GAS TURBINE ENGINE WITH ACTIVE VARIABLE TURBINE COOLING
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United States of America
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Issued Date -
Jan 16, 2020
app pub date -
Jul 13, 2018
filing date -
Jul 13, 2018
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Abstract
A gas turbine engine includes a compressor section, a combustor section, and a turbine section operably coupled to the compressor section. A primary flow path is defined through the compressor section, the combustor section, and the turbine section. An engine case surrounds the compressor section, the combustor section, and the turbine section. The gas turbine engine also includes a means for providing an active variable cooling flow through a bypass duct external to the engine case to a secondary flow cavity of the turbine section.
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