航空发动机喷嘴多物理场/多相耦合反应下静电场对积碳抑制的作用机理研究

项目来源

国家自然科学基金(NSFC)

项目主持人

周伟星

项目受资助机构

哈尔滨工业大学

立项年度

2017

立项时间

未公开

项目编号

91741204

项目级别

国家级

研究期限

未知 / 未知

受资助金额

300.00万元

学科

工程与材料科学-工程热物理与能源利用-燃烧学

学科代码

E-E06-E0604

基金类别

重大研究计划-重点支持项目-面向发动机的湍流燃烧基础研究

关键词

静电场 ; 航空发动机 ; 结焦抑制 ; 喷嘴碳沉积 ; 多相反应 ; Aircraft engine ; Carbon deposition in nozzle ; Heterogeneous reaction ; Electrostatic field ; Coking inhibiting

参与者

Yanovskiy L.S.;Martynenko S.I.

参与机构

俄罗斯中央航空发动机研究院;俄罗斯科学院化学物理问题研究所;中国航发沈阳发动机研究所

项目标书摘要:航空发动机高温喷嘴在温度场、速度场及浓度场等多物理场条件下易积碳而成为航空发动机安全运行难以解决的关键瓶颈问题之一。本项目提出了采用连续可调的静电场来对喷嘴附近气/液/固多相反应动力学进行有效控制,一方面利用同电荷相斥原理使得各种组分难以聚合而改变结焦前驱体或大颗粒形成的反应路径,另一方面各种带电粒子在电场作用下远离喷嘴壁面,从而有效抑制与消除喷嘴积碳。本项目紧密结合“面向发动机的湍流燃烧基础研究”重大研究计划中的核心基础科学问题,通过实验与数值模拟相结合,开展了复杂流场的分析,并针对不同工况开展了静电场对喷嘴内外表面的液相沉积、气相沉积及气/液/固多相耦合反应的影响机制研究,得到静电场作用下的多相反应机理。开创性地利用连续可调电场的交叉学科优势来解决复杂工况下航空发动机碳沉积问题,具有十分重要的理论意义和应用价值,属于重大研究计划指南中重点资助研究方向。

Application Abstract: One of the key problems in aircraft engine operation is that high temperature nozzle in temperature field,velocity field,concentration field and other multi-physical field conditions is prone to carbon deposition.Multiphase reactions of gas,liquid and solid near nozzle are controlled by continuously adjustable electrostatic field is put forward in this project.On one hand,various components are difficult to polymerize using the principle of same charge rejecting each other,which change coking precursors or reaction path for large particle formation.On the other hand,charged particles of gas,liquid and solid in the electric field are difficult to reach the nozzle wall,which effectively suppress and eliminate the carbon deposition on nozzle wall.This project is closely integrated with the core science issues in the major research program on“Basic Research on Engine Turbulent Combustion”.Based on experiment and numerical simulation,the complex flow field is analyzed.Then,the influence of electrostatic field on liquid deposition,vapor deposition and multiphase coupling reactions of gas,liquid and solid inside and outside of the nozzle surface is studied in different conditions.At last,multiphase reaction mechanism of electrostatic field is obtained.It is of great theoretical significance and practical value to use continuously adjustable electrostatic field to solve the problem of carbon deposition in aircraft engine under complex conditions.It belongs to Key(Key grant)Project in Major Research Plan.

项目受资助省

黑龙江省

项目结题报告(全文)

针对航空发动机燃烧室高温喷嘴多物理场下多相耦合反应导致喷嘴表面易积碳问题,提出了利用静电场同电荷相斥来改变多相反应碳沉积路径,从而对喷嘴积碳进行抑制的方法。通过数值模拟与实验相结合的方式,研究了航空煤油氧化结焦控制因素分析与流动传热耦合,航空煤油高温裂解、燃烧反应机理发展及简化等基础科学与工程问题;利用数值模拟、分子动力学及量子化学方法对焦体与碳烟颗粒的生成及运动,静电场作用下航空煤油裂解机制、结焦抑制机理、碳烟生成机理以及静电场作用下燃油流动传热特性等展开研究,提出理论可行的静电场作用下航空发动机结焦抑制方案。进一步针对真实航空发动机工程喷嘴的结焦与喷射特性进行工程实验研究,结合数值计算结果,验证了静电场作用下航空发动机结焦抑制方案的可行性。提出了高燃油裂解率和抑制结焦的航空煤油催化裂解方案;确定了航空燃油氧化结焦过程中的控制因素;获得了完整的航空煤油微观演变及焦体颗粒的运动变化规律。进一步得到了静电场对提高燃油裂解速率的微观机制及对碳烟形成的影响规律;获得了表面静电场强度对燃油表面的积碳的分布规律。工程应用上得到了航空发动机工程喷嘴在实际工作受热环境下,污染程度、喷射性能和结焦规律。开创性地利用连续可调电场的交叉学科优势来解决复杂工况下航空发动机碳沉积问题,具有十分重要的理论意义和应用价值,并可推广到火箭发动机及内燃机等所有碳氢组分作为主要燃料的工程应用领域,为其积碳问题消除提供技术指导。

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  • 1.Evaluation of reduced combustion kinetic mechanisms using global sensitivity-based similarity analysis (GSSA)

    • 关键词:
    • Computational fluid dynamics ; Errors ; Ignition ; Association reactions ; Directed graphs ; Forecasting ; Kinetics ; Reaction rates ; Uncertainty analysis;Combustion reactions ; Computational fluid dynamics simulations ; Degree of similarity ; Directed relation graph ; Ignition delay time ; Similarity analysis ; Similarity coefficients ; Uncertainty sources
    • LinShengqiang;ZhouWeixing;WuYou;LawChungK.;XieMing;YangBin
    • 《38th International Symposium on Combustion, 2021》
    • 2021年
    • January 24, 2021 - January 29, 2021
    • Adelaide, Australia
    • 会议

    Reduced combustion kinetic mechanisms, instead of detailed ones, are often used in computational fluid dynamics (CFD) simulations for reduced and frequently even affordable computational cost. The criterion for the evaluation of a reduced mechanism usually focuses on its prediction error for the global properties such as the ignition delay time, while ignoring the detailed features of reaction kinetics such as reaction pathways. In our opinion, good reduced mechanisms should have similar predicting behaviors as the detailed ones, and these behaviors include model predictions for specific targets, prediction error bars, and uncertainty sources for the errors. In this work, a new approach using global sensitivity-based similarity analysis (GSSA) is proposed to compare reduced mechanisms with detailed ones. The similarity coefficient for the reduced mechanism is calculated by similarity method based on Euclidean distance between sensitivity indices of the reduced mechanism and those of the detailed mechanism. The larger the similarity coefficient, the higher the degree of similarity between the reduced and detailed mechanisms. To demonstrate this similarity method, directed relation graph with error propagation (DRGEP) is employed to simplify both the GRI 3.0 mechanism without the NOx chemistry and the JetSurF mechanism consisting of 1459 reactions, resulting in reduced mechanisms with different sizes which can accurately predict the ignition delay times for corresponding fuel mixtures. Similarity analysis is then employed to evaluate these reduced mechanisms. The result shows that the actual reaction kinetic features cannot be replicated by some of the reduced mechanisms. First, the rankings of the important reactions obtained by reduced mechanisms are not consistent with those obtained by the detailed mechanism. Second, by investigating the sensitive reactions, the actual impact of uncertainties in reaction rates on the ignition delay times cannot be presented by reduced mechanisms. The similarity analysis on reduced mechanisms can be used to select a reduced mechanism which shows much better performance to replicate the actual combustion reaction kinetics. GSSA can provide information on the uncertainty sources induced by the reactions parameters of reduced mechanisms for target predictions, which is important for further reduced model optimization and for the sensitivity analysis of CFD simulations. © 2020 The Combustion Institute.

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  • 2.On the differential equations for orthogonal grid generation

    • 关键词:
    • Boundary value problems;Hyperbolic type;Orthogonal grid;Orthogonality conditions;Structured grid
    • Weixing, Zhou;Martynenko, S.I.;Toktaliev, P.D.
    • 《12th International Conference on Mesh Methods for Boundary-Value Problems and Applications, MMBVPA 2018》
    • 2019年
    • September 20, 2018 - September 25, 2018
    • Kazan, Russia
    • 会议

    An opportunity of the orthogonal grids generation for solving 2D and 3D (initial) boundary value problems has been analyzed in this paper. Based on orthogonality condition two variants of the orthogonal grid generation (based on PDEs of elliptic and hyperbolic types) in 2D domains and two partial cases, motion and rotation of 2D orthogonal grid, in 3D domains has been found. An equation that can be used for quality control of 3D close-to-orthogonal boundary fitted structured grids has been proposed.
    © Published under licence by IOP Publishing Ltd.

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