Table of Contents

ABSTRACT
INTRODUCTION
TURBINE RIM SEALING
ROTATING CAVITY FLOWS
COMPRESSOR STATOR WELL HEATING
TURBINE COOLING AIR PRE-SWIRL FLOW
COMPRESSOR DRIVE CONE CAVITY FLOW
CONCLUSIONS
ACKNOWLEDGEMENTS
REFERENCES

Abstract

Proceedings of ASME TURBO EXPO 2002, June 3-6, 2002, Amsterdam, The Netherlands (GT-2002-30479) The Internal Cooling Air Systems for Gas Turbines (ICAS-GT) research programme, sponsored by the European Commission, ran from January 1998 to December 2000, and was undertaken by a consortium of ten gas turbine manufacturing companies and four universities. Research was concentrated in five discrete but related areas of the air system including turbine rim seals, rotating cavity flow and heat transfer, and turbine pre-swirl system effectiveness. In each case, experiments were conducted to extend the database of pressure, temperature, flow and heat transfer measurements to engine representative non-dimensional conditions. The data was used to develop correlations, and to validate CFD and FE calculation methods, for internal fluid flow and heat transfer. This paper summarises the outcome of the project by presenting a sample of experimental results from each technical work package. Examples of the associated CFD calculations are included to illustrate the progress made in developing validated tools for predicting rotating cavity flow and heat transfer over an engine representative range of flow conditions.

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Published
Document Type	Standard
Status	Current
Publisher	American Society of Mechanical Engineers
Pages
ISBN