首页> 外国专利> 'U' BRACKET FOR RENIFORCEMENT OF STANDARD AND NON STANDARD ATR SIZE AVIONICS MOUNTING TRAY

'U' BRACKET FOR RENIFORCEMENT OF STANDARD AND NON STANDARD ATR SIZE AVIONICS MOUNTING TRAY

机译:用于加固标准和非标准ATR尺寸航空电子安装托盘的“ U”形支架

摘要

pThe joint at rear end of the Avionics mounting tray should be high enough to withstand to the vibration and shock loading , especially in arrestor landing test. Mounting tray carries two locating pins/dowel pins at this side through which total induced vibration or shock loading transferred to the tray at rear side. The total induced forces are concentrated at these two pins only. Therefore the joint and bearing member to which these pins are fixed should also have enough strength to resist the coming forces especially in Arrestor landing shock test. The 'U' Bracket is designed for any ATR sized and non ATR sized Avionics mounting tray is to reinforce the joint at which it is fixed. The geometrical shape 'U' is made to increase the Section Modulus of the bracket to withstand forces in lateral direction.'U' shaped bracket riveted at the rear side of the mounting tray increases the strength of the joint and to eliminate the welded joint. It has two flanges at both ends in addition to the 'U' shaped bend. The bracket is made of SS-304 grade sheet of 1 mm thickness with proper bending radii and corner relief for minimum stress concentration. Use of stainless steel provides harder bearing area to the locating pin/ dowel pins. The rear side of the mounting tray is formed to its shape with lapping of sheets. The pilot holes of diameter 2.1mm are drilled initially, through which rivets pass, on mounting tray and the 'U' bracket. The bracket is placed at the appropriate position and clamped temporarily, then enlarge the holes to suit to the size of the rivet. Suitable rivets are riveted and complete the joint with suitable head forming tool./p
机译:>航空电子设备安装托盘后端的接头应足够高,以承受振动和冲击负荷,尤其是在避雷器着陆测试中。安装托盘在此侧面带有两个定位销/定位销,总的感应振动或冲击载荷通过该定位销/定位销传递到背面的托盘。总感应力仅集中在这两个销钉上。因此,固定有这些销钉的接头和轴承部件也应具有足够的强度以抵抗即将到来的力,尤其是在避雷器着陆冲击试验中。 “ U”形支架设计用于任何ATR尺寸和非ATR尺寸的航空电子安装托盘,以加强固定它的接头。制成的几何形状“ U”可增加支架的截面模数,以承受横向力。铆接在安装托盘后侧的“ U”形支架可提高接头的强度并消除焊接接头。除“ U”形弯头外,它的两端还有两个法兰。支架由厚度为1 mm的SS-304等级板材制成,具有适当的弯曲半径和拐角释放,以最小化应力集中。使用不锈钢为定位销/定位销提供了更硬的支承区域。安装托盘的后侧通过叠放纸张而形成其形状。首先在安装托盘和“ U”形支架上钻出直径为2.1mm的导向孔,铆钉穿过该导向孔。将支架放置在适当的位置并暂时夹紧,然后扩大孔的大小以适合铆钉的尺寸。铆接合适的铆钉,并使用合适的头部成型工具完成连接。

著录项

  • 公开/公告号IN2013CH05898A

    专利类型

  • 公开/公告日2015-06-26

    原文格式PDF

  • 申请/专利权人 SLRDC HAL;

    申请/专利号IN2013CHE5898

  • 发明设计人 LAKSHMANA KUMAR MATHA;

    申请日2013-12-18

  • 分类号G01D;

  • 国家 IN

  • 入库时间 2022-08-21 15:14:11

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