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AIRCRAFT FUSELAGE PORTION COMPRISING MOVABLE OR DETACHABLE UNDER FLOOR STRUTS

机译:飞机机身部分包括在地板支柱下可移动或可拆卸

摘要

An aircraft fuselage portion extending in a general longitudinal direction and comprising a fuselage structure comprising annular frames and a flat floor. The fuselage portion also comprises struts perpendicular to the floor in a nominal position and extending from the floor to a frame. Each strut comprises, in the vicinity of at least one of the ends thereof, a detachable link so that the strut can be moved relative to the fuselage structure or separated from the fuselage structure to temporarily grant access to a triangle area located between the frames, the floor and the struts in the nominal position. This allows access to be granted to the area in which the ducts must be installed in the aircraft, in particular, in the form of sets of ducts assembled prior to their installation in the fuselage.
机译:飞机机身部分以一般的纵向延伸并且包括包括环形框架和平坦地板的机身结构。机身部分还包括垂直于标称位置垂直于地板的支柱,并从地板延伸到框架。每个支柱在其至少一个端部附近,可拆卸链节,使得支柱可以相对于机身结构移动或者与机身结构分离,以暂时授予对位于框架之间的三角形区域的访问,地板和标称位置的支柱。这允许被授予通往管道必须在飞机中安装的区域,特别是以在其安装在机身中之前组装的管道的形式。

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