Patent ID: 9463865
Filing Date: 2016-10-11
CPC Classification: B64C,H02G

Claim Text:
1. A fuselage cell for an aircraft comprising: a plurality of shells segments and a floor framework, at least two of the shell segments being provided with a plurality of reinforcements that are realized integrally with a skin panel of the respective shell segment so as to form integral shell segments, the reinforcements being at least one of longitudinal and circumferential, the floor framework supported on at least one of the integral shell segments, the floor framework comprising a floor surface, at least one longitudinal reinforcement integrally formed with the floor surface so as to provide a hollow space there between, and a conduit configured to receive at least one system component and/or at least one system medium, the conduit disposed in the hollow space formed between the floor surface and the at least one longitudinal reinforcement, wherein the conduit is a load bearing part of the floor framework of the aircraft.