Abstract
With the extensive use of carbon/silicon carbide composite materials(C/SiC) in aerospace fields, the bolting of C/SiC materials is important in structure of aircraft and spacecraft. However, there is a problem of the heat matching with the use of metal bolts. Now it can be solved by the development of C/SiC bolts. The C/SiC bolts were prepared by chemical vapor infiltration (CVI). The carbon fabric preform was fabricated with the three dimension needling method. The mechanical properties of C/SiC bolts were investigated. The results indicated that the average tensile strength of C/SiC bolts was 114.71 MPa and the average shear strength of C/SiC bolts was 71.34 MPa. These results are helpful for the design of C/SiC materials bolting in Aerospace Structures.
| Original language | English |
|---|---|
| Title of host publication | High Temperature Ceramic Matrix Composites 8 |
| Publisher | wiley |
| Pages | 675-679 |
| Number of pages | 5 |
| ISBN (Electronic) | 9781118932995 |
| ISBN (Print) | 9781118932988 |
| DOIs | |
| State | Published - 1 Jan 2014 |
Keywords
- Carbon/silicon carbide composites
- Chemical vapor infiltration
- Heat matching
- Mechanical properties
- Tensile strength
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