinforced zirconium carbide based composite material and a preparation method thereof, and belongs to the technical field of high temperature thermal protection materials. According to the present invention, the prepared continuous fiber-reinforced zirconium carbide based composite material has excellent performances of lightweight, high performance resistance, anti-oxidation property and the like, the density is 1.9-2.2 g/cm<3>, the tensile strength is 96-150 MPa, the bending/compressive strength is 130-180 MPa, the mass loss under the 2000 DEG C aerobic environment only is 10<-4> g/cm<2>s magnitude, and the composite material shows the good comprehensive performance advantages, and can be applied in novel high hypersonic aircrafts, high-speed re-entry vehicles, reusable orbital maneuvering aircrafts, advanced power systems, and other high temperature thermal protection systems.
Continuous fiber-reinforced zirconium carbide based composite material and preparation method thereof
The present invention relates to a continuous fiber-reinforced zirconium carbide based composite material and a preparation method thereof, and belongs to the technical field of high temperature thermal protection materials. According to the present invention, the prepared continuous fiber-reinforced zirconium carbide based composite material has excellent performances of lightweight, high performance resistance, anti-oxidation property and the like, the density is 1.9-2.2 g/cm<3>, the tensile strength is 96-150 MPa, the bending/compressive strength is 130-180 MPa, the mass loss under the 2000 DEG C aerobic environment only is 10<-4> g/cm<2>s magnitude, and the composite material shows the good comprehensive performance advantages, and can be applied in novel high hypersonic aircrafts, high-speed re-entry vehicles, reusable orbital maneuvering aircrafts, advanced power systems, and other high temperature thermal protection systems.
Continuous fiber-reinforced zirconium carbide based composite material and preparation method thereof
FENG ZHIHAI (author) / XU LIN (author) / ZHANG YIN (author) / LI WEI (author) / SONG YONGZHONG (author) / CHENG JIA (author) / LI XINGCHAO (author) / FAN ZHEN (author)
2015-09-16
Patent
Electronic Resource
English
IPC:
C04B
Kalk
,
LIME
| European Patent Office | 2020
| European Patent Office | 2023
| European Patent Office | 2015
| European Patent Office | 2021