Special optical cable, preparation method and sensing equipment with special optical cable
By designing the layer-by-layer enhanced structure and modified nanomaterials of special optical cables, the performance problems of optical fiber cables in high temperature environments are solved, and the high temperature resistance and bending and compression resistance of optical cables are improved, and are suitable for aviation structure health monitoring and data storage.
Patent Information
- Application Number
- CN202511001059.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-07-21
- Publication Date
- 2025-08-19
- Estimated Expiration
- 2045-07-21
AI Technical Summary
Existing fiber optic cables are prone to softening, yellowing, and cracking in high temperature environments, which cannot meet the requirements of special application scenarios such as aviation, and the performance of transmission cables has not been disclosed.
A special optical cable is designed, including an optical fiber body from the inside to the outside, a high-temperature resistant coating layer, a primary buffer layer, a secondary buffer layer, a reinforcement layer and a sheath layer. The coating layer is equipped with an inner layer, a transition layer and an outer layer from the inside to the outside, and a layer-by-layer reinforcement scheme of three coatings is adopted, and a microstructure is designed on the outer surface of the high-temperature resistant coating layer, combining modified nanomaterials and high-strength fiber materials to improve high-temperature, bending and compressive resistance.
It has achieved significant improvement in the high temperature resistance and bending and compression resistance of optical cables, and has excellent properties such as lightweight, fast thermal conductivity, radiation resistance, strong electric field and strong magnetic field environment, high wear resistance, flame retardant, corrosion resistance, etc. It is suitable for structural health monitoring equipment, and realizes accurate monitoring and storage of aircraft structural parameters.