Combustion Instabilities With Different Degrees of Premixedness in a Separated Dual-Swirl Burner

Author:

Wang Xinyao1,Han Xiao1,Song Heng1,Zhang Chi1,Wang Jianchen1,Hui Xin1,Lin Yuzhen1,Yang Dong2,Sung Chih-Jen3

Affiliation:

1. National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing 100083, China

2. Department of Mechanical Engineering, Imperial College London, London SW7 2AZ, UK

3. Department of Mechanical Engineering, University of Connecticut Storrs, Mansfield, CT 06269

Abstract

Abstract The effects of premixedness degrees on combustion instabilities of separated dual-swirl flames have been investigated experimentally in the Beihang Axial Swirler Independently Stratified (BASIS) burner. The degree of premixedness is modulated by the fuel split between two injection positions in the outer stream. In the spectra of pressure oscillations, both the frequency and amplitude are positively correlated with fuel split ratios under partially premixed conditions, and the mode transition between perfectly and partially premixed conditions has been observed. The location of perfectly premixed flames shows no obvious variation at different phase angles, only with a slightly wrinkling of the flame surface along the shear layer. Under partially premixed conditions, however, the flame is found to feature a large-scale periodic convective motion, accompanied by the obvious variation of heat releases due to the equivalence ratio oscillations. The local Rayleigh index map compares the thermoacoustic driving factors under perfectly and partially premixed conditions. The development of above convective motions under partially premixed conditions is explained by combining the variations of pressure oscillations and heat releases. An analysis of the thermoacoustic network and convective path is applied to explain the cause of the mode transition. The results show that the appearance of equivalence ratio oscillations and the elongated convective path under partially premixed conditions brings a longer delay time of the flame response, which could be the reason for the mode transition.

Funder

National Science and Technology Major Project

Project of National Natural Science Foundation of China

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference49 articles.

1. Dynamics and Stability of Lean-Premixed Swirl-Stabilized Combustion;Prog. Energy Combust. Sci.,2009

2. Combustion Dynamics and Instabilities: Elementary Coupling and Driving Mechanisms;J. Propul. Power,2003

3. Combustion Instabilities in a Lean Premixed Pre-Vaporized Combustor at High-Pressure High-Temperature,2017

4. Development of a Lean Staged Combustor for Small Aero-Engines,2012

5. Taps: A Fourth Generation Propulsion Combustor Technology for Low Emissions,2003

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3