Performance of a Turbine Rim Seal Subject to Rotationally-Driven and Pressure-Driven Ingestion
Author:
Affiliation:
1. Department of Engineering Science, Oxford Thermofluids Institute, University of Oxford, Oxford OX2 0ES, UK
2. Thermo-Fluid Systems UTC, University of Surrey, Guildford GU2 7XH, UK
3. Rolls-Royce plc, P. O. Box 3, Bristol BS34 7QE, UK
Abstract
Funder
Innovate UK
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/143/8/081025/6702060/gtp_143_08_081025.pdf
Reference23 articles.
1. Turbine Rim Seal Gas Path Flow Ingestion Mechanisms,1994
2. Review of Ingress in Gas Turbines;ASME J. Eng. Gas Turbines Power,2016
3. Flow Mechanisms in Axial Turbine Rim Sealing;Proc. Inst. Mech. Eng. Part C J,2019
4. Aerodynamic Aspects of the Sealing of Gas-Turbine Rotor-Stator Systems: Part 1: The Behavior of Simple Shrouded Rotating-Disk Systems in a Quiescent Environment;Int. J. Heat Fluid Flow,1988
5. Unsteady Flow Phenomena in Turbine Rim Seals;ASME J. Eng. Gas Turbines Power,2017
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1. A theoretical model for ingress through turbine rim seals based on physically-observed unsteadiness;International Journal of Heat and Fluid Flow;2024-04
2. Measurement of Inertial and Acoustic Waves in a Turbine Chute Rim Seal Cavity;Journal of Engineering for Gas Turbines and Power;2023-02-15
3. Flow and Ingestion in a Turbine Disc Cavity under Rotationally-Dominated Conditions;International Journal of Turbomachinery, Propulsion and Power;2021-07-20
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