作者: Guillaume Gallant , Philippe Bernadet
DOI:
关键词: Engineering 、 Nose cone 、 Section (archaeology) 、 Structural engineering 、 Fuselage
摘要: The invention relates to an aircraft fuselage comprising a nose cone (2), tail section (2) and central (3), the longitudinal panels (31 - 39) assembled directly with one another, at least of these having length corresponding distance between in order connect said section.