A structure system for installation into a fuselage structure in an interior of an aircraft. The system has a first carrier element, a second carrier element, an elongate frame element having a first end and a second end, a first attachment device for attaching the first carrier element to the fuselage structure or to an element coupled with the fuselage structure, a first coupling device mounted to the first end for coupling the first carrier element to the frame element, and a second coupling device mounted to the second end for coupling the second carrier element to the frame element. The frame element holds a component to be installed in the interior. The first carrier element couples with the first coupling device, the second carrier element couples with the second coupling device, and one of the coupling devices snaps into the respective carrier element.
STRUCTURE SYSTEM FOR INSTALLATION INTO A FUSELAGE STRUCTURE
2024-06-20
Patent
Electronic Resource
English
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
STRUCTURE SYSTEM FOR INSTALLATION INTO A FUSELAGE STRUCTURE
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