首页> 外国专利> Tension bolt for aircraft engine attaching device, has pin inserted in gap in radial hole of screw, and elliptical threaded crown extended by notched crown whose inner diameter is larger than base diameter of thread of nut

Tension bolt for aircraft engine attaching device, has pin inserted in gap in radial hole of screw, and elliptical threaded crown extended by notched crown whose inner diameter is larger than base diameter of thread of nut

机译:用于飞机发动机安装装置的拉紧螺栓,其销钉插入螺钉的径向孔的间隙中,并且椭圆形的齿冠由带槽的齿冠延伸,该齿冠的内径大于螺母的螺纹的底径

摘要

The tension bolt has a screw (1) pierced with a radial hole (13), and a nut (2) provided with a support face (211) and an elliptical threaded crown (25) including an elliptical section, where the threaded crown is placed at an end opposite to the support face. The threaded crown is extended by a notched crown whose inner diameter is larger than base diameter of a thread of the nut. A pin (3) i.e. split pin, is inserted in gap (23) in the radial hole of the screw. An operating unit (21) is provided between the threaded crown and the support face.
机译:张紧螺栓具有一个螺钉(1)和一个螺母(2),该螺钉(1)上有一个径向孔(13),该螺母(2)上有一个支撑面(211)和一个带有椭圆形截面的椭圆形螺纹顶盖(25),其中螺纹顶盖是放置在与支撑面相对的一端。带螺纹的冠状部由带凹口的冠状部延伸,该带齿的冠状部的内径大于螺母的螺纹的基本直径。将销钉(3),即开口销插入到螺钉的径向孔中的间隙(23)中。在螺纹冠和支撑面之间设有操作单元(21)。

著录项

  • 公开/公告号FR2955632A1

    专利类型

  • 公开/公告日2011-07-29

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS;

    申请/专利号FR20100050594

  • 申请日2010-01-28

  • 分类号F16B39/04;B64D27/26;F16B31;F16B35;F16B39/284;

  • 国家 FR

  • 入库时间 2022-08-21 17:45:45

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