Joining and Integration of Silicon Carbide-Based Materials for High Temperature Applications

Halbig, Michael C.; Singh, Mrityunjay

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NASA NTRS · 20160010279

Joining and Integration of Silicon Carbide-Based Materials for High Temperature Applications

Halbig, Michael C.·Singh, Mrityunjay

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Abstract

Advanced joining and integration technologies of silicon carbide-based ceramics and ceramic matrix composites are enabling for their implementation into wide scale aerospace and ground-based applications. The robust joining and integration technologies allow for large and complex shapes to be fabricated and integrated with the larger system. Potential aerospace applications include lean-direct fuel injectors, thermal actuators, turbine vanes, blades, shrouds, combustor liners and other hot section components. Ground based applications include components for energy and environmental systems. Performance requirements and processing challenges are identified for the successful implementation different joining technologies. An overview will be provided of several joining approaches which have been developed for high temperature applications. In addition, various characterization approaches were pursued to provide an understanding of the processing-microstructure-property relationships. Microstructural analysis of the joint interfaces was conducted using optical, scanning electron, and transmission electron microscopy to identify phases and evaluate the bond quality. Mechanical testing results will be presented along with the need for new standardized test methods. The critical need for tailoring interlayer compositions for optimum joint properties will also be highlighted.

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Halbig, Michael C., Singh, Mrityunjay. 2016-01-24. Joining and Integration of Silicon Carbide-Based Materials for High Temperature Applications. https://ntrs.nasa.gov/citations/20160010279

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