Provided is a transition assembly for a wire harness configured to be coupled to a plate in an aircraft. The transition assembly includes a slotted flange configured to abut a first side of the plate, a junction having a flange configured to abut a second side of the plate, the flange including inwardly extending cutouts on opposite sides thereof forming a reduced width portion of the flange, and a nut configured to couple to the junction.
AIRCRAFT WIRE HARNESS
2024-07-18
Patent
Electronic Resource
English
IPC: | B60R Fahrzeuge, Fahrzeugausstattung oder Fahrzeugteile, soweit nicht anderweitig vorgesehen , VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR |
Wire harness, wire harness manufacturing method, and wire harness routing structure
European Patent Office | 2024
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