Joining of carbon-carbon composites using boron and titanium disilicide interlayers
Journal Article
·
· Journal of the American Ceramic Society
- Wright State Univ., Dayton, OH (United States). Dept. of Mechanical and Materials Engineering
- Lockheed Missiles and Space Co., Sunnyvale, CA (United States)
Carbon-carbon (C-C) composites are attractive as candidate structural materials for high-temperature aerospace applications. The feasibility of joining of 3-D carbon-carbon (C-C) composites by using B and TiSi{sup 2} interlayers has been investigated. The optimum temperature for joining with a B interlayer was determined to be about 1,995 C and that for joining with a TiSi{sub 2} interlayer was about 1,490 C. The shear strengths of the joints made at these optimum temperatures were found to increase with the shear testing temperature up to a point, followed by a decrease at higher temperatures. For C-C specimens bonded at 1,995 C with a B interlayer, the maximum joint shear strength (average value 18.35 MPa) was observed at the test temperature of 1,660 C. The shear strength of joints produced with a TiSi{sub 2} interlayer showed a maximum at the test temperature of 1164 C, with an average value of 34.41 MPa. The B interlayers reacted with C-C composite pieces during joining, and the product of reaction was identified as B{sub 4}C. In specimens joined with TiSi{sub 2} interlayers, the reaction between TiSi{sub 2} and C did not go to completion, and the bond interlayer contained TiC, SiC, and TiSi{sub 2}.
- Sponsoring Organization:
- USDOE
- OSTI ID:
- 455163
- Journal Information:
- Journal of the American Ceramic Society, Journal Name: Journal of the American Ceramic Society Journal Issue: 1 Vol. 80; ISSN 0002-7820; ISSN JACTAW
- Country of Publication:
- United States
- Language:
- English
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