Turbine Wheel Relative Temperature at Freerun Conditions

921949

10/01/1992

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
Analytical predictions and laboratory measurements were made for the relative total temperature experienced at the tip diameter of a radial-inflow turbine used in an air turbine starter (ATS). The predictions showed that at freerun conditions the blade tip temperature would be significantly higher than the turbine inlet temperature. Tests to confirm this prediction were performed on an ATS modified to accept an optical pyrometer. The pyrometer was focused on the suction side of the blade at the tip radius. Blade temperature measurements conducted at the maximum attainable speed of the ATS verified the prediction to be within the error of the pyrometer measuring system.
Meta TagsDetails
DOI
https://doi.org/10.4271/921949
Pages
10
Citation
Mathis, D., "Turbine Wheel Relative Temperature at Freerun Conditions," SAE Technical Paper 921949, 1992, https://doi.org/10.4271/921949.
Additional Details
Publisher
Published
Oct 1, 1992
Product Code
921949
Content Type
Technical Paper
Language
English