A co-woven three-dimensional interpenetrating network reinforced aerogel composite material and a preparation method and application thereof
By using a co-woven three-dimensional interpenetrating network structure and supercritical drying technology, the problems of weak interfacial bonding and high thermal conductivity of traditional fiber-reinforced aerogel composites have been solved. This has enabled the development of lightweight, high-strength, ultra-low thermal conductivity, and excellent wave transmission properties for hypersonic vehicles, meeting the comprehensive performance requirements of high-end equipment.
Patent Information
- Application Number
- CN202610320113.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2026-03-17
- Publication Date
- 2026-06-02
- Estimated Expiration
- 2046-03-17
AI Technical Summary
Traditional fiber-reinforced aerogel composites in hypersonic vehicles suffer from problems such as weak interfacial bonding, difficulty in controlling fiber distribution, anisotropy, and high thermal conductivity, making it difficult to meet the requirements for synergistic optimization of mechanical, thermal, and electrical properties.
A co-woven three-dimensional interpenetrating network structure is adopted, in which hollow fibers and solid quartz fibers are integrated and woven or needle-punched to form a continuous network skeleton, and silica-based aerogel is used to fill the pores. Combined with vacuum-pressure gradient impregnation and supercritical drying technology, a composite material with strong interfacial bonding and high porosity is constructed.
The material is lightweight, high-strength, has ultra-low thermal conductivity, and excellent wave transmission performance, meeting the requirements of integrated load-bearing, heat insulation, and wave transmission for hypersonic vehicles, and improving the overall mechanical and dielectric stability of the material.