Gas turbine engine having section with thermally isolated area

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United States of America Patent

PATENT NO 9920652
SERIAL NO

14617339

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Abstract

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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.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Ackermann, William K East Hartford, US 102 891
Hill, James D Tolland, US 92 927
Merry, Brian D Andover, US 208 3607
Suciu, Gabriel L Glastonbury, US 577 7464

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