公开(公告)号：US20140286691A1

公开(公告)日：2014-09-25

申请号：US14218006

申请日：2014-03-18

申请人： Airbus Operations GmbH

发明人： Wolfgang Gleine

IPC分类号： B64C1/06

CPC分类号： B64C1/069 ,  B64C1/061 ,  B64C2211/00 ,  F16B2200/503 ,  Y10T29/49826 ,  Y10T403/28 ,  Y10T403/52

摘要： A fuselage structure for a means of transport includes at least two fuselage segments, in each case including an outer skin with an end edge. In a connecting region of two fuselage segments the end edges of the fuselage segments are spaced apart from each other. Connecting elements establish a mechanical connection between two fuselage segments. Conducting structure-borne sound is reduced by multiple deflection of the sound path, and thus results in a reduction in structure-borne sound-induced noise in the cabin of the means of transport.

摘要翻译： 用于运输工具的机身结构包括至少两个机身段，每个壳体包括具有端部边缘的外皮。 在两个机身段的连接区域中，机身段的端部边缘彼此间隔开。 连接元件在两个机身部分之间建立机械连接。 传导结构声音通过声道的多次偏转而减少，从而导致运输工具舱内的结构声音引起的噪声的降低。