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入口流动参数脉动对燃气轮机燃烧室燃烧不稳定的影响
引用本文:谢法,张珊珊,蒋洪德.入口流动参数脉动对燃气轮机燃烧室燃烧不稳定的影响[J].航空动力学报,2015,30(7):1561-1565.
作者姓名:谢法  张珊珊  蒋洪德
作者单位:清华大学 热能工程系 燃气轮机研究所, 北京 100084,北京华清燃气轮机与煤气化联合循环工程技术有限公司, 北京 100084,清华大学 热能工程系 燃气轮机研究所, 北京 100084
摘    要:通过均匀搅拌器(PSR)模型研究了某型燃气轮机燃烧室入口流动参数脉动对燃烧不稳定的影响.研究结果表明:对于贫预混燃烧室(燃烧室工作在较低的入口当量比下)来说,当入口温度、入口气体流量和入口当量比的相对脉动幅值相同时,入口当量比的脉动对燃烧不稳定性的影响最大,其次是入口气体流量,而入口温度的脉动对燃烧不稳定性的影响相对较小.

关 键 词:燃气轮机  贫预混燃烧室  均匀搅拌器模型  燃烧不稳定性  入口流动参数  脉动
收稿时间:2014/2/10 0:00:00

Effects of inlet flow parameters oscillation on combustion instability of gas turbine combustor
XIE F,ZHANG Shan-shan and JIANG Hong-de.Effects of inlet flow parameters oscillation on combustion instability of gas turbine combustor[J].Journal of Aerospace Power,2015,30(7):1561-1565.
Authors:XIE F  ZHANG Shan-shan and JIANG Hong-de
Affiliation:Gas Turbine Institute, Department of Thermal Engineering, Tsinghua University, Beijing 100084, China,Beijing Huatsing Gas Turbine and Integrated Gasification Combined Cycle Technology Company Limited, Beijing 100084, China and Gas Turbine Institute, Department of Thermal Engineering, Tsinghua University, Beijing 100084, China
Abstract:The effects of inlet flow parameters oscillation on combustion instabilities of a gas turbine combustor were studied by introducing perfectly stirred reactor (PSR) model. The simulation results demonstrate that, for lean premixed combustor (combustor operating at low inlet equivalence ratio), when the relative oscillation amplitudes of inlet temperature, inlet mixture mass flow rate and inlet equivalence ratio are the same, the oscillation of inlet equivalence ratio has the largest effect on combustion instability phenomenon, then followed by inlet mixture mass flow rate, and the inlet temperature yields the lowest effect.
Keywords:gas turbine  lean premixed combustor  perfectly stirred reactor model  combustion instability  inlet flow parameters  oscillation
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