A Study on Effects of Spray Characteristics on Prevaporization and Premix Combustion Mechanism
喷雾特性对预汽化及预混燃烧机理的影响研究
基本信息
- 批准号:07650232
- 负责人:
- 金额:$ 1.41万
- 依托单位:
- 依托单位国家:日本
- 项目类别:Grant-in-Aid for Scientific Research (C)
- 财政年份:1995
- 资助国家:日本
- 起止时间:1995 至 1996
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
This study aims to clarify the relationship between spray characteristics, evaporation characteristics, combustion characteristics and emission characteristics, and to obtain the guide to the design of a premix and prevaporization combustor with low NOx emission. From the results of atomization experiments at room temperature, the radial profile of droplet mass flux approaches to uniform profile downstream. At the exit of the evaporation tube (495mm downstream from the nozzle), the droplet mass flux at the center is about twice of that near the tube wall. By evaporation experiments using a water at 30m/s of inlet air velocity and 550K of inlet air temperature, at 175mm far from the nozzle the droplet mass flux at the center is larger than that of the vapor. The droplet evaporation advances rapidly downstream, and at 430mm far from the nozzle the mass flux of the vapor at the center becomes larger than that of the droplet. Concerning to the radial profile of a rate of the vapor to the w … More ater component including droplets and vapor, the rate has a peak at the middle between the center and the tube wall. From the results of combustion experiments using a kerosene, the flame holding mechanism changes at 0.6 of equivalence ratio. The lower flammability limit decreases with a increase of a length of the vaporization tube, the inlet air temperature and the inlet air velocity. The NOx concentration in the exhausted gas increases exponentially with a increase of the equivalence ratio. The empirical equation of the emission index of NOx was obtained. The emission index of NOx can be reduced less than 1g (NOx) /kg (Fuel) and that of CO less than 10g (CO) /kg (Fuel) within the range of 0.54 to 0.68 of the equivalence ratio using newly designed combustor. By the numerical simulation of the spray flow and the spray evaporation without combustion under the condition of 30m/s of the inlet air velocity and 550K of the inlet air temperature, at 500mm far from the nozzle the air temperature at the center is 35K lower than that at the periphery, and the Sauter's mean diameter of the spray at the center is 30 micron smaller than that at the periphery. Less
本研究旨在阐明喷雾特性、蒸发特性、燃烧特性与排放特性之间的关系,为低NOx排放预混预汽化燃烧室的设计提供指导。从室温下的雾化实验结果来看,液滴质量通量的径向分布在下游趋于均匀分布。在蒸发管出口(喷嘴下游495mm处),中心液滴质量通量约为管壁附近液滴质量通量的2倍。在进气速度为30m/s,进气温度为550K的条件下,在距离喷嘴175mm处,液滴中心的质量通量大于水蒸气的质量通量。液滴蒸发向下游快速推进,在距离喷嘴430mm处,中心蒸汽的质量通量大于液滴的质量通量。在含液滴和水蒸气的水组分较多的情况下,在中心和管壁之间的中间位置有一个峰值。从煤油燃烧实验结果来看,当当量比为0.6时,持焰机理发生变化。可燃性下限值随汽化管长度、进气温度和进气速度的增加而减小。废气中NOx浓度随当量比的增大呈指数增长。得到了NOx排放指数的经验方程。采用新设计的燃烧室,在等效比0.54 ~ 0.68的范围内,NOx排放指标可降至1g (NOx) /kg(燃料)以下,CO排放指标可降至10g (CO) /kg(燃料)以下。通过对进气速度为30m/s、进气温度为550K条件下的喷雾流动和无燃烧蒸发的数值模拟,在距离喷嘴500mm处,中心处的空气温度比外围低35K,中心处喷雾的Sauter平均直径比外围小30微米。少
项目成果
期刊论文数量(10)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
稲村隆夫: "予蒸発予混合燃焼器の特性" 第33回燃焼シンポジウム前刷集. 210-212 (1995)
Takao Inamura:“预汽化预混燃烧器的特性”第 33 届燃烧研讨会预印本集 210-212(1995 年)。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
稲村隆夫: "予蒸発予混合燃焼における排ガス特性" 第34回燃焼シンポジウム前刷集. 624-626 (1996)
Takao Inamura:“预蒸发和预混合燃烧中的废气特性”第 34 届燃烧研讨会预印本 624-626(1996 年)。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
Takao Inamura: "Emission Characteristics of Prevaporization and Premix Combustion" Proc.34th Japanese combustion Symposium. 624-626 (1996)
Takao Inamura:“预汽化和预混燃烧的排放特性”Proc.34th 日本燃烧研讨会。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
稲村隆夫: "予蒸発予混合燃焼における排ガス特性" 第34回燃焼シンポジウム前刷集. 1996. 624-626
Takao Inamura:“预蒸发和预混合燃烧中的废气特性”第 34 届燃烧研讨会预印本,1996 年。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
稲村隆夫: "予蒸発予混合燃焼の特性" 第33回燃焼シンポジウム前刷集. 210-212 (1995)
Takao Inamura:“预蒸发和预混合燃烧的特性”第 33 届燃烧研讨会预印本集 210-212(1995 年)。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
{{
item.title }}
{{ item.translation_title }}
- DOI:
{{ item.doi }} - 发表时间:
{{ item.publish_year }} - 期刊:
- 影响因子:{{ item.factor }}
- 作者:
{{ item.authors }} - 通讯作者:
{{ item.author }}
数据更新时间:{{ journalArticles.updateTime }}
{{ item.title }}
- 作者:
{{ item.author }}
数据更新时间:{{ monograph.updateTime }}
{{ item.title }}
- 作者:
{{ item.author }}
数据更新时间:{{ sciAawards.updateTime }}
{{ item.title }}
- 作者:
{{ item.author }}
数据更新时间:{{ conferencePapers.updateTime }}
{{ item.title }}
- 作者:
{{ item.author }}
数据更新时间:{{ patent.updateTime }}
INAMURA Takao其他文献
Fundamental study on cooling of biological phantom using ice slurry in limited space
有限空间冰浆冷却生物体模的基础研究
- DOI:
10.1299/jfst.2019jfst0020 - 发表时间:
2019 - 期刊:
- 影响因子:0.8
- 作者:
OKABE Takahiro;NISHIKAWA Haruki;MIYAGAWA Taimei;INAMURA Takao;FUMOTO Koji - 通讯作者:
FUMOTO Koji
INAMURA Takao的其他文献
{{
item.title }}
{{ item.translation_title }}
- DOI:
{{ item.doi }} - 发表时间:
{{ item.publish_year }} - 期刊:
- 影响因子:{{ item.factor }}
- 作者:
{{ item.authors }} - 通讯作者:
{{ item.author }}
{{ truncateString('INAMURA Takao', 18)}}的其他基金
Mass production method of micron liquid droplets by active control of cavitation flow
主动控制空化流大规模生产微米级液滴的方法
- 批准号:
18560151 - 财政年份:2006
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (C)
Basic Research on Wall Impinging Jet and Its Application to High Performance Spray Formation
冲击壁射流基础研究及其在高性能喷雾形成中的应用
- 批准号:
14550172 - 财政年份:2002
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (C)
Basic Studies on Spray Formation Mechanism and Its Modeling
喷雾形成机理及其建模的基础研究
- 批准号:
12650189 - 财政年份:2000
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (C)
Modeling of Spray Formation Mechanism and Numerical Simulation of Spray Flow
喷雾形成机理建模及喷雾流动数值模拟
- 批准号:
09650217 - 财政年份:1997
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (C)
相似海外基金
Micro-scale Additive Manufacturing (3D Printing) of High-Temperature Strain Sensors on Non-Planar Surfaces of Jet Engine Components
喷气发动机部件非平面表面高温应变传感器的微型增材制造(3D 打印)
- 批准号:
576693-2022 - 财政年份:2022
- 资助金额:
$ 1.41万 - 项目类别:
Alliance Grants
Effects of Sustainable Aviation Fuel Components on Jet Engine Combustion and Exhaust Gas Dynamics
可持续航空燃料成分对喷气发动机燃烧和废气动力学的影响
- 批准号:
22H01676 - 财政年份:2022
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Low dislocation AlN growth by super high temperature MOVPE in jet engine model
喷气发动机模型中超高温 MOVPE 低位错 AlN 生长
- 批准号:
20K21006 - 财政年份:2020
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Challenging Research (Exploratory)
Development of Modeling and Multi-Physics Predicition Methods for Particulate Deposition in Jet Engine
喷气发动机颗粒沉积建模和多物理预测方法的发展
- 批准号:
20H04200 - 财政年份:2020
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Developing high Co-containing Ni-based superalloys with improved oxidation behaviour for future jet-engine applications
开发具有改善氧化行为的高钴镍基高温合金,用于未来喷气发动机应用
- 批准号:
2386298 - 财政年份:2020
- 资助金额:
$ 1.41万 - 项目类别:
Studentship
Quickest change detection, statistical learning and nonlinear filtering of jet engine data
喷气发动机数据的最快变化检测、统计学习和非线性过滤
- 批准号:
543433-2019 - 财政年份:2020
- 资助金额:
$ 1.41万 - 项目类别:
Collaborative Research and Development Grants
Quickest change detection, statistical learning and nonlinear filtering of jet engine data
喷气发动机数据的最快变化检测、统计学习和非线性过滤
- 批准号:
543433-2019 - 财政年份:2019
- 资助金额:
$ 1.41万 - 项目类别:
Collaborative Research and Development Grants
Radio Frequency Jet Engine Airfoil Clearance Sensor
射频喷气发动机翼型间隙传感器
- 批准号:
543879-2019 - 财政年份:2019
- 资助金额:
$ 1.41万 - 项目类别:
Collaborative Research and Development Grants
Micro-Scale Additive Manufacturing of Strain Gauges on Non-planar Surface of Jet Engine Blades: Extended Objectives
喷气发动机叶片非平面表面应变计的微尺度增材制造:扩展目标
- 批准号:
521292-2017 - 财政年份:2019
- 资助金额:
$ 1.41万 - 项目类别:
Collaborative Research and Development Grants
Analysis on combustion instability of jet engine combustor for bio-jet fuel
喷气发动机燃烧室生物航煤燃烧不稳定性分析
- 批准号:
19H02341 - 财政年份:2019
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (B)