Turbine stage cooling
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United States of America Patent
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Oct 20, 2020
Grant Date -
Dec 6, 2018
app pub date -
Jun 6, 2018
filing date -
Jun 6, 2014
priority date (Note) -
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Abstract
A turbine injection system for a gas turbine engine includes a first end operable to receive air from a heat exchanger, a second end operable to distribute mixed cooling air to a turbine stage, an opening downstream of said first end and a mixing plenum downstream of said first end and said opening. The opening provides a direct fluid pathway into said turbine injection system.
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