首页> 外国专利> PRIMARY STRUCTURE OF AN AIRCRAFT PYLON HAVING AT LEAST ONE TRANSVERSE REINFORCER EQUIPPED WITH TWO DIAGONALLY DISPOSED LINK RODS, AND AIRCRAFT COMPRISING SUCH A PRIMARY STRUCTURE

PRIMARY STRUCTURE OF AN AIRCRAFT PYLON HAVING AT LEAST ONE TRANSVERSE REINFORCER EQUIPPED WITH TWO DIAGONALLY DISPOSED LINK RODS, AND AIRCRAFT COMPRISING SUCH A PRIMARY STRUCTURE

机译:带有两个对角布置的连杆的至少一个横向加劲器的飞机塔架的主要结构,以及具有这种主要结构的飞机

摘要

A primary structure of an aircraft pylon, which comprises upper and lower spars, right-hand and left-hand lateral panels, transverse reinforcers that are disposed in transverse planes and, each have a square or rectangular contour and at least one sole to which the upper and lower spars and the right-hand and left-hand lateral panels are fastened. At least one of the transverse reinforcers of the primary structure has first and second link rods that are oriented along diagonals of the transverse reinforcer, and connecting systems that each connect first and second ends of the first and second link rods to the sole or to one of the soles.
机译:飞机吊架的主要结构,包括上部和下部梁,左右侧板,布置在横向平面上的横向加强筋,每个横向钢筋都具有正方形或矩形轮廓,并至少具有一个底面上部和下部梁以及右侧和左侧侧板均已固定。主体结构的横向加强件中的至少一个具有沿着横向加强件的对角线定向的第一和第二连杆,以及分别将第一和第二连杆的第一和第二端连接到鞋底或鞋底的连接系统。鞋底。

著录项

  • 公开/公告号US2020269987A1

    专利类型

  • 公开/公告日2020-08-27

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS SAS;

    申请/专利号US202016782271

  • 发明设计人 OLIVIER GLEIZE;

    申请日2020-02-05

  • 分类号B64D27/26;B64D29/02;

  • 国家 US

  • 入库时间 2022-08-21 11:23:36

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