Carbon fibrous aerogels, distinguished by low density, outstanding mechanical properties and thermal stability, hold great promise for applications in aerospace, military, and environmental protection. However, large-scale production and precise structure control of carbon fibrous aerogels present significant challenges. Herein, solution blow spinning combined with rotating receiving apparatus was employed to fabricate elastic lamellar carbon/silica nanofibrous aerogels (CSNFAs). The utilization of receiving apparatus for traction enabled efficient assembly of PAN nanofiber networks into layered and stacked structure. Interlayer spacing of CSNFAs could be finely tuned within range of 30–250 μm by adjusting speed with range of 500–1000 RPM. The mesoporous architecture of CSNFAs, along with their intrinsic properties, significantly enhanced adsorption capabilities. Integration of lamellar structure enabled precise control over thermal stability. Capitalizing on laminated structure, CSNFAs exhibited excellent compressive elasticity while maintaining exceptional super elasticity across extreme temperatures ranging from 600 °C to −196 °C. CSNFAs guaranteed reliable performance across a wide temperature range and supported repeated use.
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