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Electrical and electronics bay of an aircraft with an improved architecture and aircraft incorporating said bay

机译:具有改进的架构的飞机的电气和电子舱以及包含所述舱的飞机

摘要

An electrical and electronics bay of an aircraft has at least two rows of systems elements, each row being separated by a single corridor extending an entire longitudinal length of the electrical and electronics bay and being devoid of the systems elements. Each row has at least one set of systems elements and at least one electrical power center, wherein the systems elements are arranged in cabinets. At least one of the cabinets includes at least one removable mobile shelf for allowing access from a front to the back of the cabinets. Bottom edges of back faces of the cabinet are arranged against the fuselage to remove an additional corridor at the back of the cabinet, and front faces of the cabinet are directly accessible from the single corridor.
机译:飞机的电气和电子设备舱室具有至少两排系统元件,每行由单个走廊隔开,该走廊在电气和电子设备舱室的整个纵向长度上延伸并且没有系统元件。每行具有至少一组系统元件和至少一个电力中心,其中系统元件布置在机柜中。至少一个机柜包括至少一个可移动的移动架,以允许从机柜的前部到后部进入。机柜背面的底边靠着机身排列,以在机柜背面移除一条额外的走廊,并且可以从单个走廊直接进入机柜的正面。

著录项

  • 公开/公告号US9351412B2

    专利类型

  • 公开/公告日2016-05-24

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS (SAS);

    申请/专利号US201314138543

  • 发明设计人 YVES DURAND;BERNARD GUERING;

    申请日2013-12-23

  • 分类号H05K5/02;B64D43/00;H05K7/14;

  • 国家 US

  • 入库时间 2022-08-21 14:30:05

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