This invention relates to the field of
aviation safety monitoring technology, and discloses a
fiber optic dual-line
icing detection
system and method. It employs
Raman scattering distributed optical fibers laid in high-
icing areas on the upper surface of the wing to monitor temperature data in the corresponding areas; FBG
fiber gratings with a
metal coating are bonded along the spanwise direction of the wing
skin to
stress concentration areas to monitor strain data in the corresponding areas; the temperature and
strain monitoring data are demodulated separately; the demodulated temperature and strain data are received, and
icing is determined and thickness assessed using a preset icing identification
algorithm; during flight, the icing situation is sensed by changes in ambient temperature and ice pressure caused by icing at the installation location, and the
signal is transmitted to the anti-icing and de-icing
system, improving reliability and safety during flight.