乙醇/RP-3 航空煤油混合物液滴在高压和高温下的蒸发和微爆特性实验研究

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-07-29 DOI:10.1016/j.ast.2024.109433
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引用次数: 0

摘要

在航空业节能减排的大背景下,乙醇与航空煤油的混合物作为一种潜在的替代燃料已被广泛接受。研究其蒸发过程对于全面了解喷雾燃烧过程的机理至关重要,这为提高航空燃料的利用率提供了重要启示。因此,本研究通过实验研究了初始液滴大小、环境温度和压力对 RP70E30 液滴(RP-3 航空煤油和乙醇的质量比分别为 70% 和 30%)的微爆和蒸发特性的影响。通过悬挂式热电偶和高速摄像机同时获得了液滴温度和大小的变化。结果表明,在无微爆炸的情况下,RP70E30 液滴的蒸发经历了两个阶段,即:瞬时加热阶段和平衡蒸发阶段。而有微爆的 RP70E30 液滴蒸发过程可分为三个阶段:瞬态加热阶段、波动蒸发阶段和平衡蒸发阶段。波动蒸发阶段和平衡蒸发阶段的先后顺序由微爆炸发生的时间决定。RP70E30 液滴只表现出微弱的破裂现象:微爆和膨化。在所有试验条件下,液滴温度在整个蒸发过程中持续上升,其趋势呈现三阶段特征,包括快速上升阶段、缓慢上升阶段和再次快速上升阶段。在 400 °C 和 1 巴条件下,增大液滴初始直径(从 0.746 毫米到 1.258 毫米)可促进 RP70E30 液滴的加热和蒸发。而在 1 巴和 600 °C 条件下,初始直径为 1.156 毫米的液滴在早期蒸发过程中的蒸发速度要慢于初始直径为 1.030 毫米的液滴。这是因为微弱的微爆炸在一定程度上抑制了 PR70E30 液滴的蒸发,其原因是气泡的形成增加了液滴内部的传热阻力。为了研究环境压力和温度对蒸发的影响,我们选择了初始直径(0.95 至 1.05 毫米)相似的液滴。在所有研究温度(400-600 °C)和压力(1-20 巴)下,环境压力和温度的增加都会促进 RP70E30 液滴的加热和蒸发。此外,在 1 巴的压力下,高温会增加微爆的可能性。在 5-20 巴的压力下,不会发生微爆。
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Experimental investigation on evaporation and micro-explosion characteristics of ethanol/RP-3 aviation kerosene blend droplets at elevated pressures and temperatures

Under the background of energy conservation and emission reduction in the aviation industry, blends of ethanol with aviation kerosene have been widely accepted as a potential alternative fuel. Investigating its evaporation process is essential for comprehensively understanding the mechanisms of spray combustion process, which provides significant insights for improving the utilization of aviation fuel. Therefore, in this study, the effects of initial droplet size, ambient temperature and pressure on the micro-explosion and evaporation characteristics of RP70E30 droplets (70% RP-3 aviation kerosene and 30% ethanol by mass) are experimentally investigated. The evolutions of droplet temperature and size are simultaneously obtained by a suspended thermocouple and a high-speed video camera. The results indicate that in the cases without micro-explosion, RP70E30 droplet evaporation undergoes two stages, namely: transient heating and equilibrium evaporation stages. While the evaporation process of RP70E30 droplet with micro-explosion could be separated into three stages: transient heating, fluctuation evaporation and equilibrium evaporation stages. The sequential order of fluctuation evaporation stage and equilibrium evaporation stage is determined by the occurrence time of micro-explosion. RP70E30 droplets only exhibit weak rupture phenomena: weak micro-explosion and puffing. For all test conditions, a continuous increase in droplet temperature is observed throughout the entire evaporation process, and its trend exhibits a three-stage characteristic, including a rapid rise, a slow rise and then another rapid rise stages. At 400 °C and 1 bar, increasing initial droplet diameter (from 0.746 to 1.258 mm) can promote the heating and evaporation of RP70E30 droplet. While at 1 bar and 600 °C, the droplet with an initial diameter of 1.156 mm evaporates at a slower rate than droplet with an initial diameter of 1.030 mm in the early evaporation process. This is because weak micro-explosion somewhat suppresses the evaporation of PR70E30 droplet, which is attributed to the formation of bubbles increasing the heat transfer resistance inside the droplet. The droplets having similar initial diameters (from 0.95 to 1.05 mm) were selected to investigate the effects of ambient pressure and temperature on evaporation. At all the studied temperatures (400–600 °C) and pressures (1–20 bar), increasing ambient pressure and temperature both have a promoting effect on the heating and evaporation of RP70E30 droplet. Moreover, at 1 bar, high temperature can increase the possibility of micro-explosion. At 5–20 bar, no micro-explosion occurs.

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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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