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US 2026/0260783 A1Published application
Electric Power Harness for An Aircraft
AssigneeSafran Electrical & Power
InventorsJérôme GENOULAZ, Laurent Pierre François Jules AZEMARD
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Abstract
An electric-power harness for aircraft includes a plurality of cables. Each cable has, radially from the inside to the outside, a conducting core, a first layer of semiconductor material, an insulating layer, and a second layer of semiconductor material. The harness further includes a shared shielding placed in electrical contact with the second layers of semiconductor material of each cable.
Claims11
An electric-power harness (10) for aircraft, comprising a plurality of cables (11), where each cable (11) comprises, radially from the inside to the outside:
- a conducting core (12);
- a first layer (13) of semiconductor material;
- an insulating layer (14);
- and
- a second layer (15) of semiconductor material;
- wherein the harness (10) further comprises a shared shielding (16, 16′) placed in electrical contact with the second layers (15) of semiconductor material of each cable (11).
3 more elements
Dependencies are inferred from the claim text.