A power and thermal management system for long endurance hypersonic vehicle

被引：0

作者：

Liang GUO ^{[1
]}

Liping PANG ^{[1
]}

Xiaodong YANG ^{[2
]}

Jingquan ZHAO ^{[1
]}

Desheng MA ^{[1
]}

机构：

[1] School of Aeronautic Science and Engineering, Beihang University

[2] Institute of Artificial Intelligence, Beihang University

来源：

Chinese Journal of Aeronautics | 2023年 / 02期

关键词：

Fuel vapor turbine; Hypersonic vehicle; Power and thermal management system; Scramjet; Supercritical carbon dioxide;

D O I：

暂无

中图分类号：

V231 [发动机原理];

学科分类号：

082502 ;

摘要：

Due to the pneumatic heating and combustion effect, the scramjet engine of hypersonic vehicle faces high temperature challenge. It is necessary to comprehensively consider its thermal management and power generation together. A new Power and Thermal Management System(PTMS) combined with Supercritical Carbon Dioxide(SCO2) closed Brayton cycle and fuel vapor turbine is proposed and discussed in this paper. The new PTMS can meet the cooling requirement of hypersonic vehicle at Mach number 6–7, and avoid the coking and scrapping in the scramjet cooling channels. Compared with the PTMS only based on fuel vapor turbine, the new PTMS utilizes the waste heat of scramjet to generate more electricity. In addition, it can reduce the use of fuel sink for cooling, and the additional weight penalty can be compensated for long endurance hypersonic flight.

引用

页码：29 / 40

页数：12

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