A landing gear of an aircraft includes a pair of wheels between which an electric actuator at least partially covered with a lightning arrester cowl is placed. The lightning arrester cowl has an insulating matrix onto which at least an electrical conductor is attached. The electrical conductor includes electrical connection means for connecting the electrical conductor to a ground conductor of the aircraft.
Landing gear with lightning protection
2025-01-28
Patent
Electronic Resource
English
Landing gear up-down position detection assembly and landing gear up-down position protection system
European Patent Office | 2025
|Tema Archive | 1975