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A ROBUST RADIAL TRAVERSE TEMPERATURE PROBE FOR APPLICATION TO A GAS TURBINE HP/IP STAGE

Abstract:

The requirements to reduce engine fuel burn costs and gaseous emissions combine to ensure that gas turbine engine manufacturers continually seek to increase the peak cycle temperatures of new engine designs. Consequently, high-pressure turbine components must be developed that can withstand increasing gas temperatures, resulting in the continuous introduction of new technologies that allow appropriate service life. Accurate gas path measurements are vital for early understanding of the perfor...

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Publication status:
Published

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Publisher copy:
10.1115/GT2012-68331

Authors


Wilson, AJW More by this author
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Institution:
University of Oxford
Department:
Oxford, MPLS, Engineering Science
Stevenson, R More by this author
Thorpe, SJ More by this author
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Journal:
PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 1
Volume:
1
Pages:
63-71
Publication date:
2012
DOI:
URN:
uuid:c4764c57-94df-4153-8901-b95c5234cad2
Source identifiers:
418028
Local pid:
pubs:418028
Language:
English

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