摘要
为了研究3D打印制造技术在固体火箭发动机领域的应用可行性,以某典型铣削制造难加工的固体火箭发动机用金属支撑构件为研究对象,在制备技术、基础性能、效率对比、结构轻质化、使用性能等方面进行了研究,获得了3D打印制造TC4构件的性能数据、数值分析结果及实现工程应用的研究路径。较传统铣削制造工艺,3D打印构件不仅可满足工程应用要求,还可协同结构优化设计,实现制备效率提升50%、轻质化结构最大减重13.6%及最大拉力达63.9kN,为难加工、复杂零件的轻质化高效成型提供了新的途径,值得进一步深入系统研究。
In order to study the feasibility of the application of 3D printing manufacturing technology on solid rocket motor(SRM),a typical milling to manufacture difficult-to-process metal support components for SRM was studied.The preparation techniques,basic performance,efficiency comparison,structure weight-lightening,use performance and other aspects were studied.The performance data,numerical analysis results and engineering application research path of a TC4 component manufactured by 3D printing were obtained.Compared with the traditional milling manufacturing process,3D printed components can not only meet the requirements of engineering applications,but also cooperate with structural optimization design,achieving a 50%increase in manufacturing efficiency,a maximum weight reduction of 13.6%and a maximum tension of 63.9kN for lightweight structures.It provides a new way for the lightweight and efficient molding of difficult and complex parts to process,which is worthy of further in-depth systematic research.
作者
赵勇
林峰
田银俊
ZHAO Yong;LIN Feng;TIAN Yin-jun(China Aerospace Science and Industry Power Technology Academy,Hohhot 010010,China;Departmengt of Mechanical Engineering,Tsinghua University,Beijing 100084,China;Key Laboratory for Advanced Materials Processing Technology,Ministry of Education of China,Tsinghua University,Beijing 100084,China)
出处
《推进技术》
EI
CAS
CSCD
北大核心
2022年第12期271-279,共9页
Journal of Propulsion Technology
