Patent ID: 9693474
Date: 2017-06-27
CPC Classifications: B64D,H05K

Claim:
1. An electrical core of an aircraft comprising: at least one shelf on which is disposed at least one module, the at least one module having a substantially planar face containing components and including at least one input connection on a rear face of the at least one module at a first edge of the substantially planar face, the at least one input connection being configured to be linked to at least one power supply cable, wherein the substantially planar face of the at least one module further includes a protuberance along a second edge of the substantially planar face opposite the first edge, wherein the protuberance extends below the at least one shelf and comprises a face configured to coincide with at least one lip of the at least one shelf, and wherein the protuberance supports at least one output connection of the at least one module; and wherein the at least one output connection is configured to be linked to at least one output cable and is situated on the face of the protuberance coinciding with the at least one lip of the at least one shelf on an opposite side of the at least one shelf from the at least one input connection, wherein the at least one shelf has a hollow structure so that the at least one output cable travels in the hollow structure of the at least one shelf.