首页> 外国专利> REAR ENGINE MOUNT OF AN AIRCRAFT WITH TIE RODS IN TWO PARTS AND AIRCRAFT COMPRISING AT LEAST ONE SUCH REAR ENGINE MOUNT

REAR ENGINE MOUNT OF AN AIRCRAFT WITH TIE RODS IN TWO PARTS AND AIRCRAFT COMPRISING AT LEAST ONE SUCH REAR ENGINE MOUNT

机译:带有拉杆的飞机的后发动机安装架,包括两个部分,并且飞机至少由一个这样的后发动机安装架组成

摘要

The object of the invention is an aircraft rear engine attachment connecting a primary structure (56) of a mast and an engine (58) of an aircraft. The rear engine attachment comprises first and second links (70, 76), each of them comprising at least two parts (86.1, 86.2), a first part (86.1) comprising at least one support hole (70.1, 70.2, 76.1 ), housing a support link pin (72.1, 72.2, 72.3) configured to connect the rod (70, 76) directly or indirectly to the primary structure (56), at least a second part (86.2) comprising at least one engine orifice (74.1, 74.2), housing an engine connecting pin (74.1, 74.2, 78) configured to connect the rod (70, 76) directly or indirectly to the engine (58), as well as removable connecting elements (88) to connect the first and second parts (86.1, 86.2) oriented parallel to the direction of the rod.
机译:发明内容本发明的目的是一种飞机后发动机附件,其连接桅杆的主要结构(56)和飞机的发动机(58)。发动机后部附件包括第一和第二连杆(70、76),每个连杆均包括至少两个部分(86.1、86.2),包括至少一个支撑孔(70.1、70.2、76.1)的第一部分(86.1),壳体支撑连杆销(72.1、72.2、72.3),其构造成将杆(70、76)直接或间接连接到主结构(56),至少第二部分(86.2)包括至少一个发动机孔(74.1、74.2) )上装有一个发动机连接销(74.1、74.2、78),该销配置为直接或间接将杆(70、76)连接到发动机(58),以及可移动的连接元件(88),用于连接第一部分和第二部分(86.1,86.2)的方向平行于杆的方向。

著录项

  • 公开/公告号EP3715258A1

    专利类型

  • 公开/公告日2020-09-30

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS SAS;

    申请/专利号EP20200161078

  • 发明设计人 BERJOT MICHAEL;GELIOT JEAN;

    申请日2020-03-05

  • 分类号B64D27/26;

  • 国家 EP

  • 入库时间 2022-08-21 11:39:38

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