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飞机机翼微小创伤修复模具的设计

范文学 李宗学 李林喜 王东辉

现代电子技术Issue(2):26-28,3.
现代电子技术Issue(2):26-28,3.

飞机机翼微小创伤修复模具的设计

Design of repairing mould for minor trauma of Aircraft wing

范文学 1李宗学 2李林喜 2王东辉2

作者信息

  • 1. 内蒙古工业大学 矿业学院,内蒙古 呼和浩特 010051
  • 2. 内蒙古工业大学 工程训练中心,内蒙古 呼和浩特 010051
  • 折叠

摘要

Abstract

An easy,economic and accurate micro-knocking repairing method that the micro trauma in aircraft wing crashed by the bird is quickly repaired by precise pad mould is put forward. The important step of method is to design the pad mould, so the repairing principle of the aircraft wing micro trauma is analyzed. Three repairing plans are proposed and their advantages and disadvantages are compared. The laminated wood was selected as material of pad mould,three-coordinate measuring instru-ment was used as a tool of data acquisition,and CNC milling and grinder were used as processing equipments,by which the pad mould design was achieved. The practical application proves that method is able to meet the repair requirements.

关键词

机翼修复/模具设计/逆向工程/衬模

Key words

repair of aircraft wing/mould design/reverse engineering/pad mould

分类

信息技术与安全科学

引用本文复制引用

范文学,李宗学,李林喜,王东辉..飞机机翼微小创伤修复模具的设计[J].现代电子技术,2014,(2):26-28,3.

基金项目

内蒙古工业大学科学研究项目(X201239) (X201239)

现代电子技术

OA北大核心CSTPCD

1004-373X

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