公开(公告)号：US09638104B2

公开(公告)日：2017-05-02

申请号：US14262970

申请日：2014-04-28

Applicant: INDUSTRY-ACADEMIC COOPERATION FOUNDATION YONSEI UNIVERSITY

Inventor： Hyung Hee Cho ,  Kyung Min Kim ,  Ho Kyu Moon ,  Beom Seok Kim ,  Jun Su Park ,  Seon Ho Kim

IPC: F02C7/18 ,  F02C7/16 ,  F02C7/12 ,  F02C1/08 ,  F02C6/18 ,  F23M5/08 ,  F23R3/00

CPC classification number: F02C7/18 ,  F02C1/08 ,  F02C6/18 ,  F02C7/12 ,  F02C7/16 ,  F05D2210/14 ,  F23M5/08 ,  F23R3/005

Abstract: The present invention relates to a gas turbine device using a supercritical fluid as a cooling fluid, the gas turbine device having a compressor for compressing air, a combustor for burning the air emitted from the compressor and fuel, and a turbine driven by the burned gas emitted from the combustor, wherein the gas turbine device includes cooling passages formed in the combustor and the turbine, along which the supercritical fluid as a cooling fluid flows to allow the combustor and the turbine to be cooled.