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Joining and integration of advanced carbon-carbon composites to metallic systems for thermal management applications
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Singh, M. Asthana, R. |
| Copyright Year | 2008 |
| Description | Recent research and development activities in joining and integration of carbon-carbon (C/C) composites to metals such as Ti and Cu-clad-Mo for thermal management applications are presented with focus on advanced brazing techniques. A wide variety of carbon-carbon composites with CVI and resin-derived matrices were joined to Ti and Cu-clad Mo using a number of active braze alloys. The brazed joints revealed good interfacial bonding, preferential precipitation of active elements (e.g., Ti) at the composite/braze interface. Extensive braze penetration of the inter-fiber channels in the CVI C/C composites was observed. The chemical and thermomechanical compatibility between C/C and metals at elevated temperatures is assessed. The role of residual stresses and thermal conduction in brazed C/C joints is discussed. Theoretical predictions of the effective thermal resistance suggest that composite-to-metal brazed joints may be promising for lightweight thermal management applications. |
| File Size | 3443835 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20090008500 |
| Archival Resource Key | ark:/13960/t08w8d18j |
| Language | English |
| Publisher Date | 2008-11-10 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Carbon-carbon Composites Systems Management Thermal Resistance Metal Joints Titanium Temperature Control Cladding Soldered Joints Bonding Chemical Compatibility Residual Stress Resin Matrix Composites Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |