4.7 Article

Spark Plasma Joining of ZrB2-SiC Composites Using Zirconium-Boron Reactive Filler Layers

Journal

JOURNAL OF THE AMERICAN CERAMIC SOCIETY
Volume 94, Issue 11, Pages 3825-3832

Publisher

WILEY-BLACKWELL
DOI: 10.1111/j.1551-2916.2011.04739.x

Keywords

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Funding

  1. Air Force Office of Scientific Research [FA9550-10-C-0084]
  2. Advanced Ceramics Manufacturing LLC.
  3. Division Of Materials Research
  4. Direct For Mathematical & Physical Scien [0954110] Funding Source: National Science Foundation

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Spark plasma joining is used to join ZrB2-SiC composites with seamless microstructures at the joint that results in retention of high-temperature mechanical and oxidation properties after joining. Our approach uses a spark plasma sintering furnace and Zr-B powder filler layers to join the parts together. The joining processing parameters used to optimize the joint microstructure were filler composition, target temperature, hold time, and volume of filler. A filler of 1 mm(3) and spark plasma joining conditions at 1800 degrees C for 300 s resulted in the formation of a joint region that was indistinguishable from the bulk substrates. Room and high-temperature (1350 degrees C) shear strengths of joined substrates measured equal to baseline substrates and oxidation behavior for joined and baseline substrates were equivalent after static air oxidation at 1700 degrees C. X-Ray diffraction measurements show the joint is composed of ZrB2 and ZrC. We found the joining mechanism to be solid-state bonding of ZrB2 that formed from the Zr-B filler and reaction bonding by the formation of ZrC. Spark plasma joining rapidly joins ZrB2-SiC and probably other conductive ultra high-temperature ceramic composites, and has the potential to impact the rapid assembly and joining of complex thermal protection material systems.

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