航空学报2025，Vol.46Issue(5)：33-44,12.DOI:10.7527/S1000-6893.2025.31745
飞行包线内空气换热器能力边界研究及进展
Research progress on performance boundary of air heat exchanger within flight envelope
摘要
Abstract
Understanding the heat transfer limits of heat exchangers for aero-engines within the flight envelope and ex-panding their performance boundaries are critical measures to advance aero-engines toward higher thrust-to-weight ra-tios.This paper focuses on the design requirements of heat exchangers used in cooled cooling air technology.First,the structures of typical air heat exchangers in aero-engines and novel heat exchanger structures with promising appli-cations are reviewed.Then,the method for analyzing and expanding the performance boundaries of heat exchangers within the flight envelope is proposed to ensure the stable and efficient operation of the aero-engines under complex working conditions.The performance boundary range of non-uniformly arranged serpentine tube heat exchangers is also provided.Subsequently,the existing heat exchanger performance evaluation methods are reviewed,and the comprehensive performance evaluation plot for aero-engine heat exchangers is developed.Finally,the development prospects of air heat exchangers for aero-engines are discussed.关键词
航空发动机/换热器/飞行包线/性能评价/冷却冷却空气Key words
aero-engine/heat exchanger/flight envelope/performance evaluation/cooled cooling air分类
航空航天引用本文复制引用
何雅玲,姜涛,杜燊,徐国强..飞行包线内空气换热器能力边界研究及进展[J].航空学报,2025,46(5):33-44,12.基金项目
国家科技重大专项(J2019-Ⅲ-0021-0065) （J2019-Ⅲ-0021-0065）
陕西省重点研发专项计划(2022GXLH-01-04) National Science and Technology Major Project of China(J2019-Ⅲ-0021-0065) （2022GXLH-01-04）
The Key R&D Special Program of Shaanxi Province(2022GXLH-01-04) （2022GXLH-01-04）
