University of Sussex
Browse
ASME_TURBO_EXPO2012_Paper_GT2012-68588_final.pdf (1.61 MB)

Main annulus gas path interactions – turbine stator well heat transfer

Download (1.61 MB)
chapter
posted on 2023-06-08, 14:01 authored by J A Dixon, A G Valencia, D Coren, D Eastwood, Christopher Long
This paper summarises the work of a 5-year research programme into the heat transfer within cavities adjacent to the main annulus of a gas turbine. The work has been a collaboration between several gas turbine manufacturers, also involving a number of universities working together. The principal objective of the study has been to develop and validate computer modelling methods of the cooling flow distribution and heat transfer management, in the environs of multi-stage turbine disc rims and blade fixings, with a view to maintaining component and sub-system integrity, whilst achieving optimum engine performance and minimising emissions. A fully coupled analysis capability has been developed using combinations of commercially available and in-house computational fluid dynamics (CFD) and finite element (FE) thermo-mechanical modelling codes. The main objective of the methodology is to help decide on optimum cooling configurations for disc temperature, stress and life considerations. The new capability also gives us an effective means of validating the method by direct use of disc temperature measurements, where otherwise, additional and difficult to obtain parameters, such as reliable heat flux measurements, would be considered necessary for validation of the use of CFD for convective heat transfer. A two-stage turbine test rig has been developed and improved to provide good quality thermal boundary condition data with which to validate the analysis methods. A cooling flow optimisation study has also been performed to support a re-design of the turbine stator well cavity, to maximise the effectiveness of cooling air supplied to the disc rim region. The benefits of this design change have also been demonstrated on the rig. A brief description of the test rig facility will be provided together with some insights into the successful completion of the test programme. Comparisons will be provided of disc rim cooling performance, for a range of cooling flows and geometry configurations. The new elements of this work are the presentation of additional test data and validation of the automatically coupled analysis method applied to a partially cooled stator well cavity, (i.e. including some local gas ingestion); also the extension of the cavity cooling design optimisation study to other new geometries

History

Publication status

  • Published

File Version

  • Published version

Journal

Proceedings of ASME Turbo Expo 2012: Power for Land, Sea and Air

Publisher

American Society of Mechanical Engineers

Volume

4b

Page range

68588

Book title

Proceedings of the ASME Turbo Expo 2012

Place of publication

New York, NY

ISBN

9780791844670

Department affiliated with

  • Engineering and Design Publications

Notes

June 11 – 15, 2012, Bella Center, Copenhagen, Denmark

Full text available

  • Yes

Peer reviewed?

  • Yes

Legacy Posted Date

2012-12-01

First Open Access (FOA) Date

2016-03-22

First Compliant Deposit (FCD) Date

2016-03-22

Usage metrics

    University of Sussex (Publications)

    Categories

    No categories selected

    Exports

    RefWorks
    BibTeX
    Ref. manager
    Endnote
    DataCite
    NLM
    DC