中文

Electrochemical machining of blades with cross-structural cathodes at leading/trailing edges

Hits:

  • Affiliation of Author(s):机电学院

  • Journal:INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY

  • Key Words:Electrochemical machining Blade Electric field Simulation Cross-structural cathodes Conventional cathode

  • Abstract:Blades are key components in modern aero engines. Their leading and trailing edges are extremely difficult to machine using electrochemical machining (ECM) because of their small thickness and radius of curvature and their marginal location. Traditional ECM of blades requires gaps between the convex part cathode and concave part cathode at the leading and trailing edges to allow passage of electrolyte. The presence of these gaps may lead to large variations in electric field intensity at the end of the machining process as the leading and trailing edges are forming. This paper proposes a new design of cross-structural cathodes to decrease the dynamic variation of the electric field at marginal locations. A mathematical model of material removal is established, taking account principally of the electric field factor. The forming process of the leading edge is simulated, and changes in electric field intensity during the final stages of the process are analyzed. The simulation results show that the maximum fluctuation in the electric field intensity at the leading edge is 62.42% when a conventional cathode is used, but only 30.51% with cross-structural cathodes. Experiments are conducted to compare the performance of conventional and cross-structural cathodes. The results show that, in comparison with conventional cathodes, the use of cross-structural cathodes reduces variations in machining current in the forming stage of margin profiles and leads to more accurate repeatability of the process.

  • ISSN No.:0268-3768

  • Translation or Not:no

  • Date of Publication:2017-12-01

  • Co-author:Zhao, Jibin,Zhang, Ronghui,Yu, Lingguo

  • Correspondence Author:zd

  • Date of Publication:2017-12-01

Copyright©2018- Nanjing University of Aeronautics and Astronautics·Informationization Department(Informationization Technology Center) Click:
  MOBILE Version

The Last Update Time:..