首页 | 本学科首页   官方微博 | 高级检索  
     检索      

航天高强不锈钢LMD成形缺陷分析及控制
引用本文:周亚雄,吴晓明,杨欢庆,雷钥.航天高强不锈钢LMD成形缺陷分析及控制[J].火箭推进,2022,48(1):90-96.
作者姓名:周亚雄  吴晓明  杨欢庆  雷钥
作者单位:西安航天发动机有限公司,陕西西安710100
基金项目:民用航天技术预先研究项目
摘    要:为明晰航天高强不锈钢激光熔化沉积成形过程基础科学问题,推动其在航天液体火箭发动机领域的应用进程,针对航天高强不锈钢LMD成形过程中常见表面焊瘤、气孔、熔合不良等缺陷的形貌特征及产生机理进行深入分析,并提出对应的控制措施:通过优化边框扫描速度促进熔覆道的流动变形,极大减少了成形件侧表面及倾斜面的焊瘤缺陷; 使用PREP方...

关 键 词:激光熔化沉积  高强不锈钢  缺陷类型  控制措施

Defect analysis and control in aerospace high strength stainless steel by laser melting deposition
ZHOU Yaxiong,WU Xiaoming,YANG Huanqing,LEI Yue.Defect analysis and control in aerospace high strength stainless steel by laser melting deposition[J].Journal of Rocket Propulsion,2022,48(1):90-96.
Authors:ZHOU Yaxiong  WU Xiaoming  YANG Huanqing  LEI Yue
Institution:(Xi'an Aeropsace Engine Co., Ltd., Xi'an 710100,China)
Abstract:In order to clarify the basic scientific problems of laser melting deposition forming process of aerospace high strength stainless steel,to promote its application in the field of aerospace liquid rocket engine,the defect types and mechanism of aerospace high strength stainless steel by laser melting deposition were analyzed.Besides,the corresponding control measures were put forward.First,the flow deformation of cladding channel was promoted by optimizing the scanning speed of border,the defects of weld nodules on the side surface and inclined surface of the formed part are greatly reduced.Second,the PREP method of powder preparation was used instead of the current GA method,the porosity of the formed specimen was reduced to less than 0.1%,and the stomatal defects were basically eliminated.Finally,the method of increasing the"layer remelting capacity"and decreasing the"gully"height between adjacent cladding channels was adopted,the defects of bad internal fusion were eliminated.
Keywords:laser melting deposition  high strength stainless steel  defect type  control measures
本文献已被 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号