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带锯齿形叶冠叶片接触应力计算及静强度分析

  • Beihang University
  • Aero Engine Corporation of China

科研成果: 期刊稿件文章同行评审

摘要

The "displacement extraction method" was proposed to calculate the contact stress of the zig-zag shroud contact surface according to the convergent displacement of contact surface. The contact stress can be obtained accurately with the surface mesh size of 0.202mm, and the maximum value was 453.48MPa. The stress level and torsion degree of the shrouded blade under different conditions were analyzed. The stress level increased with the increase of initial installation tightness, and the blade torsion angle increased with the increase of centrifugal load. According to the relationship between the load on the contact surface and the torsion angle, the compressional rigidity and torsional rigidity of blade were obtained. The compressional rigidity was much higher than torsional rigidity, so the stress of blade body restricted the stress of contact surface. It was proposed that the average contact stress of shroud should not be greater than 40% nominal yield limit and the equivalent stress of blade body should not be greater than 75% nominal yield limit as a criterion for the static load strength analysis, and the shrouded blade model of 0.127mm initial installation tightness can meet this strength requirement.

投稿的翻译标题Contact stress calculation and static strength analysis of zig-zag shrouded blade
源语言繁体中文
页(从-至)732-743
页数12
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
35
4
DOI
出版状态已出版 - 1 4月 2020

关键词

  • Contact stress
  • Static strength analysis
  • Tightness of contact surface
  • Turbine blade
  • Zig-zag blade shroud

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