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有声腔燃烧室的声学特性实验
引用本文:严宇,王延涛,李佳明,李龙飞.有声腔燃烧室的声学特性实验[J].航空动力学报,2016,31(7):1785-1792.
作者姓名:严宇  王延涛  李佳明  李龙飞
作者单位:中国航天科技集团公司 航天推进技术研究院 西安航天动力研究所 液体火箭发动机技术重点实验室, 西安 710100
摘    要:为了掌握声腔对燃烧室声学特性的影响规律,采用冷态实验方法,研究了带有轴向直圆孔声腔的模拟燃烧室的声学特性,其中声腔长度、开口面积比(声腔横截面积除以燃烧室横截面积)和个数均可调节.研究结果表明:燃烧室固有频率随声腔长度的增加而逐渐减小;声腔存在最佳深度,能够抑制一阶切向振型,该最佳深度不受声腔开口面积比影响,略小于1/4一阶切向波长;对抑制一阶切向振型而言,声腔存在最佳开口面积比,在本研究中约为0.17;声腔的分布对燃烧室的声学特性影响较大,相同开口面积比下,声腔个数越多,声波衰减越快. 

关 键 词:冷态实验    声腔    燃烧室    声学特性    燃烧不稳定
收稿时间:2014/10/10 0:00:00

Experiment on acoustic characteristic of combustion chamber with acoustic resonators
YAN Yu,WANG Yan-tao,LI Jia-ming and LI Long-fei.Experiment on acoustic characteristic of combustion chamber with acoustic resonators[J].Journal of Aerospace Power,2016,31(7):1785-1792.
Authors:YAN Yu  WANG Yan-tao  LI Jia-ming and LI Long-fei
Institution:Science and Technology on Liquid Rocket Engine Laboratory, Xi'an Aerospace Propulsion Institute, Academy of Aerospace Propulsion Technology, China Aerospace Science and Technology Corporation, Xi'an 710100, China
Abstract:In order to obtain influence of acoustic resonators on the acoustic characteristic of combustors, a model combustor with axial resonators was investigated experimentally in cold flow tests. The length, area ratio (section area of acoustic resonators divided by section area of combustor) and number of acoustic resonators were changeable in the experiments. It was found that the eigen frequencies of combustor decreased as the length of acoustic resonators increased. The results show that there exists an optimal acoustic resonator length for restraining 1T mode, which is independent from area ratio of acoustic resonators and a little smaller than quarter wave length of 1T mode. For restraining 1T mode, there also exists an optimal area ratio, which is 0.17 in present study. This also indicates that the distribution of acoustic resonators can dramatically affect the acoustic characteristic of a combustor, with acoustic wave decaying faster for more resonators at the same area ratio.
Keywords:cold flow experiment  acoustic resonator  combustor  acoustic characteristic  combustion instability
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