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MASTER OF HITCH OF A MOTOR UNDER A PLANE OF SUSTAINATION OF AN AIRCRAFT.

机译:在飞机持续维持的平面上,电动机的牵引力大师。

摘要

Mast (10) of engagement of an engine (16) under a lift plane (12) of an aircraft, comprising a rigid structure and engagement means of said rigid structure under the lift plane, including said engagement means a front fastener (22), a rear fastener (24) and a stress recovery means (26), characterized in that the rigid structure comprises a rear part (20b) that has a width that increases substantially as it advances towards the part rear, the rear fixing (24) comprising two rear fittings (36) fixed to the rigid structure, so that they protrude laterally on either side of it, in a rear area of said rear part (20b), and at least two connecting elements that connect each of the aforementioned rear fittings (36) with a structural part (37) of the lift plane (12).
机译:发动机(16)在飞机的升力平面(12)下的接合的桅杆(10),其包括刚性结构和所述刚性结构在升力平面下方的接合装置,包括所述接合装置,前紧固件(22),后紧固件(24)和应力恢复装置(26),其特征在于,刚性结构包括后部(20b),后部(20b)的宽度随着其向后部的前进而基本上增加,后部固定件(24)包括固定在刚性结构上的两个后配件(36)分别在所述后部(20b)的后部区域中在其两侧横向突出,并具有至少两个连接上述每个后配件的连接元件( 36)具有提升平面(12)的结构部件(37)。

著录项

  • 公开/公告号ES2258717T3

    专利类型

  • 公开/公告日2006-09-01

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号ES20030720648T

  • 发明设计人 MARCHE HERVE;

    申请日2003-02-26

  • 分类号B64D27/18;B64D27/26;

  • 国家 ES

  • 入库时间 2022-08-21 21:35:49

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