Abstract:During flight, aircraft accumulate high-potential precipitation static on their surfaces due to air friction and particle collisions, which can interfere with communication and navigation systems or even damage critical equipment. Electrostatic dischargers are essential protective measures, and their layout is critical to effective static discharge. This study, based on the mechanisms of static generation and empirical formulas, investigates key aspects such as the calculation of the required number of dischargers, optimization of installation locations, the impact of device performance parameters, and simulation-based validation methods. By integrating theoretical analysis and simulation validation, a scientific layout method for electrostatic dischargers is proposed, significantly enhancing the safety and efficiency of static protection design. The findings provide valuable technical references for the static protection design of aircraft.