自然杂志 ›› 2017, Vol. 39 ›› Issue (2): 79-86.

• 特约专稿 •    下一篇

计算机模拟技术在航空发动机涡轮叶片制造中的应用

  

  1. 清华大学材料学院,北京 100084
  • 收稿日期:2016-11-08 修回日期:2016-12-08 出版日期:2017-04-25 发布日期:2017-05-17
  • 通讯作者: 许庆彦,通信作者,E-mail: scjxqy@mail.tsinghua.edu.cn
  • 作者简介:柳百成,中国工程院院士,研究方向:材料加工工程、集成计算材料工程等

Application of computer simulation technology in turbine blades of aero engines manufacturing

  1. School of Materials Science and Engineering, Tsinghua University, Beijing 100084, China
  • Received:2016-11-08 Revised:2016-12-08 Online:2017-04-25 Published:2017-05-17

摘要:

航空发动机涡轮叶片结构复杂,制造工艺繁琐,在高温高压环境下服役需要使用特殊的材料——单晶高温合金。随着叶片几何结构的日趋复杂(如空心、薄壁等),单纯依靠经验和实验进行叶片研制和工艺开发已经落后于时代的要求,而模拟仿真技术不仅能够计算凝固过程中的各项参数,极大地丰富研发手段,而且能够精准、高效、可视化地分别针对缺陷、性能进行预测和优化,从而达到工艺-组织-性能相耦合的多尺度、全流程模拟的目标。

关键词: 航空发动机, 单晶叶片, 模拟仿真, 工艺优化

Abstract:

Single crystal superalloy is widely used in the turbin blades of aero engines due to its outstanding mechanical properties under extreme conditions, such as high temperature and pressure. The traditional research and developing methods can’t meet the needs for the modern blades with more complicated structure. The situation became to change with the advent of numerical simulation technique. Various field distributions during solidification can be calculated based on the numerical simulation, so as to predict casting defects, mechanical properties and help to optimize the manufacturing process. This can lead to the full coupling of process-structureproperty and fulfill its goal of multi-scale, through-process simulation.

Key words: aero-engine, single crystal turbine blade, numerical simulation, process optimization