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非定常条件下喷嘴结构对燃油流量脉动的影响
引用本文:汤冠琼,秦皓,李林,林宇震,李继保. 非定常条件下喷嘴结构对燃油流量脉动的影响[J]. 航空动力学报, 2015, 30(4): 831-837. DOI: 10.13224/j.cnki.jasp.2015.04.009
作者姓名:汤冠琼  秦皓  李林  林宇震  李继保
作者单位:1. 北京航空航天大学 能源与动力工程学院航空发动机气动热力国家级重点实验室, 北京 100191;
摘    要:假设油路处于小脉动条件下,燃油流量连续,以流量数为中间变量,推导了燃油流量脉动关于喷嘴结构的关系模型.得出结论:当外部激励一定时,燃油流量脉动与流量数成正比,与平均燃油压降的0.5次方成反比.通过喷嘴标定得出了减小流量数进而减小燃油流量脉动的方法:增加节流级数、减小节流面积,并用脉动试验证明了此方法的正确性,为喷嘴设计者在面对不稳定性问题时提供了一般的设计步骤. 

关 键 词:非定常   直射式喷嘴   喷嘴结构   燃油流量脉动   关系模型   节流级数   节流面积
收稿时间:2013-11-09

Nozzle structure's influence on fuel flow oscillation in unsteady conditions
TANG Guan-qiong,QIN Hao,LI Lin,LIN Yu-zhen and LI Ji-bao. Nozzle structure's influence on fuel flow oscillation in unsteady conditions[J]. Journal of Aerospace Power, 2015, 30(4): 831-837. DOI: 10.13224/j.cnki.jasp.2015.04.009
Authors:TANG Guan-qiong  QIN Hao  LI Lin  LIN Yu-zhen  LI Ji-bao
Affiliation:1. National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;2. Commercial Aircraft Engine Company Limited, Aviation Industry Corporation of China, Shanghai 200241, China
Abstract:Assuming that fuel flow is continuous under small oscillation conditions, a correlation model about fuel flow oscillation and the nozzle structure was derived with flow number as an intermediate variable. Under this model, conclusion are made as follows: fuel flow oscillation is proportional to the flow number, and inversely proportional to the 0.5th power of average fuel pressure drop when the external excitation is given. Methods of decreasing fuel flow oscillation by decreasing flow number are obtained by nozzle calibration: increasing the throttling stage, decreasing throttling area. This method is validated through oscillation experiment. A general design procedure is suggested for nozzle designers in face of the instability problem.
Keywords:unsteady  plane orifice nozzle  nozzle structure  fuel flow oscillation  correlation model  throttling stage  throttling area
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