航空学报 > 2025, Vol. 46 Issue (16): 231682-231682   doi: 10.7527/S1000-6893.2025.31682

固体力学与飞行器总体设计

机载液氢燃料储供系统发展现状与展望

朱斌1,2, 杨少柒1, 郭梁1,2, 贾启明1, 陈烨1,2, 谢秀娟1()   

  1. 1.中国科学院 理化技术研究所 低温科学与技术国家重点实验室,北京 100190
    2.中国科学院大学,北京 100049
  • 收稿日期:2024-12-18 修回日期:2025-01-15 接受日期:2025-02-25 出版日期:2025-02-28 发布日期:2025-02-28
  • 通讯作者: 谢秀娟 E-mail:xiexiujuan@mail.ipc.ac.cn
  • 基金资助:
    国家重点研发计划(2022YFB4002801)

Development and prospects of on-borne liquid hydrogen fuel storage and supply system

Bin ZHU1,2, Shaoqi YANG1, Liang GUO1,2, Qiming JIA1, Ye CHEN1,2, Xiujuan XIE1()   

  1. 1.State Key Laboratory of Cryogenic Science and Technology,Technical Institute of Physics and Chemistry,Chinese Academy of Sciences,Beiing 100190,China
    2.University of Chinese Academy of Sciences,Beijing 100049,China
  • Received:2024-12-18 Revised:2025-01-15 Accepted:2025-02-25 Online:2025-02-28 Published:2025-02-28
  • Contact: Xiujuan XIE E-mail:xiexiujuan@mail.ipc.ac.cn
  • Supported by:
    National Key Research and Development Program(2022YFB4002801)

摘要:

氢动力飞机具有高质量能量密度和近零排放的优势,成为航空业绿色转型中的重要方向。液氢燃料储供系统作为氢动力飞机的核心系统之一,其关键核心技术突破直接影响到飞机的经济性和实用性。系统综述了氢动力飞机的发展现状,重点探讨了液氢储罐、液氢增压泵、换热器等机载液氢燃料储供系统关键部件的设计与集成挑战,并凝练出机载液氢燃料储供系统发展的6项关键核心技术,包括布局优化技术、系统轻量化技术、液氢储罐高质量储氢比与高效存储技术、供氢动态匹配控制技术、液氢冷能综合调控技术以及安全与风险控制技术。分析结果表明:机载液氢燃料储供系统布局优化是基础,依据不同飞机类型给出适用布局;液氢燃料储供系统的轻量化有助于提升飞机的航程和有效载荷,特别是液氢储罐高质量储氢比与高效存储尤其重要;供氢动态匹配控制和液氢冷能综合调控技术适用于飞机动态工作阶段;通过结合国际标准并采用多重安全设计以降低泄漏与火灾风险,保障氢动力飞机运行安全。以上机载液氢燃料储供系统的关键部件研制、关键核心技术突破与相关标准建立,不仅有效推动氢动力飞机的商业化进程,而且为低空经济及航空业碳中和目标提供了重要支撑。

关键词: 氢动力飞机, 机载, 液氢燃料储供系统, 液氢储罐, 质量储氢比

Abstract:

Hydrogen-powered aircraft, with the advantages of high mass-energy density and near-zero emissions, has become an important direction in the green transformation of the aviation industry. As one of the core systems of hydrogen-powered aircraft, the breakthrough of key core technologies in the liquid hydrogen fuel storage and supply system directly affects the economy and practicality of the aircraft. This paper systematically reviews the development status of hydrogen-powered aircraft, with a focus on discussing the design and integration challenges of key components in the on-board liquid hydrogen fuel storage and supply systems, including liquid hydrogen storage tanks, liquid hydrogen booster pumps, and heat exchangers. Furthermore, and s six key core technologies for the development of on-board liquid hydrogen fuel storage and supply systems are condensed: layout optimization technology, system lightweight technology, high-quality hydrogen storage ratio and efficient storage technology for liquid hydrogen storage tanks, hydrogen supply dynamic matching control technology, liquid hydrogen cold energy comprehensive regulation technology, and safety and risk control technology. The analysis results show that the layout optimization of the on-board liquid hydrogen fuel storage and supply system is fundamental, and applicable layouts are given according to different aircraft types; the lightweight of the liquid hydrogen fuel storage and supply system helps to improve the range and payload of the aircraft, especially the high gravimetric hydrogen storage density and efficient storage of liquid hydrogen storage tanks are particularly important. Dynamic hydrogen supply control and liquid hydrogen cold energy comprehensive regulation technologies are applicable to the dynamic working stages of the aircraft. By combining international standards and adopting multiple safety designs to reduce the risks of leakage and fire, the operation safety of hydrogen-powered aircraft is ensured. The development of key components, the breakthrough of key core technologies, and the establishment of relevant standards for the above-mentioned on-board liquid hydrogen fuel storage and supply systems will not only effectively promote the commercialization process of hydrogen-powered aircraft, but also provide important support for the low-altitude economy and the carbon-neutrality goal of the aviation industry.

Key words: hydrogen-powered aircraft, on-board, liquid hydrogen fuel storage and supply system, liquid hydrogen storage tank, gravimetric hydrogen storage density

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