The Manufacturing and Experimental Validation of a Nickel Superalloy Double-Wall, Effusion Test Specimen

Alexander V. Murray, Peter T. Ireland, Nick R. Green, Michael Wickins, Richard Hood, Janendra Telisinghe

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

Abstract

With the hot stage of a modern aeroengine operating with combustor firing temperatures well beyond the melting point of the nickel superalloys from which the turbine blades are manufactured, developments to the methods of cooling of these components are required to advance performance. Double-wall, effusion systems exhibit a quasi-transpiration like cooling effect with recent work demonstrating their exceptional cooling performance. Such systems are characterised by two walls, one with impingement holes and the other with film cooling holes, that are mechanically and thermally connected via pedestals. However, manufacturing such geometries from single crystal nickel superalloys remains a significant barrier to entry into service.


This paper presents a method of manufacturing double-wall effusion specimens from a nickel superalloy commonly used in modern commercial high pressure turbine components. The method maintains the mechanical integrity associated with nickel superalloys. Details of the method are presented alongside x-ray and GOM laser scan data of a flat-plate test article that demonstrates the success of the manufacturing process. Aerothermal testing of the specimen in a bespoke recirculating wind-tunnel facility was undertaken in which the overall cooling effectiveness of the system is obtained. The results reaffirm the excellent cooling performance of double-wall, effusion systems and further validate the manufacturing methodology as a method by which to realise enhanced cooling effectiveness in service.

Original languageEnglish
Title of host publicationTurbo Expo: Power for Land, Sea and Air
Subtitle of host publicationVolume 8: Industrial and Cogeneration; Manufacturing Materials and Metallurgy
PublisherAmerican Society of Mechanical Engineers (ASME)
Volume8
ISBN (Electronic)9780791887028
DOIs
Publication statusPublished - 28 Sept 2023
EventASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition, GT 2023 - Boston, United States
Duration: 26 Jun 202330 Jun 2023

Publication series

NameProceedings of the ASME Turbo Expo
Volume8

Conference

ConferenceASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition, GT 2023
Country/TerritoryUnited States
CityBoston
Period26/06/2330/06/23

Bibliographical note

Funding Information:
The authors would like to express their thanks for the on-going support provided by the EPSRC Transpiration Cooling grant (EP/P000878/1) and by Rolls-Royce plc. The authors

Funding Information:
The authors would like to express their thanks for the ongoing support provided by the EPSRC Transpiration Cooling grant (EP/P000878/1) and by Rolls-Royce plc. The authors would also like to thank the technicians and staff at the High Temperature Research Centre, University of Birmingham and the Oxford Thermofluids Institute, University of Oxford.

Publisher Copyright:
Copyright © 2023 by ASME.

ASJC Scopus subject areas

  • General Engineering

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