| Citation: | Chen Xinran, Shen Xiuli, Dong Shaojing, et al. Review of ceramic matrix composites and metal junction structures[J]. Journal of Aerospace Power, 2026, 41（11）：20250365 doi: 10.13224/j.cnki.jasp.20250365
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The ceramic matrix composites (CMCs) and metal connection structures in aero-engine combustion chambers and turbine guide vanes were systematically examined, covering structural design, numerical simulation, and experimental validation. Current studies put focus on four thermal mismatch mitigation strategies: transition region coordination, clearance design, interlocking fit, and thermal stress-free fastener. Multi-scale modeling and progressive damage analysis were widely employed in simulations, alongside a stepwise experimental verification framework. Structural configurations varied with specific application scenarios and operational conditions. Future development should combine multiple design strategies and shift from component-level connection design to system-level thermo-mechanical-cooling multifunctional coordinated design, so as to ensure long-term structural reliability under extreme conditions.
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