J. Mater. Sci. Technol. ›› 2019, Vol. 35 ›› Issue (12): 2743-2750.DOI: 10.1016/j.jmst.2019.07.020
• Orginal Article • Next Articles
Pengren Wang, Fengqi Liu, Hao Wang*(), Hao Li, Yanzi Gou*()
Received:
2019-01-26
Revised:
2019-03-17
Accepted:
2019-05-15
Online:
2019-12-05
Published:
2019-12-18
Contact:
Wang Hao,Gou Yanzi
Pengren Wang, Fengqi Liu, Hao Wang, Hao Li, Yanzi Gou. A review of third generation SiC fibers and SiCf/SiC composites[J]. J. Mater. Sci. Technol., 2019, 35(12): 2743-2750.
Trade mark | Tensile strength (GPa) | Young’s modulus (GPa) | Diameter (μm) | C/Si ratio | Oxygen content (wt%) |
---|---|---|---|---|---|
Hi-Nicalon S | 2.6 | 340 | 12.0 | 1.05 | <1.0 |
KD-S | 2.7 | 310 | 11.0 | 1.0˜1.1 | <1.0 |
Tyranno SA | 2.5 | 375 | 8.0&10.0 | 1.08 | <0.5 |
KD-SA | 2.5 | 380 | 10.5 | 1.05 | <0.5 |
Sylramic | 3.2 | 400 | 10.0 | 1.01 | 0.8 |
Sylramic-iBN | 3.5 | 400 | 10.0 | N/A | N/A |
Table 1 Properties of third generation SiC fibers [10,26,29].
Trade mark | Tensile strength (GPa) | Young’s modulus (GPa) | Diameter (μm) | C/Si ratio | Oxygen content (wt%) |
---|---|---|---|---|---|
Hi-Nicalon S | 2.6 | 340 | 12.0 | 1.05 | <1.0 |
KD-S | 2.7 | 310 | 11.0 | 1.0˜1.1 | <1.0 |
Tyranno SA | 2.5 | 375 | 8.0&10.0 | 1.08 | <0.5 |
KD-SA | 2.5 | 380 | 10.5 | 1.05 | <0.5 |
Sylramic | 3.2 | 400 | 10.0 | 1.01 | 0.8 |
Sylramic-iBN | 3.5 | 400 | 10.0 | N/A | N/A |
Fig. 4. Prototypical SiC/SiC components for GE Aviation’s next generation GE9X engine for Boeing 777X and other wide-body twinjet passenger aircrafts (Courtesy, GE Aviation) [65].
Fig. 5. Volume swelling of CVI SiC matrix composites by neutron irradiation as a function of irradiation temperature [70]. Error bars indicate?±?one standard deviation. Additional composite swelling data were taken from Refs. [75,76]. Data for highpurity CVD SiC in a monolithic form from various references are shown together as dot symbols [68,[77], [78], [79], [80], [81]].
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