Carlson, Gaskey & Olds, P.C.
Gas turbine engine having section with thermally isolated area
A section of a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a thermally isolated area, and a first rotor disk and a second rotor disk. Each of the first and second rotor disks are provided within the thermally isolated area.
UNITED TECHNOLOGIES CORPORATION
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Gabriel L. James D. Brian D. William K.
Suciu Hill Merry Ackermann