A bypass device (3) having an electrical harness (4) for an aircraft cable raceway, said device being suitable for steering the trajectory of an electrical harness away from a cable guide channel of an aircraft cable raceway, said bypass device being characterised in that it comprises: - a clip-on support base (5); - a pad (13) opposite the support base (5), said pad (13) comprising a support groove; - a central body (15) attached on one side to the support base (5) and on the other side to the pad (13), said central body (15) being suitable for being positioned opposite a cable guide channel when the bypass device (3) is attached to an aircraft cable raceway, said central body (15) comprising a bypass clamp (17) for the electrical harness; the support base (5) and the pad (13) being suitable for being attached to two side walls (1,2) adjacent to a guide channel of a cable raceway.
DISPOSITIF DE DERIVATION POUR CHEMIN DE CABLES D'AERONEF
BYPASS DEVICE FOR AN AIRCRAFT CABLE RACEWAY
BYPASSVORRICHTUNG FÜR EINEN KABELKANAL EINES FLUGZEUGS
2024-06-05
Patent
Elektronische Ressource
Französisch
IPC: | H02G INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES , Verlegen oder Installieren elektrischer Kabel oder Leitungen, Verlegen oder Installieren kombinierter optischer und elektrischer Kabel oder Leitungen / B64C AEROPLANES , Flugzeuge / F16L PIPES , Rohre |
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