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作 者:郭婧 何歆 周晨阳 付秋菊 刘伟 王天元 吴宇 GUO Jing;HE Xin;ZHOU Chenyang;FU Qiuju;LIU Wei;WANG Tianyuan;WU Yu(Fundamental Technology Research Department,Hunan Aviation Powerplant Research Institute,Aero Engine Corporation of China,Zhuzhou Hunan 412002,China;Structural Certification Division,Airworthiness Certification Center,Civil Aviation Administration of China,Beijing 100102,China;3D Printing Research and Engineering Technology Center,Beijing Institute of Aeronautical Materials,Aero Engine Corporation of China,Beijing 100095,China)
机构地区:[1]中国航发湖南动力机械研究所基础技术研究部,湖南株洲412002 [2]中国民用航空局适航审定中心结构审定室,北京100102 [3]中国航发北京航空材料研究院3D打印研究与工程技术中心,北京100095
出 处:《航空动力学报》2024年第9期484-490,共7页Journal of Aerospace Power
摘 要:针对民用航空发动机激光选区熔化制件适航符合性验证需求,总结了激光选区熔化技术在航空发动机中的应用现状,分析了激光选区熔化制件适航符合性验证相关参考资料要求,研究了激光选区熔化航空发动机制件适航符合性验证方法。目前,国外已有激光选区熔化航空发动机制件通过了适航审定,而我国在该领域仍处于起步阶段。基于相关参考资料及传统工艺适航符合性验证方法,认为激光选区熔化航空发动机制件的适航符合性验证方法主要应包括:建立激光选区熔化材料规范、认证激光选区熔化工艺、鉴定激光选区熔化成形材料是否合格及确定设计用材料性能。Motivated by the demand of airworthiness compliance of civil aeroengine components fabricated using selective laser melting(SLM)technique,the applications of SLMed aeroengine components were summarized.Additionally,reference related to airworthiness compliance of SLMed components were analyzed.Meanwhile,airworthiness compliance demonstration method of SLMed aeroengine components was investigated.Presently,some SLMed aeroengine components have passed the airworthiness certification in foreign countries.However,China is still in the initial stage in this field.According to the related reference and airworthiness compliance demonstration method of aeroengine components manufactured through traditional processing techniques,the airworthiness compliance demonstration method of SLMed aeroengine components should mainly contain the following parts:establishment of selective laser melted material specifications,certification of selective laser melting process,identification of material quality and determination of material properties.
关 键 词:激光选区熔化 航空发动机 制件 适航 符合性验证方法
分 类 号:V37[航空宇航科学与技术—航空宇航推进理论与工程]
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