公开(公告)号：US20180149085A1

公开(公告)日：2018-05-31

申请号：US15362202

申请日：2016-11-28

Applicant: General Electric Company

Inventor： Veerraju Chennoju ,  Debabrata Mukhopadhyay ,  Rohit Pruthi

IPC: F02C7/18

CPC classification number: F02C7/18 ,  F01D9/065 ,  F01D25/125 ,  F01D25/162 ,  F01D25/30 ,  F05D2260/232

Abstract: This application provides exhaust frame cooling systems for use with gas turbine engines. Example systems may include an exhaust system for use with a gas turbine engine. The exhaust system may include a strut positioned between an inner barrel and an outer barrel. The strut may include an inner body and an outer body. The exhaust system may include at least one strut hole formed in the inner body, where the at least one strut hole forms a first cooling path for cooling flow in a first direction, a cavity between the inner body and the outer body, where the cavity forms a second cooling path for the cooling flow in a second direction, and a purge outlet to purge the cooling flow at the inner barrel.

公开(公告)号：US11761347B2

公开(公告)日：2023-09-19

申请号：US18148504

申请日：2022-12-30

Applicant: General Electric Company

Inventor： Mithun Raj K K ,  Veerraju Chennoju

IPC: F01D25/12 ,  F01D25/14 ,  F01D9/06 ,  F01D25/28

CPC classification number: F01D25/125 ,  F01D9/065 ,  F01D25/14 ,  F01D25/28 ,  F05D2220/32 ,  F05D2260/232 ,  F05D2260/60 ,  F05D2270/303

Abstract: The present application provides an exhaust frame differential cooling system of a gas turbine engine to mitigate a temperature differential along a compressor and/or a turbine to minimize centerline eccentricity of a shaft. The exhaust frame differential cooling system may include a number of compressor temperature sensors positioned about the compressor and/or a number of turbine temperature sensors positioned about the turbine, an exhaust frame including an inner barrel with a bearing tunnel for the shaft, an outer barrel, and a number of struts extending from the inner barrel to the outer barrel, a blower, and a cooling air metering system that provides cooling air from the blower to the bearing tunnel and through the inner barrel, the struts, and the outer barrel in response to the temperature differential being determined along the compressor and/or the turbine.