An aircraft fuselage body is constructed of an upper body section (14) having a curved cross-section configuration and a lower body section (16) having a curved cross-section configuration. The upper body section (14) and the lower body section (16) are joined together to form an aircraft fuselage body by splice straps (88) that are secured, end to end along interior surfaces of the upper body section (14) and the lower body section (16). The aircraft fuselage body being constructed of an upper body section (14) and a lower body section (16) enables installation of systems separately into the upper body section (14) and the lower body section (16) prior to the upper body section (14) and lower body section (16) being joined together.
AIRCRAFT FUSELAGE LONGITUDINAL SPLICE FOR JOINING HALF BARREL FUSELAGE SECTIONS AND OTHER SPLICED FUSELAGE SECTIONS
LÄNGSSPLEISS FÜR EINEN FLUGZEUGRUMPF ZUM VERBINDEN VON HALBTONNENRUMPFABSCHNITTEN UND ANDEREN GESPLEISSTEN RUMPFABSCHNITTEN
ÉPISSURE LONGITUDINALE DE FUSELAGE D'AÉRONEF POUR ASSEMBLER DES SECTIONS DE FUSELAGE EN DEMI-TONNEAU ET D'AUTRES SECTIONS DE FUSELAGE ÉPISSÉES
2022-04-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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