A fuselage having a longitudinal window belt (58) has a composite outer skin including upper and lower composite skin sections (52, 54). The skin includes at least one window opening (70) located at the window belt (58). The upper and lower skin sections are joined together by a longitudinal splice joint (56) located at the window belt (58).
Joining composite fuselage sections along window belts
Verbinden von Verbundwerkstoffrumpfabschnitten entlang von Fensterbändern
Fixation des sections de fuselage composite le long des bandes de fenêtre
2021-12-08
Patent
Electronic Resource
English