Invention Grant
- Patent Title: Gas turbine engine having section with thermally isolated area
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Application No.: US14617339Application Date: 2015-02-09
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Publication No.: US09920652B2Publication Date: 2018-03-20
- Inventor: Gabriel L. Suciu , William K. Ackermann , James D. Hill , Brian D. Merry
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Hartford
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D25/14
- IPC: F01D25/14 ; F01D5/08 ; F01D25/12
Abstract:
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.
Public/Granted literature
- US20160230597A1 GAS TURBINE ENGINE HAVING SECTION WITH THERMALLY ISOLATED AREA Public/Granted day:2016-08-11
Information query
