| Download | - View final version: Early development work on thermocouple-slipring instrumentation of Orenda XIV turbine blades (PDF, 4.4 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003918 |
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| Author | Search for: Bannister, John D.1; Search for: Cockshutt, E. Philip1 |
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| Affiliation | - National Research Council Canada. National Aeronautical Establishment
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| Format | Text, Memorandum |
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| Physical description | 23 p. |
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| Abstract | During the period May to September 1957, development work was continued on a thermocouple-slipring system f or measuring turbine blade temperatures on an Orenda XIV two-stage turbine to the state where reasonably consistent results could be obtained from test-bed engine runs. These results revealed that the N.A.E. reheat system cooled the first stage blades a maximum of approximately 140°C in the immediate region of the Impinging reheat fuel· The second stage blades received negligible cooling. |
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| Publication date | 1957-09-17 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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| Identifier | NAE-499 |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 70e6e573-9e70-43ee-83d4-2b846414d0b3 |
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| Record created | 2025-12-01 |
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| Record modified | 2025-12-02 |
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