The system for repairing aircraft structures comprises a frame (2) that is divided into two portions, and in that the system also comprises one or more straps (3) that attach both portions of the frame (2) to each other.The method comprises the steps of making a cutout in the skin (1) of the structure to be repaired; dividing the frame (2) into two portions; placing the two portions of the frame (2) on the internal side of the skin (1) through said cutout; and attaching the two portions of the frame (2) to each other by one or more straps (3).They permit the installation of an internal frame in a structure of an aircraft without internal access.
SYSTEM AND METHOD FOR REPAIRING AIRCRAFT STRUCTURES
SYSTEM UND VERFAHREN ZUR REPARATUR VON FLUGZEUGSTRUKTUREN
SYSTÈME ET PROCÉDÉ DE RÉPARATION DE STRUCTURES D'AÉRONEF
2025-07-30
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 |
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