Crimped insert for improved turbine vane internal cooling
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United States of America Patent
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Jan 30, 2018
Issued Date -
N/A
app pub date -
Jan 9, 2015
filing date -
Jan 9, 2015
priority date (Note) -
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Abstract
An insert tube of a turbine vane is disclosed. The insert tube includes a pressure side wall, a suction side wall opposite and spaced apart from the pressure side wall, a leading edge, and a trailing edge opposite the leading edge. The insert tube includes a plurality of cooling channels spaced along the pressure side wall. The insert tube includes an indented portion located between the trailing edge and the pressure side wall.
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