• DocumentCode
    523708
  • Title

    Research on Cutting Temperature Using FEM Method while Machining Titanium Alloy TC4

  • Author

    Liu Dong ; Chen Wuyi ; Shi Rui

  • Author_Institution
    Coll. of Mech. Electron. & Eng., North China Univ. of Technol., Beijing, China
  • Volume
    2
  • fYear
    2010
  • fDate
    11-12 May 2010
  • Firstpage
    1130
  • Lastpage
    1133
  • Abstract
    Titanium alloys are widely used in aerospace industry due to their excellent mechanical properties. Because of their low thermal conductivity, high chemical activity, large friction coefficient and so on, such problems occur during the cutting process as high cutting temperature, large specific cutting force and serious tool wear, leading to low machining efficiency. The titanium alloys classified as difficult machining materials. The finite element method is the new method to study the machining process. The FEM method was used to simulate the cutting temperature while machining titanium alloy TC4. The temperature of cutting zone was measured by natural thermocouple and compared with the simulated results.
  • Keywords
    aerospace industry; cutting; finite element analysis; friction; machining; thermal conductivity; thermocouples; titanium alloys; wear; FEM method; TiJk; aerospace industry; chemical activity; cutting force; cutting temperature; finite element method; friction coefficient; machining; thermal conductivity; thermocouple; titanium alloy TC4; tool wear; Aerospace industry; Chemical processes; Conducting materials; Friction; Machining; Mechanical factors; Temperature; Thermal conductivity; Thermal force; Titanium alloys; FEM method; cutting temperature; natural thermocouple; titanium alloys;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Computation Technology and Automation (ICICTA), 2010 International Conference on
  • Conference_Location
    Changsha
  • Print_ISBN
    978-1-4244-7279-6
  • Electronic_ISBN
    978-1-4244-7280-2
  • Type

    conf

  • DOI
    10.1109/ICICTA.2010.270
  • Filename
    5522900