Study on the performance of catalytic reactor for aircraft fuel tank inerting system

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-08-24 DOI:10.1016/j.ast.2024.109440
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Abstract

The catalytic reactor, which plays a pivotal role in the novel aircraft fuel tank green inerting system, encounters complex and alternating inlet boundary conditions. In this study, a transient theoretical model of the catalytic reactor was established and solved through programming, and its accuracy was verified through self-built experimental setups. The dynamic performance of the catalytic reactor and the impact of operational parameters were investigated. Additionally, a method for determining the operational range of the catalytic reactor was proposed. The results indicate that the bed temperature gradually increases to 370°C along the axial direction as the reaction progresses over time. In addition, the concentrations of fuel vapor and oxygen gradually decrease along the axial direction or with time, while achieving a fuel vapor conversion rate of 70.13% under design conditions. The promotion of catalytic reactions can be achieved by lowering the inlet gas velocity, elevating temperature, or increasing the concentrations of fuel vapor and oxygen. However, the bed's maximum temperature may surpass the self-ignition temperature of fuel vapor by 425°C. A novel indicator for oxygen consumption rate is proposed, which should be comprehensively evaluated in conjunction with the conversion rate to determine the performance of catalytic reactors. Moreover, increasing the reactor diameter can enhance both conversion rate and oxygen consumption rate. Pressure drop is detrimental to the catalytic reaction, therefore, high altitude and low-pressure conditions should be considered as the standard for reactor design. Meanwhile, this paper proposes a theoretical model to determine the operational range of the catalytic reactor based on criteria such as suitable catalytic efficiency and flight temperature. The research findings presented in this study provide a solid theoretical foundation for optimizing catalytic reactor design, thereby significantly promoting the application of green inerting systems.

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飞机油箱惰化系统催化反应器性能研究
催化反应器在新型飞机油箱绿色惰化系统中起着举足轻重的作用,会遇到复杂和交替的入口边界条件。本研究通过编程建立并求解了催化反应器的瞬态理论模型,并通过自建实验装置验证了模型的准确性。研究了催化反应器的动态性能和运行参数的影响。此外,还提出了确定催化反应器运行范围的方法。结果表明,随着反应时间的推移,床层温度沿轴向逐渐升高至 370°C。此外,燃料蒸汽和氧气的浓度沿轴向或随时间逐渐降低,而在设计条件下,燃料蒸汽转化率达到 70.13%。降低进气速度、提高温度或增加燃料蒸汽和氧气的浓度都能促进催化反应。然而,床层的最高温度可能会超过燃料蒸汽的自燃温度 425°C。提出了一种新的氧气消耗率指标,应结合转化率进行综合评估,以确定催化反应器的性能。此外,增大反应器直径可提高转化率和氧气消耗率。压降对催化反应不利,因此应将高空低压条件作为反应器设计的标准。同时,本文提出了一个理论模型,根据合适的催化效率和飞行温度等标准来确定催化反应器的运行范围。本文的研究成果为优化催化反应器设计提供了坚实的理论基础,从而极大地推动了绿色惰化系统的应用。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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