Carlson, Gaskey & Olds, P.C.
Turbine stage cooling
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.
Raytheon Technologies Corporation
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Gabriel L. Brian D. James D.
Suciu Merry Hill