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 language | English |
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Title of host publication | Turbo Expo: Power for Land, Sea and Air |
Subtitle of host publication | Volume 8: Industrial and Cogeneration; Manufacturing Materials and Metallurgy |
Publisher | American Society of Mechanical Engineers (ASME) |
Volume | 8 |
ISBN (Electronic) | 9780791887028 |
DOIs | |
Publication status | Published - 28 Sept 2023 |
Event | ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition, GT 2023 - Boston, United States Duration: 26 Jun 2023 → 30 Jun 2023 |
Publication series
Name | Proceedings of the ASME Turbo Expo |
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Volume | 8 |
Conference
Conference | ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition, GT 2023 |
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Country/Territory | United States |
City | Boston |
Period | 26/06/23 → 30/06/23 |
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