| abstract |
A kind of system for status monitoring fiber compound structure, the fiber compound structure of the fiber compound structure especially aircraft or spacecraft, which includes: fiber compound structure；Multiple state sensors, the state sensor are located on fiber compound structure and/or in complex structure of filament, and are configured as the status data of detection fiber compound structure；Energy storage device, the energy storage device are configured as storing the electric energy of the power supply for state sensor in a manner of rechargeable；Energy generation layer, the energy generation layer are configured as generating the electric energy of the power supply for state sensor on fiber compound structure；Data processing unit, which is configured as carrying out wireless data communication with state sensor, to be further processed the status data detected. |