The present invention regards an aircraft structure comprising an aerodynamic composite shell (7), the interior face (9) of which in whole or in part is bonded with at least one two- or three-dimensional structural composite part (11) by means of a bonding material (15). It also regards a method of manufacture of the aircraft structure. The bonding material (15) comprises a non-structural fiber reinforced resin system, wherein at least one portion of the bonding material, which portion spatially corresponds with an interior face filling volume (21), is thicker than other portions of the bonding material (15), due to settlement of resin of the non-structural fiber reinforced resin system in said interior face filling volume (21) during the viscous phase of the curing of the non-structural fiber reinforced resin system.
AN AIRCRAFT STRUCTURE WITH STRUCTURAL NON-FIBER REINFORCING BONDING RESIN LAYER
FLUGZEUGSTRUKTUR MIT STRUKTURELLER FASERFREIER VERSTÄRKENDER BINDEHARZSCHICHT
STRUCTURE D'AÉRONEF POSSÉDANT UNE COUCHE DE RÉSINE DE LIAISON DE RENFORCEMENT À FIBRES NON STRUCTURELLES
2016-01-06
Patent
Electronic Resource
English
ORGANIC FIBER CORD FOR TIRE REINFORCING LAYER AND AIRCRAFT TIRE USING THE SAME
European Patent Office | 2024
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