A method for wiring an aircraft is described. The method includes installing a plurality of equipment (330) in a plurality of volumes, the volumes being defined by one or more of structural members and walls (360) of the aircraft, installing a backplane (320) that extends across at least a portion of the plurality of volumes, the backplane (320) including a plurality of connectors (380), connecting the plurality of equipment (330) to a first plurality of the connectors (380) on the backplane (320), and connecting shipside wiring to a second plurality of connectors (380) on the backplane (320).
METHODS AND SYSTEMS FOR INCORPORATING TRANSLATING BACKPLANES TO FACILITATE WIRE SEPARATION
VERFAHREN UND SYSTEME ZUR INTEGRATION VON ÜBERSETZENDEN RÜCKWANDPLATINEN ZUR ERMÖGLICHUNG VON DRAHTTRENNUNG
PROCÉDÉS ET SYSTÈMES PERMETTANT D'INCORPORER DES FONDS DE PANIER DE TRANSLATION POUR FACILITER LA SÉPARATION DE FIL
2021-04-28
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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