首页> 外国专利> ASSEMBLY FOR AIRCRAFT COMPRISING A MOUNTING STRUT PRIMARY STRUCTURE ATTACHED TO A WING BOX BY COMPACT FASTENERS IN THE LEADING EDGE AREA

ASSEMBLY FOR AIRCRAFT COMPRISING A MOUNTING STRUT PRIMARY STRUCTURE ATTACHED TO A WING BOX BY COMPACT FASTENERS IN THE LEADING EDGE AREA

机译:用于飞机组件,包括通过紧凑的紧固件在翼盒中连接到翼盒中的安装支柱初级结构

摘要

An aircraft comprising a wing, an engine attachment pylon comprising a primary structure and an arrangement for securing the primary structure to a wing box. The arrangement comprises two lateral front fittings, each of these fittings comprising a first connecting portion secured to the front wing spar, a second connecting portion secured to the primary structure of the attachment pylon, at least one securing member linking the first and second connecting portions, this securing member being articulated to the first connecting portion with the aid of a first pin system oriented substantially parallel to the front wing spar.
机译:包括机翼的飞机,发动机附接塔架,其包括主要结构和用于将初级结构固定到翼盒的装置。 该装置包括两个横向前部配件,每个配件中的每一个包括固定到前翼翼翼的第一连接部分,第二连接部分固定到附接塔的主要结构,至少一个连接第一和第二连接部分的固定构件 ,该固定构件借助于基本平行于前翼翼垫的第一销系统铰接到第一连接部分。

著录项

  • 公开/公告号EP3505448B1

    专利类型

  • 公开/公告日2021-10-13

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS SAS;

    申请/专利号EP20180214883

  • 发明设计人 PAUTIS OLIVIER;COLMAGRO JÉRÔME;

    申请日2018-12-20

  • 分类号B64D27/18;B64D27/26;

  • 国家 EP

  • 入库时间 2022-08-24 21:39:48

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