Project Code: 36203
Start date and planned duration: January 2025, 12 months
Objective
- Evaluate thermal and mechanical compatibility of CMCs and metals to identify suitable combinations for high temperature applications.
- Develop suitable brazing and diffusion bonding parameters to ensure stable joints between dissimilar materials.
- Characterise joint integrity and performance through microstructural and mechanical testing.
Project Outline
Ceramic Matrix Composites (CMC’s) are emerging as an alternative to monolithic ceramics, offering comparable high temperature performance and significantly enhanced mechanical properties due to their fiber reinforced matrix structure. These attributes make CMCs highly suitable for demanding high performance applications.
Currently there are manufacturing techniques to fabricate Ceramic Matrix Composites (CMCs); however, one of the key challenges facing the industry is the development of reliable methods to join these materials. The joining process is particularly critical for ensuring structural integrity under extreme operating conditions. Therefore, we are proposing to develop a market offering focussed on joining solutions for high temperature operation of CMCs.
Industry Sectors
- Aerospace
- Space
- Defense
- Nuclear
Benefits to Industry
- Facilitates the development of components that can withstand extreme environments, crucial for aerospace, space, defense and nuclear sectors.
- Supports the integration of lightweight, heat resistant CMCs into metallic systems, enabling higher operating temperatures and improved thermodynamic efficiency.
- Bridges a critical materials integration gap, helping industries fast tract the deployment of next generation propulsion systems, thermal protection systems and structural components.
- Opens new pathways for hybrid material design and multifunctional component development driving innovation in advanced materials.