High temperature heat exchanger studies for applications to gas turbines

被引：110

作者：

Min, June Kee ^{[2
]}

Jeong, Ji Hwan ^{[1
]}

Ha, Man Yeong ^{[1
]}

Kim, Kui Soon ^{[3
]}

机构：

[1] Pusan Natl Univ, Sch Mech Engn, Pusan 609735, South Korea

[2] Pusan Natl Univ, Rolls Royce Univ Technol Ctr, Pusan 609735, South Korea

[3] Pusan Natl Univ, Dept Aerosp, Pusan 609735, South Korea

来源：

HEAT AND MASS TRANSFER | 2009年 / 46卷 / 02期

关键词：

CREEP-RESISTANCE; ADVANCED ALLOYS; HIGH-EFFICIENCY; AEROENGINES; COMPACT; DESIGN; PERFORMANCE;

D O I：

10.1007/s00231-009-0560-3

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

Growing demand for environmentally friendly aero gas-turbine engines with lower emissions and improved specific fuel consumption can be met by incorporating heat exchangers into gas turbines. Relevant researches in such areas as the design of a heat exchanger matrix, materials selection, manufacturing technology, and optimization by a variety of researchers have been reviewed in this paper. Based on results reported in previous studies, potential heat exchanger designs for an aero gas turbine recuperator, intercooler, and cooling-air cooler are suggested.

引用

页码：175 / 186

页数：12

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