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基于CAM/CNC集成的航空大型薄壁件数控加工在机刀轨调整方法
  • ISSN号:1000-6893
  • 期刊名称:《航空学报》
  • 时间:0
  • 分类:V262.33[航空宇航科学与技术—航空宇航制造工程] TG506[金属学及工艺—金属切削加工及机床]
  • 作者机构:南京航空航天大学机电学院,南京210016
  • 相关基金:国家自然科学基金(51375239); 江苏省杰出青年基金(BK20140036)
中文摘要:

航空大型薄壁零件刚性弱,加工过程中易产生超差变形,需要对零件进行在机检测,并将检测数据反馈给CAM系统进行拟合并调整刀轨。以上过程需要在不同部门和系统间进行切换,严重影响了生产效率。针对以上问题,提出了一种基于CAM/CNC集成的航空大型薄壁件数控加工在机刀轨调整方法。建立了CAM/CNC集成框架,并构建了用于CAM/CNC间信息传递的动态特征信息模型,基于CAM系统离线生成特征理论中间状态,基于CNC系统建立特征实际中间状态检测点同理论中间状态的映射关系。通过分析理论厚度和实际厚度,确定特征中间状态的变形情况。针对变形导致特征中间状态加工余量无法包络符合公差要求的最终加工状态的情况,进行在机刀轨调整。基于所提出的方法开发的航空大型薄壁件数控加工在机刀轨调整系统在某大型航空企业得到了应用验证,可有效避免信息的反复传递,减少了工艺人员的重复劳动,提高了生产效率。

英文摘要:

Deformation is easy to occur during the machining process for the large thin-walled aeronautical part,which has bad rigidity.In this case,on-machine inspection is needed.The inspection points are obtained and fed back to CAM system to fit surface and generate new tool path.The information needs to be transmitted between different departments and system platform during the above process,which reduces the productivity.In order to address the issues above,an adjusting method of tool path on machine for the manufacture of large thin-walled aeronautical part based on the integration of CAM and CNC is proposed in this paper.The frame of the integration of CAM and CNC is built and the dynamic feature information model is also built in this method to transmit information between CAM and CNC system.The theoretical interim state of part feature is generated based on the CAM system offline.The deformation of the feature interim state is confirmed based on the mapping relationship between theoretical interim state and the actual interim state,and the comparison for the theoretical and actual thickness in the CNC system.The tool path is adjusted on-machine for the situation that the final machining status conforming to the requirement of the tolerance cannot be enveloped by the machining allowance of the feature interim state.The system based on the adjusting method of tool path on machine for the manufacture of large thin-walled aeronautical part based on the integration of CAM and CNC is verified in an aviation manufacturing corporation.Using the proposed method,the transmission of information is reduced,the intensity of labor for technologist is decreased and the productivity is increased.

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期刊信息
  • 《航空学报》
  • 中国科技核心期刊
  • 主管单位:中国科学技术协会
  • 主办单位:中国航空学会
  • 主编:孙晓峰
  • 地址:北京海淀区学院路37号
  • 邮编:100083
  • 邮箱:hkxb@buaa.edu.cn
  • 电话:010-82317058 82318016
  • 国际标准刊号:ISSN:1000-6893
  • 国内统一刊号:ISSN:11-1929/V
  • 邮发代号:82-148
  • 获奖情况:
  • 国内外数据库收录:
  • 俄罗斯文摘杂志,美国化学文摘(网络版),荷兰文摘与引文数据库,美国工程索引,美国剑桥科学文摘,英国科学文摘数据库,日本日本科学技术振兴机构数据库,美国应用力学评论,中国中国科技核心期刊,中国北大核心期刊(2004版),中国北大核心期刊(2008版),中国北大核心期刊(2011版),中国北大核心期刊(2014版),中国北大核心期刊(2000版)
  • 被引量:24676