航天器通风结构激光选区熔化成形技术研究
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  • 英文篇名:Research on Selective Laser Melting Technology of Spacecraft Ventilation Structure
  • 作者:王震 ; 巩维艳 ; 祁俊峰 ; 赵长喜
  • 英文作者:Wang Zhen;Gong Weiyan;Qi Junfeng;Zhao Changxi;Beijing Spacecrafts Co., Ltd.;
  • 关键词:铝合金 ; 薄壁 ; SLM ; 3D打印
  • 英文关键词:aluminium alloy;;thin-wall;;selective laser melting;;3D printing
  • 中文刊名:HTGY
  • 英文刊名:Aerospace Manufacturing Technology
  • 机构:北京卫星制造厂有限公司;
  • 出版日期:2018-10-25
  • 出版单位:航天制造技术
  • 年:2018
  • 期:No.211
  • 基金:国防基础科研计划项目(JCKY2016606C010);; “十三五”装备预研共用技术课题(41423030516)
  • 语种:中文;
  • 页:HTGY201805001
  • 页数:4
  • CN:05
  • ISSN:11-4763/V
  • 分类号:5-7+13
摘要
分析了目前航天器中薄壁铝合金通风结构在传统加工工艺过程中存在的问题。基于激光选区熔化成形技术(SLM)开展了薄壁铝合金通风结构的3D打印技术研究。研究分析了航天器薄壁结构SLM成形的工艺性、成形工艺支撑设计和成形工艺过程控制,总结了薄壁铝合金结构SLM成形的技术要点。结合我国航天器产品结构特点和发展趋势,对SLM技术的应用研究提出几点建议。
        The problems of thin-walled aluminium alloy ventilation structure in spacecraft are analyzed. 3D printing of thin-walled aluminium alloy ventilation structure was studied based on selective laser melting(SLM) technology. The technological properties, supporting design and the control of forming process are studied about thin-walled aluminium alloy structure of spacecraft, and the main technical points of SLM are summarized. According to the structral characteristics and development of China aerospace products, the suggestions for application of SLM are put forward.
引文
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