Isothermal compressed air system for internal channel cooling

Amin Safi, Emad Elnajjar, Mohammad Hamdan

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The objective of the current experimental study is to build a system that can provide a steady state mass flow rate of air and constant temperature which will be used for cooling system of gas turbine blade. The compressed air is used as air supply for jet impingement in a rotating test model. The system is capable to provide 200 l/min of compressed air at constant temperature for a period of 50 minutes at 4 bar pressure. Three different designs have been tested with different tanks arrangements. Three tanks with total volume of 2 m2 where used to produce the compressed air conditions.

Original languageEnglish
Title of host publication2019 Advances in Science and Engineering Technology International Conferences, ASET 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781538682715
DOIs
Publication statusPublished - May 14 2019
Event2019 Advances in Science and Engineering Technology International Conferences, ASET 2019 - Dubai, United Arab Emirates
Duration: Mar 26 2019Apr 10 2019

Publication series

Name2019 Advances in Science and Engineering Technology International Conferences, ASET 2019

Conference

Conference2019 Advances in Science and Engineering Technology International Conferences, ASET 2019
Country/TerritoryUnited Arab Emirates
CityDubai
Period3/26/194/10/19

Keywords

  • cooling system
  • gas turbine blade
  • isothermal compressed air
  • steady state condition

ASJC Scopus subject areas

  • Electronic, Optical and Magnetic Materials
  • Artificial Intelligence
  • Computer Networks and Communications
  • Energy Engineering and Power Technology
  • Civil and Structural Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering
  • Ceramics and Composites

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