Superconducting Propulsion System with LH2 Cooling for All-Electric Aircraft

被引：17

作者：

Dezhin, D. ^{[1
]}

Dezhina, I ^{[1
]}

Ilyasov, R. ^{[1
]}

机构：

[1] Moscow Aviat Inst NRU, Dept Elect Machines & Power Elect, Moscow, Russia

来源：

14TH EUROPEAN CONFERENCE ON APPLIED SUPERCONDUCTIVITY (EUCAS2019) | 2020年 / 1559卷

关键词：

D O I：

10.1088/1742-6596/1559/1/012143

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

The article discusses the advantages of using liquid hydrogen to cool superconducting electric machines for an all-electric aircraft. Calculation schemes and basic parameters of superconducting electric machines with liquid hydrogen cooling are presented. It is shown that liquid hydrogen is practically a non-alternative type of fuel for future electric aircraft because of its high energy intensity and environmental cleanliness.

引用

页数：5

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