Patent ID: 9644765
Date: 2017-05-09
CPC Classifications: B64C,B64D,B64F,F16L,Y02T,Y10T

Claim:
1. A system for mounting aircraft system components in the crown area of an aircraft, said system comprising: a first longitudinal carrier element; a second longitudinal carrier element disposed substantially parallel to and at a distance from said first longitudinal carrier element; and a bridging element which connects the first longitudinal carrier element to the second longitudinal carrier element, wherein the system is mountable in the crown area of an aircraft in such a way that a longitudinal axis of each of the first and the second longitudinal carrier element extend substantially parallel to a longitudinal axis of the aircraft, and wherein a plurality of cable ducts for accommodating electrical lines is provided on at least one of the first and the second longitudinal carrier elements, wherein the first longitudinal carrier element comprises a main body having a first main surface and a second main surface, the first and second main surfaces forming an outer appearance of the first longitudinal carrier element and extending substantially parallel to the longitudinal axis of the first longitudinal carrier element, the first main surface facing towards the second longitudinal carrier element and the second main surface facing away from said second longitudinal carrier element, cable ducts provided on the first longitudinal carrier element being disposed both in the region of the first main surface and in the region of the second main surface of the main body of the first longitudinal carrier element.