A ROBUST RADIAL TRAVERSE TEMPERATURE PROBE FOR APPLICATION TO A GAS TURBINE HP/IP STAGE
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 increasi...
| Main Authors: | , , , , , |
|---|---|
| Format: | Journal article |
| Language: | English |
| Published: |
2012
|