A floor assembly for an aircraft comprising a multiplicity of supports configured to be fastened in pairs to opposite sides of a frame of the aircraft, and a monolithic self-supporting floor element comprising at least two longitudinal members, a floor plate arranged on the longitudinal members and a respective connecting element arranged at each end of each of the longitudinal members. The floor element can be fastened to the frame by fastening of each connecting element to a corresponding support, and the floor plate can extend in the direction of the longitudinal members at least between two supports fastened in pairs. Furthermore, an aircraft region comprises such a floor assembly, an aircraft comprises such an aircraft region.
Floor assembly comprising a monolithic floor element, and aircraft region and aircraft comprising a floor assembly
2021-11-02
Patent
Electronic Resource
English
European Patent Office | 2019
|AIRCRAFT FLOOR COMPRISING A SEALING TARPAULIN, AND AIRCRAFT COMPRISING SAID FLOOR
European Patent Office | 2024
|European Patent Office | 2022
|AIRCRAFT-FLOOR ELEMENT, AIRCRAFT ZONE AND AIRCRAFT HAVING AN AIRCRAFT-FLOOR ELEMENT
European Patent Office | 2020
|Aircraft-floor element, aircraft zone and aircraft having an aircraft-floor element
European Patent Office | 2024
|