Patent ID: 9327821
Filing Date: 2016-05-03
CPC Classification: B64C,Y10T

Claim Text:
1. Aircraft structural assembly having an area element which comprises a core and an outer layer, wherein: a first surface of the area element, when seen from the outside of the area element, is convexly curved relative to an imaginary central area of the area element extending through the core of the area element, and a second surface of the area element located opposite the first surface is oriented parallel to the imaginary central area of the area element extending through the core of the area element, the area element being configured in the form of a floor panel of a floor system, the second surface of the area element being structured to form a walkable floor surface of the floor system when the aircraft structural assembly is mounted in an aircraft, and the area element of the aircraft structural assembly being convexly curved in the region of the entire first surface of the area element relative to the imaginary central area of the area element, wherein the area element has at least one area region not provided with a core, wherein the area region not provided with a core extends along a section of a peripheral edge of the area element, wherein a plurality of fastening rails for fixing one of a seat and a structural monument to the area element is integrated into the core of the area element, the plurality of fastening rails including one of the at least one outermost fastening rails located closest to one of the area region not provided with a core, and wherein the area element comprises a connecting device that connects the area element to a first end of a supporting rod for connecting the area element to the aircraft structure, the connecting device being integrated into the core at a location of the core that is adjacent to but spaced apart from the area region not provided with a core and between the one of the at least one outermost fastening rails and the area region not provided with a core.