Carlson, Gaskey & Olds, P.C.
Method and assembly for reducing secondary heat in a gas turbine engine
A turbine section includes a rotor assembly which includes an internal cooling passage. A segmented seal is adjacent the rotor assembly and includes a fluid passage that is in fluid communication with the internal cooling passage.
UNITED TECHNOLOGIES CORPORATION
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Gabriel L. Brian D. Mark F. James D.
Suciu Merry Zelesky Hill