An aircraft fuselage body is constructed of an upper body section having a curved cross-section configuration and a lower body section having a curved cross-section configuration. The upper body section and the lower body section are joined together to form an aircraft fuselage body by splice straps that are secured, end to end along interior surfaces of the upper body section and the lower body section. The aircraft fuselage body being constructed of an upper body section and a lower body section enables installation of systems separately into the upper body section and the lower body section prior to the upper body section and lower body section being joined together.
AIRCRAFT FUSELAGE LONGITUDINAL SPLICE FOR JOINING HALF BARREL FUSELAGE SECTIONS AND OTHER SPLICED FUSELAGE SECTIONS
EPISSURE LONGITUDINALE DE FUSELAGE D'AERONEF POUR JOINDRE LES SECTIONS DE FUSELAGE MI-TONNEAU ET D'AUTRES SECTIONS DE FUSELAGE EPISSEES
30.03.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile |
Europäisches Patentamt | 2022
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|SPLICE AND ASSOCIATED METHOD FOR JOINING FUSELAGE SECTIONS
Europäisches Patentamt | 2018
Splice and associated method for joining fuselage sections
Europäisches Patentamt | 2016
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