推进技术 ›› 1995, Vol. 16 ›› Issue (2): 36-39.

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传热对叶尖间隙的影响

王宝官,李玲   

  1. 南京航空航天大学动力工程系;南京航空航天大学动力工程系
  • 发布日期:2021-08-15

A STUDY IN EFFECT OF HEAT TRANSFER ON BLADE-TIP-CLEARANCE

  1. Dep. of Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing,210016;Dep. of Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing,210016
  • Published:2021-08-15

摘要: 分析了影响叶尖间隙的诸因素,提出了计算瞬变状态下叶尖间隙变化的方法,并以某发动机为例,计算出一级压气机在不同工况下的间隙量,给出了间隙随时间变化的曲线图。

关键词: 压气机部件;叶尖间隙;热应力;热膨胀分析

Abstract: Transient clearances at blade tips are discussed, which transient rotational speeds, thermal parameters,physical parameters, geometrical parameters,etc. Among of these, the main effects are thermal expansion and centrifugal extension.With a series of calculations, a variation map of the clearance along with time has been drawn.

Key words: Compressor part;Blade tip clearance;Thermal stress;Thermal expansion analysis