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.
United Technologies Corporation
F F F Y F F F F F F F F
F05D F01D F23R Y02T F01D F02C F02C F05D F01D F05D F05D F02C
additional inventional inventional additional inventional inventional inventional additional inventional additional additional inventional
James D Gabriel L Brian D
Hill Suciu Merry