ASME_TURBO_EXPO2012_Paper_GT2012-68588_final.pdf (1.61 MB)
Main annulus gas path interactions – turbine stator well heat transfer
chapter
posted on 2023-06-08, 14:01 authored by J A Dixon, A G Valencia, D Coren, D Eastwood, Christopher LongThis 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 AirPublisher
American Society of Mechanical EngineersVolume
4bPage range
68588Book title
Proceedings of the ASME Turbo Expo 2012Place of publication
New York, NYISBN
9780791844670Department affiliated with
- Engineering and Design Publications
Notes
June 11 – 15, 2012, Bella Center, Copenhagen, DenmarkFull text available
- Yes
Peer reviewed?
- Yes
Legacy Posted Date
2012-12-01First Open Access (FOA) Date
2016-03-22First Compliant Deposit (FCD) Date
2016-03-22Usage metrics
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