电点火模式下高性能绿色推进剂的液滴动力学行为和燃烧特性实验研究

IF 3.1 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE
JinZe Wu , GuoXiu Li , HongMeng Li , Shuo Zhang , ZhaoPu Yao , Tao Zhang
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引用次数: 0

摘要

以二硝基铵基液体推进剂为代表的高性能绿色推进剂及其新型点火方式是21世纪空间推进领域的研究热点。探索多组分二硝胺基铵液体推进剂液滴在电点火模式下复杂的多尺度物理性质,对喷射、推进系统设计和燃烧控制具有广泛的应用意义。实验研究了不同点火电压下推进剂液滴的动力学行为和燃烧特性。蒸发过程中的液滴动力学行为,包括剧烈的体积振荡、近似稳态膨胀、收缩、二次膨胀、膨化和微爆,由汽泡的产生、增长和排出决定。在初始蒸发过程中,异质成核占主导地位。随着液滴不断受热,均质成核逐渐占据主导地位。温度驱动气泡演化的主要物理和化学机制包括甲醇沸腾、水过热、二硝铵分解和蒸汽分子间的燃烧反应。提高点火电压会增加液滴动力学行为和燃烧,但会加剧燃烧的不稳定性。增加点火电压会增加点火延迟时间、膨化延迟时间、液滴寿命、液滴最高温度,并减小点火临界直径。提出了抑制分解区液滴破裂动力学和增强燃烧区液滴破裂动力学的方法,有利于电点火模式下推进器的燃烧控制。这项研究为研究液体燃料的电点火机制提供了新的见解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental study on droplet dynamics behavior and combustion characteristics of high performance green propellant in electrical ignition mode
High performance green propellant represented by ammonium dinitramide-based liquid propellant and its new ignition method are the research hotspots of space propulsion in the 21st century. Exploring the complex multi-scale physical properties of multi-component ammonium dinitramide-based liquid propellant droplets in the electrical ignition mode has wide application significance for spray, propulsion system design and combustion control. The droplet dynamics behavior and combustion characteristics of propellant droplets at different ignition voltages were studied experimentally. The droplet dynamics behavior during the evaporation process, including violent volume oscillation, approximate steady-state expansion, contraction, secondary expansion, puffing and micro-explosion, have been determined by the generation, growth, and discharge of vapor bubbles. In the initial evaporation process, the heterogeneous nucleation is dominant. As the droplet is continuously heated, homogenization nucleation gradually dominates. The main physical and chemical mechanisms of bubble evolution driven by temperature involve methanol boiling, water overheating, ammonium dinitramide decomposition and combustion reaction between vapor molecules. Increasing the ignition voltage increases the droplet dynamics behavior and the combustion, but promotes the combustion instability. Increasing the ignition voltage increases the ignition delay time, puffing delay time, droplet lifetime, maximum temperature of droplet, and reduces the ignition critical diameter. It is proposed that the method of suppressing the droplet breakup dynamics at decomposition area and enhancing the droplet breakup dynamics at the combustion area are conducive to the combustion control of the thruster in electrical ignition mode. This research provides novel insight into the study of the electrical ignition mechanism of liquid fuels.
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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