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
18.07.2024
Patent
Elektronische Ressource
Englisch
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 MANUFACTURING DEVICE
Europäisches Patentamt | 2021
|WIRE HARNESS SHEET, WIRE HARNESS, AND METHOD OF MANUFACTURING WIRE HARNESS
Europäisches Patentamt | 2018
|