A system (200) for transmitting an alternating current in an aircraft. The system includes a source of electricity (121) in the aircraft having a source connector housing (202), an electric load (106) in the aircraft having a load connector housing (204), a cable (206) electrically coupling the source of electricity (121) to the electric load (106), a shield (220) surrounding the cable (206) and having a first end (208) electrically connected to the source connector housing (202), and a capacitor (226) disposed inside the load connector housing (204) and electrically coupling a second end (210) of the shield (220) to the load connector housing (204).
WIRING HARNESS CONDUCTIVE SHIELD TERMINATION ARRANGEMENT
LEITFÄHIGE ABGESCHIRMTE KABELBAUMABSCHLUSSANORDNUNG
AGENCEMENT DE TERMINAISON DE BLINDAGE CONDUCTEUR DE FAISCEAU DE CÂBLES
2025-08-13
Patent
Electronic Resource
English
WIRING HARNESS CONDUCTIVE SHIELD TERMINATION ARRANGEMENT
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