An aircraft cabin embedded optical fiber sensor method

A method of embedded optical fiber sensor of an aircraft cabin, the cabin of the aircraft surface defines a plurality of predetermined longitude and latitude recess grooves, and are set aside and arranged on the circumference of the longitude, latitude Rucang holes at both ends of the concave aircraft cabin latitude Rucang slot holes one correspondence; and the multiplexing a plurality of optical fiber sensors laid in longitude and latitude recess grooves, filling the grooves with adhesive agent is fixed, to achieve the embedded optical fiber sensor surface of an aircraft cabin ; multiplexing optical fiber sensor via respective holes Rucang longitude and latitude Rucang hole into the cabin, collection bundle of optical fibers at both ends of the hull and integrated into the optical fiber connector, and then connected to the information collection device or communication with the adjacent pods . The present invention may be implemented in a single abutment surface of the aircraft cabin or pods embedded optical fiber sensor, fiber optic sensing network is formed, the mechanical performance of the aircraft cabin to solve the problems and comprehensive monitoring of damage, high reliability, easy to operate advantage.