Electrical and electronics bay of an aircraft with an improved architecture and aircraft incorporating said bay

摘要

An electrical and electronics bay of an aircraft has at least two rows of systems elements, each row being separated by a single corridor extending an entire longitudinal length of the electrical and electronics bay and being devoid of the systems elements. Each row has at least one set of systems elements and at least one electrical power center, wherein the systems elements are arranged in cabinets. At least one of the cabinets includes at least one removable mobile shelf for allowing access from a front to the back of the cabinets. Bottom edges of back faces of the cabinet are arranged against the fuselage to remove an additional corridor at the back of the cabinet, and front faces of the cabinet are directly accessible from the single corridor.

主权项

1. An electrical and electronics bay of an aircraft being delimited by a fuselage and comprising:
at least two sets of systems elements having electrical and electronics components, and at least two electrical power centers; wherein said at least two sets of systems elements and said at least two electrical power centers are arranged in two rows, each row being separated by a single corridor extending an entire longitudinal length of the electrical and electronics bay and being devoid of the systems elements, each row having at least one set of systems elements and at least one electrical power center, and wherein the systems elements are arranged in a plurality of cabinets, at least one of the plurality of cabinets including at least one of a first removable mobile shelf that is mounted on sliders and configured for allowing access from a front to a back of the corresponding cabinet by crossing the corresponding cabinet, at least another one of the plurality of cabinets including at least one of a second removable mobile shelf that is mounted around a pivot axis and configured for allowing access from the front to the back of the corresponding cabinet by crossing the corresponding cabinet, and bottom edges of back faces of the plurality of cabinets are arranged against the fuselage to preclude an additional corridor at the back of the corresponding cabinet, and front faces of the plurality of cabinets are directly accessible from the single corridor, and wherein the at least another one of the plurality of cabinets includes at least two struts, and the pivot axis is disposed on one side of the corresponding cabinet and on one of the at least two struts.