Invention Grant
- Patent Title: Method and assembly for reducing secondary heat in a gas turbine engine
-
Application No.: US14844082Application Date: 2015-09-03
-
Publication No.: US10077666B2Publication Date: 2018-09-18
- Inventor: Gabriel L. Suciu , Brian D. Merry , James D. Hill , Mark F. Zelesky
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D5/08 ; F01D11/00 ; F02C3/08 ; F01D5/06
Abstract:
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.
Public/Granted literature
- US20160084090A1 METHOD AND ASSEMBLY FOR REDUCING SECONDARY HEAT IN A GAS TURBINE ENGINE Public/Granted day:2016-03-24
Information query
