Estimation of gas turbine blades cooling efficiency

A.B. Moskalenko, A. Kozhevnikov

Research output: Contribution to journalArticleAcademicpeer-review

8 Citations (Scopus)
362 Downloads (Pure)

Abstract

This paper outlines the results of the evaluation of the most thermally stressed gas turbine elements, first stage power turbine blades, cooling efficiency. The calculations were implemented using a numerical simulation based on the Finite Element Method. The volume average temperature of the blade and the coefficient of heat transfer from the cooling medium to the cooling channel wall were chosen as the cooling efficiency criteria. A comparison of steam and air used as coolants was done, and the calculations were performed using ANSYS Fluent software.
Original languageEnglish
Pages (from-to)61-67
Number of pages7
JournalProcedia Engineering
Volume150
DOIs
Publication statusPublished - 2016
Event2nd International Conference on Industrial Engineering (ICIE-2016), 25-26 Januari 2016, Teheran, Iran - Tehran, Iran, Islamic Republic of
Duration: 25 Jan 201626 Jan 2016
http://icie.aconf.org/

Keywords

  • gas turbine blade; cooling efficiency; CFD; thermal analysis; thermal stresses

Fingerprint Dive into the research topics of 'Estimation of gas turbine blades cooling efficiency'. Together they form a unique fingerprint.

  • Cite this