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Heat transferring design for the first guide blade of a high pressure turbine

Research output: Contribution to journalArticlepeer-review

Abstract

Based on Matlab heat transferring program and combined with CFX three-dimensional temperature field of thermal conductivity for calculation, included design of pipe network computing plan and three dimensional heat transferring calculation, a guiding blade of high pressure turbine is researched and the cooling structure is designed according to the characteristics of the guiding blade. A high temperature zone about 1 700 K appears on the blade, but the average temperature is about 1300 K, because the trailing edge vortex cooling structure enhances heat transfer coefficient. A good cooling structure design and verifying calculation of temperature distribution in 3 D can be completed on the cooling structure design platform.

Original languageEnglish
Pages (from-to)42-46
Number of pages5
JournalHarbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology
Volume45
Issue number9
StatePublished - Sep 2013

Keywords

  • Cooling structure
  • Guiding blade
  • Heat transferring calculation
  • Temperature
  • Turbine

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