Fitting for aircrafts, comprising two angled pieces (1) joined to each other, each of them defining a first section (11) and a second section (12), an external plate (2) joined with both angled pieces (1), and a skin (3) joined to the external plate (2), the skin (3) being independent from the angled pieces (1).It permits to discharge the radius of the fitting angles defined by the angled pieces, discharging both angles, assuring than there is no rivet or similar joining elements installed in the angled pieces, assuring no ply continuity in the marked area.
FITTING FOR AIRCRAFTS
BESCHLAG FÜR FLUGZEUGE
FERRURE POUR AÉRONEFS
05.06.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2017
Europäisches Patentamt | 2016
|TIBKAT | 2020
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