A system for transmitting an alternating current in an aircraft. The system includes a source of electricity in the aircraft having a source connector housing, an electric load in the aircraft having a load connector housing, a cable electrically coupling the source of electricity to the electric load, a shield surrounding the cable and having a first end electrically connected to the source connector housing, and a capacitor disposed inside the load connector housing and electrically coupling a second end of the shield to the load connector housing.
WIRING HARNESS CONDUCTIVE SHIELD TERMINATION ARRANGEMENT
2025-08-07
Patent
Electronic Resource
English
WIRING HARNESS CONDUCTIVE SHIELD TERMINATION ARRANGEMENT
European Patent Office | 2025
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