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Analysis for fracture characteristic of pre-cracked directionally solidified turbine blades

  • The First Inst. Air Force

Research output: Contribution to journalArticlepeer-review

Abstract

Based on the numerical simulation of fracture toughness of the compact tensile (CT) specimen, a numerical model for the stress intensity factor of turbine blades was established by use of MSC. MARC software. The stress intensity factor of pre-cracked turbine blades was evaluated for the fracture state of blades. The fracture toughness of blades shows great scatter, and some of them are remarkably lower than that obtained in material testing. The simulation results of failure blade under operating condition show that the characteristic in fracture section, i.e. the area of fatigue zone is small while that of the instantaneous fracture zone is large.

Original languageEnglish
Pages (from-to)89-92
Number of pages4
JournalTuijin Jishu/Journal of Propulsion Technology
Volume29
Issue number1
StatePublished - Feb 2008

Keywords

  • Aircraft engine
  • Directional solidification
  • Fracture toughness
  • Stress-intensity factor
  • Turbine blade

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