Thermal Protection System and Thermal Management for Combined-Cycle Engine: Review and Prospects

被引：13

作者：

Dong, Yiwei ^{[1
,2
]}

Wang, Ertai ^{[1
]}

You, Yancheng ^{[1
]}

Yin, Chunping ^{[1
]}

Wu, Zongpu ^{[1
]}

机构：

[1] Xiamen Univ, Sch Aerosp Engn, 422 South Siming Rd, Xiamen 361005, Peoples R China

[2] Xiamen Univ, Shenzhen Res Inst, 19 Gaoxin South 4th Rd, Shenzhen 518057, Peoples R China

来源：

ENERGIES | 2019年 / 12卷 / 02期

基金：

中国国家自然科学基金;

关键词：

hypersonic aircraft; combined-cycle propulsion; thermal management; thermal protection; HEAT-TRANSFER; STARTING CHARACTERISTICS; NUMERICAL-SIMULATION; HYPERSONIC VEHICLES; STRUCTURAL ANALYSIS; OXIDATION BEHAVIOR; BARRIER COATINGS; STRUT INJECTOR; LEADING-EDGE; SCRAMJET;

D O I：

10.3390/en12020240

中图分类号：

TE [石油、天然气工业]; TK [能源与动力工程];

学科分类号：

0807 ; 0820 ;

摘要：

Combined-cycle engine is a potential propulsion system for hypersonic aircraft. To ensure long-term, normal operation of combined-cycle engine under the harsh environment of high thermal load, it is of great significance to study the thermal protection and management of the propulsion system. In this study, the objective and development status of thermal protection and thermal management systems for the combined-cycle propulsion system were described. The latest research progresses of thermal protection, thermal barrier coating, and thermal management system of the combined-cycle propulsion system were summarized. Moreover, the problems and shortcoming in current researches were summarized. In addition, a prospect for the future development of thermal protection and management of the combined-cycle propulsion system was presented, pointing out a direction of great value and vital research significance to thermal protection and management of the combined-cycle propulsion system.

引用

页数：51

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