The distributed aircraft anti-icing and de-icing power system is a power device that achieves ice prevention and treatment on aircraft wings through electrothermal and shock vibration. Based on the thermo-mechanical coupling of the composite de-icing method, it combines electrothermal de-icing with shock vibration de-icing to form an efficient and low-energy de-icing method. It complies with and passes the environmental testing standards of the GJB Standard, as well as the GJB151B electromagnetic compatibility emission and conduction interference standards. It has been verified through ice-forming wind tunnel tests for its good de-icing performance.

The distributed airborne anti-icing and de-icing power supply system can perform de icing work through ground manual control, and can also develop automatic de-icing strategies based on the airflow temperature and flight altitude provided by the aircraft platform.