Aircraft fuselage section
AssigneeAirbus Operations GmbH
InventorsMarie Ange Barre, Didier de Villele, Thierry Duperou, Christian Godenzi, Mathieu Tesson, Anne Laure Vedel
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Abstract
The invention relates to an aircraft fuselage section comprising several longitudinal strengthening beams attached to the fuselage section lower panel and several longitudinal rails intended for supporting the floor boards, characterized by at least one crosspiece laid transversally between two strengthening beams and supporting one longitudinal rail, said crosspiece said crosspiece being mounted swiveling on the fuselage section lower panel in order to permit the rotation of the crosspiece around a longitudinal axis.
Claims8
Aircraft fuselage section comprising a number of longitudinal strengthening beams attached to a fuselage section lower panel and a number of longitudinal rails designed to support the floor boards, in which at least one crosspiece is laid transversally between two strengthening beams and supports a longitudinal rail, said crosspiece being mounted swiveling on the fuselage section lower panel in order to permit the rotation of the crosspiece around a longitudinal axis.
Dependencies are inferred from the claim text.