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Characteristics of polyhedral hydrogen-ammonia Bunsen flames 多面体氢-氨本生火焰的特性
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-07-02 DOI: 10.1016/j.proci.2026.106087
Allen Hsing, Jose G. Rivera Lizarralde, Mario Sánchez-Sanz, Abhishek Saha
Hydrogen-ammonia blends are increasingly considered as promising carbon-free fuels for future combustion systems. In this study, we investigate the dynamics of cellular instabilities in hydrogen-ammonia Bunsen flames. While previous studies have examined such instability phenomena in hydrocarbon and pure hydrogen flames, the influence of ammonia addition, particularly under flow-driven configuration, remains less explored. Using chemiluminescence and Mie-scattering imaging, we characterize the effect of ammonia concentration on the transition between stable and unstable flame regimes and on the morphology of the resulting polyhedral structures. Our results show that increasing ammonia content narrows the range of unstable operating conditions due to its lower chemical reactivity, whereas higher hydrogen fractions promote flashback, thereby limiting stable flame operation. The observed transitions and modifications in flame morphology are further interpreted using scaling analyses derived from the corresponding dispersion relations.
Novelty and significance statement: While hydrogen-ammonia blends are widely regarded as promising carbon-free fuels, important questions remain regarding their suitability for practical engine operation. Pure hydrogen flames, especially under fuel-lean conditions, are susceptible to cellular instabilities that induce intrinsic self-acceleration and thereby, elevated propagation speeds. This study demonstrates how the addition of ammonia to hydrogen modulates the transition between stable and unstable regimes.
While cellular instabilities are most often studied in freely expanding flames, we explore them in a burner-stabilized configuration. To the authors’ best knowledge, this is the first study to systematically investigate how varying the degree of ammonia blending in hydrogen affects the morphology, stability, and transition dynamics of polyhedral flames. In addition, the study also confirms that intense local stretch near the cusps of polyhedral ridges can trigger localized extinction. Beyond its fundamental significance, the experimental observations and accompanying scaling analysis offer a practical framework for identifying operating conditions that suppress such instabilities.
氢-氨混合物越来越被认为是未来燃烧系统中有前途的无碳燃料。在这项研究中,我们研究了氢氨本生火焰中细胞不稳定性的动力学。虽然以前的研究已经研究了碳氢化合物和纯氢火焰中的这种不稳定现象,但氨添加的影响,特别是在流动驱动配置下的影响,仍然很少被探索。利用化学发光和米散射成像,我们表征了氨浓度对稳定和不稳定火焰状态之间转变的影响,以及对所产生的多面体结构的形貌的影响。我们的研究结果表明,由于氨的化学反应活性降低,氨含量的增加缩小了不稳定操作条件的范围,而氢含量的增加促进了闪回,从而限制了稳定的火焰操作。观察到的火焰形态的转变和变化可以用相应的分散关系得出的标度分析进一步解释。新颖性和重要性声明:虽然氢氨混合物被广泛认为是有前途的无碳燃料,但其在实际发动机运行中的适用性仍然存在重要问题。纯氢火焰,特别是在燃料贫乏的条件下,容易受到细胞不稳定的影响,从而导致内在的自加速,从而提高传播速度。本研究证明了氨对氢的添加如何调节稳定和不稳定状态之间的过渡。虽然细胞不稳定性最常在自由膨胀的火焰中研究,但我们在燃烧器稳定的配置中探索它们。据作者所知,这是第一个系统地研究氢中氨混合程度如何影响多面体火焰的形态、稳定性和过渡动力学的研究。此外,该研究还证实了多面体脊尖附近的强烈局部拉伸可以引发局部灭绝。除了其基本意义之外,实验观察和随附的标度分析为确定抑制此类不稳定性的操作条件提供了实用框架。
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引用次数: 0
Adaptive learning of data assimilated combustion reaction model 数据同化燃烧反应模型的自适应学习
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-07-20 DOI: 10.1016/j.proci.2026.106249
Wendi Dong, Andrea Nobili, Hai Wang
Data-assimilated combustion reaction models must evolve as new fundamental combustion property data become available. This work introduces an adaptive learning framework, built on the Method of Uncertainty Minimization by Polynomial Chaos Expansions (MUM-PCE), that enables established data-assimilated models to efficiently incorporate additional data without requiring a complete re-optimization of the original database. The method is demonstrated by assimilating new hydrogen laminar flame speed measurements at elevated pressure and unburned gas temperature into the Foundational Fuel Chemistry Model version 2 (FFCM-2). Using the proposed adaptive optimization strategy, the updated model successfully reconciles the newly introduced data while remaining consistent with the rate parameter uncertainty space defined by the original FFCM-2 optimization. The approach also enables analysis of the effects of different inert flame diluents, revealing the degree of orthogonality and correlation among flame-speed measured with various diluents and among their corresponding third-body efficiencies. These results illustrate how adaptive learning can maintain model fidelity while progressively expanding the assimilated data base, leading to a more reliable reaction model for combustion simulations.
Novelty and significance statement: This work introduces an adaptive learning framework for updating data-assimilated combustion reaction models as new combustion property experiments become available. Unlike previous approaches that require re-optimizing against the entire experimental database, the proposed method efficiently assimilates new measurements while preserving the parameter uncertainty constraints established in the original optimization. Demonstrated using new hydrogen laminar flame speed data added to the FFCM-2 database, the framework maintains model consistency and reveals correlations among measurements with different diluents and their associated third-body efficiencies. The methodology provides a scalable strategy for continuously updating large kinetic models, enabling combustion reaction models to evolve systematically with emerging experimental data while retaining computational efficiency and predictive reliability.
数据同化的燃烧反应模型必须随着新的基本燃烧特性数据的出现而发展。这项工作引入了一个自适应学习框架,该框架建立在多项式混沌展开的不确定性最小化方法(MUM-PCE)上,使已建立的数据同化模型能够有效地合并额外的数据,而无需对原始数据库进行完全的重新优化。通过将高压和未燃烧气体温度下的新氢层流火焰速度测量结果纳入基础燃料化学模型2 (FFCM-2),验证了该方法。利用所提出的自适应优化策略,更新后的模型成功地协调了新引入的数据,同时与原FFCM-2优化定义的速率参数不确定性空间保持一致。该方法还可以分析不同惰性火焰稀释剂的影响,揭示用各种稀释剂测量的火焰速度及其相应的第三体效率之间的正交性和相关性程度。这些结果说明了自适应学习如何在逐步扩展同化数据库的同时保持模型保真度,从而为燃烧模拟提供更可靠的反应模型。新颖性和意义声明:随着新的燃烧特性实验的出现,这项工作引入了一个自适应学习框架,用于更新数据同化的燃烧反应模型。与以往需要针对整个实验数据库重新优化的方法不同,该方法有效地吸收了新的测量结果,同时保留了原始优化中建立的参数不确定性约束。使用添加到FFCM-2数据库中的新氢层流火焰速度数据进行演示,该框架保持了模型的一致性,并揭示了不同稀释剂及其相关第三体效率之间的相关性。该方法为持续更新大型动力学模型提供了一种可扩展的策略,使燃烧反应模型能够随着新出现的实验数据系统地发展,同时保持计算效率和预测可靠性。
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引用次数: 0
Flame speed enhancement in narrow channels of low effusivity aerogel 低渗透气凝胶窄通道中火焰速度的增强
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-07-29 DOI: 10.1016/j.proci.2026.106293
Zachary T. Negrette, Mark Short, Scott I. Jackson
Flame dynamics in narrow channels are governed by thermal and momentum interactions at the walls, which become increasingly dominant as the surface-area-to-volume ratio increases. Understanding these near-quenching phenomena is critical for the development of small-scale combustion devices, such as microcombustors and flame arresters. This study investigates the influence of low-thermal-conductivity polyimide aerogel walls (Airloy H116) on freely propagating, constant-pressure ethylene–air flames, benchmarking the results against aluminum, PMMA, and soda-lime glass. Experiments were conducted in rectangular channels (25.4 mm depth, 305 mm length) with widths varying from 1.5 to 12.7 mm. High-speed imaging and synchronized pressure measurements revealed that while flame speeds were relatively insensitive to channel width for conventional materials above 4.7 mm, aerogel-confined flames exhibited a dramatic velocity enhancement in excess of 300%, just prior to the critical quenching width. This pronounced acceleration is attributed to the aerogel’s exceptionally low thermal effusivity, which elevates gas-wall interface temperatures and preheats the near-wall reactants. These findings demonstrate that strategic selection of wall materials can transform boundary layers from traditional loss mechanisms into combustion enhancers. Such extreme variation in flame speed has significant implications for the thermal management, efficiency, and safety parameters of microscale propulsion and power systems.
Novelty and significance statement: This study reports an unprecedented enhancement in flame propagation speeds near quenching limits, identifying a phenomenon unique to low-effusivity aerogel walls. We demonstrate that near-adiabatic boundary layers can fundamentally transform from a loss mechanism into a combustion enhancer. These findings provide a novel framework for “tuning” microscale devices, where millimeter-scale adjustments to channel geometry toggle between total flame extinction and peak thermal performance.
窄通道内的火焰动力学是由壁面的热和动量相互作用决定的,随着表面积体积比的增加,热和动量相互作用越来越占主导地位。了解这些近淬灭现象对于小型燃烧装置的开发至关重要,例如微燃烧器和阻火器。本研究探讨了低导热聚酰亚胺气凝胶壁(Airloy H116)对自由传播的恒压乙烯-空气火焰的影响,并将结果与铝、PMMA和钠石灰玻璃进行了比较。实验在矩形通道(25.4 mm深,305 mm长)中进行,宽度从1.5到12.7 mm不等。高速成像和同步压力测量显示,对于4.7 mm以上的传统材料,火焰速度对通道宽度相对不敏感,而气凝胶限制的火焰在临界淬火宽度之前表现出超过300%的显著速度增强。这种明显的加速归因于气凝胶异常低的热渗出率,这提高了气壁界面温度,并预热了近壁反应物。这些发现表明,墙体材料的战略性选择可以将边界层从传统的损失机制转变为燃烧增强机制。这种火焰速度的极端变化对微尺度推进和动力系统的热管理、效率和安全参数具有重要意义。新颖性和意义声明:本研究报告了在淬火极限附近火焰传播速度的前所未有的增强,确定了低流通量气凝胶壁特有的现象。我们证明了近绝热边界层可以从根本上从损失机制转变为燃烧增强机制。这些发现为“调谐”微尺度器件提供了一个新的框架,其中毫米尺度的通道几何调整在总火焰熄灭和峰值热性能之间切换。
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引用次数: 0
The role of ab-initio chemical kinetics of N2H2/NNH with NO2 and OH in gas-phase modeling hypergolic ignition of monomethylhydrazine/hydrazine and nitrogen dioxide N2H2/NNH与NO2和OH的ab-initio化学动力学在单甲基肼/肼和二氧化氮气相自燃模拟中的作用
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-09-12 DOI: 10.1016/j.proci.2026.106377
Junfeng Bai, Lidong Zhang, Lei Zhou, Peng Zhang
The high-level ab initio chemical kinetics of N2H2/NNH with NO2 and OH and its application to modeling hypergolic ignition of the hydrazine-based fuels and NO2 system were investigated in this work. The CCSD(T)/CBS//M06-2X/6–311++G(d,p) single-reference method and the MRCI(7e,6o)/CBS//M06–2X/6–311++G(d,p) multi-reference method was employed for the calculations of the potential energy surfaces (PESs). The temperature- and pressure-dependent rate constants are determined by using the RRKM/Master Equation approach with the transition state theory (TST), and the variable reaction coordinate transition state theory (VRC-TST) for barrierless reactions, and the variational transition state theory (VTST) for the reactions with rather low barriers. The calculated rate constants and thermodynamics data were incorporated into the reaction mechanisms of bipropellant systems involving monomethylhydrazine(MMH) with nitrogen dioxide (NO2) and hydrazine (N2H4) with nitrogen dioxide (NO2) to evaluate their influence on modeling the hypergolic ignition of these systems. With the updated rate constants, the consumptions of MMH and NO2 were found to be highly promoted due to the fast consumption of N2H2. Important reaction pathways were identified by the rate of production and the sensitivity analyses. Moreover, the new N2H4/NO2 mechanism captures the gas-phase kinetic limits for the N2H4/NO2 system, although below 400 K, multiphase effects completely dominate.
Novelty and Significance Statement
This study presents the first high-level theoretical investigation of N2H2/NNH reactions with NO2 and OH radicals using both single-reference (CCSD(T)/CBS) and multi-reference (MRCI/CBS) methods coupled with variational transition state theory. The calculated accurate rate constants and thermochemistry enable critical updates to MMH/NO2 and N2H4/NO2 chemical mechanisms, substantially improving predictive capability for low-temperature hypergolic ignition. These findings resolve long-standing discrepancies in ignition simulations and provide the combustion community with essential kinetic parameters for hydrazine-based propulsion systems. The methodological framework underscores the importance of multi-reference calculations in complex radical reactions, establishing a foundation for optimizing bipropellant combustion efficiency and controlling ignition characteristics in aerospace applications.
本文研究了N2H2/NNH在NO2和OH作用下的高水平从头算化学动力学及其在肼基燃料和NO2体系自燃着火模拟中的应用。采用CCSD(T)/CBS//M06-2X/ 6-311 ++G(d,p)单参考法和MRCI(7e, 60)/CBS//M06-2X/ 6-311 ++G(d,p)多参考法计算势能面(PESs)。温度和压力相关的速率常数采用RRKM/Master方程方法和过渡态理论(TST)确定,无势垒反应采用变反应坐标过渡态理论(VRC-TST),低势垒反应采用变分过渡态理论(VTST)确定。将计算得到的速率常数和热力学数据纳入一元甲基肼(MMH)与二氧化氮(NO2)和肼(N2H4)与二氧化氮(NO2)二元推进剂体系的反应机理,评价其对系统自燃着火模型的影响。在更新速率常数后,由于N2H2的快速消耗,MMH和NO2的消耗得到了极大的促进。通过产率和灵敏度分析确定了重要的反应途径。此外,新的N2H4/NO2机制捕获了N2H4/NO2体系的气相动力学极限,尽管在400 K以下,多相效应完全占主导地位。新颖性和意义声明本研究首次采用单参考(CCSD(T)/CBS)和多参考(MRCI/CBS)方法结合变分过渡态理论对N2H2/NNH与NO2和OH自由基的反应进行了高水平的理论研究。计算出的精确速率常数和热化学性质使MMH/NO2和N2H4/NO2的化学机制得到重要更新,大大提高了低温自燃着火的预测能力。这些发现解决了点火模拟中长期存在的差异,并为燃烧界提供了基于肼的推进系统的基本动力学参数。该方法框架强调了复杂自由基反应中多参考计算的重要性,为优化双推进剂燃烧效率和控制航天应用中的点火特性奠定了基础。
{"title":"The role of ab-initio chemical kinetics of N2H2/NNH with NO2 and OH in gas-phase modeling hypergolic ignition of monomethylhydrazine/hydrazine and nitrogen dioxide","authors":"Junfeng Bai,&nbsp;Lidong Zhang,&nbsp;Lei Zhou,&nbsp;Peng Zhang","doi":"10.1016/j.proci.2026.106377","DOIUrl":"10.1016/j.proci.2026.106377","url":null,"abstract":"<div><div>The high-level ab initio chemical kinetics of N<sub>2</sub>H<sub>2</sub>/NNH with NO<sub>2</sub> and OH and its application to modeling hypergolic ignition of the hydrazine-based fuels and NO<sub>2</sub> system were investigated in this work. The CCSD(T)/CBS//M06-2X/6–311++G(d,p) single-reference method and the MRCI(7e,6o)/CBS//M06–2X/6–311++G(d,p) multi-reference method was employed for the calculations of the potential energy surfaces (PESs). The temperature- and pressure-dependent rate constants are determined by using the RRKM/Master Equation approach with the transition state theory (TST), and the variable reaction coordinate transition state theory (VRC-TST) for barrierless reactions, and the variational transition state theory (VTST) for the reactions with rather low barriers. The calculated rate constants and thermodynamics data were incorporated into the reaction mechanisms of bipropellant systems involving monomethylhydrazine(MMH) with nitrogen dioxide (NO<sub>2</sub>) and hydrazine (N<sub>2</sub>H<sub>4</sub>) with nitrogen dioxide (NO<sub>2</sub>) to evaluate their influence on modeling the hypergolic ignition of these systems. With the updated rate constants, the consumptions of MMH and NO<sub>2</sub> were found to be highly promoted due to the fast consumption of N<sub>2</sub>H<sub>2</sub>. Important reaction pathways were identified by the rate of production and the sensitivity analyses. Moreover, the new N<sub>2</sub>H<sub>4</sub>/NO<sub>2</sub> mechanism captures the gas-phase kinetic limits for the N<sub>2</sub>H<sub>4</sub>/NO<sub>2</sub> system, although below 400 K, multiphase effects completely dominate.</div><div><strong>Novelty and Significance Statement</strong></div><div>This study presents the first high-level theoretical investigation of N<sub>2</sub>H<sub>2</sub>/NNH reactions with NO<sub>2</sub> and OH radicals using both single-reference (CCSD(T)/CBS) and multi-reference (MRCI/CBS) methods coupled with variational transition state theory. The calculated accurate rate constants and thermochemistry enable critical updates to MMH/NO<sub>2</sub> and N<sub>2</sub>H<sub>4</sub>/NO<sub>2</sub> chemical mechanisms, substantially improving predictive capability for low-temperature hypergolic ignition. These findings resolve long-standing discrepancies in ignition simulations and provide the combustion community with essential kinetic parameters for hydrazine-based propulsion systems. The methodological framework underscores the importance of multi-reference calculations in complex radical reactions, establishing a foundation for optimizing bipropellant combustion efficiency and controlling ignition characteristics in aerospace applications.</div></div>","PeriodicalId":408,"journal":{"name":"Proceedings of the Combustion Institute","volume":"42 ","pages":"Article 106377"},"PeriodicalIF":4.6,"publicationDate":"2026-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148951579","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Exploring long range dynamics using neural network potentials: From recrossing coefficients to roaming 利用神经网络电位探索远程动态:从重交系数到漫游
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-09-16 DOI: 10.1016/j.proci.2026.106450
Simone Vari, Sarah N. Elliott, Yuri Georgievskii, Stephen J. Klippenstein, Carlo Cavallotti
<div><div>Accurate determination of the rate coefficients and branching ratios for the various channels in a barrierless reaction process are critical for reliable mechanistic predictions, but they are often treated approximately due to several substantial challenges. The gold standard for computing rate constants of barrierless reactions is variable reaction coordinate transition state theory (VRC-TST), with accuracies approaching those of experimental measurements. However, the statistical assumptions that provide the basis for VRC-TST may not adequately describe certain dynamical effects, such as transition state recrossing fractions, especially for reactions with multiple bottlenecks, and roaming pathways. Although these processes can be adequately described with rigid-body trajectory simulations, doing so requires a sufficiently accurate potential energy surface (PES). Direct trajectory simulations come at a huge computational cost, requiring up to millions of single point energy evaluations and are thus unfeasible for the vast majority of chemical reactions. In this work we investigate whether it is possible to determine a PES suitable for trajectory simulations using a novel machine learning approach that exploits ab-initio calculations to feed a physics-inspired neural network (PHINN) architecture. The main result of this work is that the PHINN PES is sufficiently accurate not only to carry out VRC-TST simulations, but also to perform trajectory simulations, thus opening the path to the systematic use of trajectory simulations to study the kinetics of barrierless reactions. The developed framework is validated via a study of formaldehyde decomposition, providing roaming fractions in agreement with existing studies. After validation, the PHINN is employed to compute temperature-dependent recrossing coefficients for the recombination reactions between CH<sub>3</sub> + H and NH<sub>2</sub> + CH<sub>3</sub>, providing in the latter case a framework for validating the accuracy of two-state transition state theory. The developed computational approach is then used to study the long-range recombination roaming dynamics between H and phenoxy radical, providing site-specific branching fractions among the three possible addition sites.</div></div><div><h3>Novelty and significance statement</h3><div>In this work, we demonstrate for the first time that rate constants and roaming fluxes can be computed using trajectory simulations combined with neural network potential energy surfaces, enabling new approaches to reaction kinetics. We present a robust framework to (i) compute temperature-dependent recrossing coefficients, (ii) assess the accuracy of 2-state transition state theory, and (iii) determine roaming branching fractions, which are extremely difficult to evaluate accurately with existing methods. These advances are critical for improving the understanding of barrierless reactions, typically involving radical–radical recombination, which are pre
准确确定无障碍反应过程中各种通道的速率系数和分支比对于可靠的机理预测至关重要,但由于一些重大挑战,它们通常被近似处理。计算无障碍反应速率常数的金标准是变反应坐标过渡态理论(VRC-TST),其精度接近实验测量值。然而,为VRC-TST提供基础的统计假设可能无法充分描述某些动态效应,例如过渡态重相交分数,特别是对于具有多个瓶颈的反应和漫游路径。虽然这些过程可以用刚体轨迹模拟来充分描述,但这样做需要一个足够精确的势能面(PES)。直接的轨迹模拟需要巨大的计算成本,需要多达数百万的单点能量评估,因此对绝大多数化学反应来说是不可行的。在这项工作中,我们研究了是否有可能使用一种新的机器学习方法来确定适合轨迹模拟的PES,该方法利用从头计算来提供物理启发的神经网络(PHINN)架构。这项工作的主要结果是,PHINN PES不仅能够进行VRC-TST模拟,而且能够进行轨迹模拟,从而为系统地使用轨迹模拟来研究无障反应动力学开辟了道路。开发的框架通过甲醛分解研究得到验证,提供与现有研究一致的漫游分数。验证后,利用PHINN计算CH3 + H和NH2 + CH3复合反应的温度相关重交系数,为验证两态过渡态理论的准确性提供了一个框架。该计算方法用于研究H和苯氧基之间的长距离重组漫游动力学,提供三个可能的加成位点之间的特定位点分支分数。在这项工作中,我们首次证明了可以使用轨迹模拟结合神经网络势能面来计算速率常数和漫游通量,从而为反应动力学提供了新的方法。我们提出了一个健壮的框架来(i)计算温度相关的重交系数,(ii)评估两态过渡态理论的准确性,以及(iii)确定漫游分支分数,这是很难用现有方法准确评估的。这些进展对于提高对无阻碍反应的理解至关重要,通常涉及自由基-自由基重组,这在燃料氧化、热解和污染物形成动力学机制中很普遍。研究的体系范围从碳氢化合物(包括芳香族)到氨基自由基。因此,这项工作为加速和提高理论速率常数预测的准确性提供了一个重要的新工具,代表了燃烧界的关键资产。
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引用次数: 0
Reactions of chemically activated oxosilanol formed via SiO2+H2 SiO2+H2催化氧化硅醇的化学活化反应
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-09-17 DOI: 10.1016/j.proci.2026.106454
Malte Döntgen
<div><div>The present work investigates the reactions of chemically activated oxosilanol formed via the reduction of silicon dioxide (SiO<sub>2</sub>) with hydrogen (H<sub>2</sub>), focusing on its potential as a greener alternative to traditional carbon-based processes. The study highlights the theoretical framework for understanding the potential energy surface (PES) of oxosilanol and its kinetics, comparing it to the well-studied formic acid. It is found that the reaction pathway leading to silicon monoxide (SiO) and water (H<sub>2</sub>O) is significantly faster for oxosilanol than for formic acid, despite oxosilanol having a flipped order of reactivity. This is due to, first, a smaller barrier height of <span><math><mrow><msub><mrow><mtext>SiO</mtext></mrow><mrow><mtext>2</mtext></mrow></msub><mo>+</mo><msub><mrow><mtext>H</mtext></mrow><mrow><mtext>2</mtext></mrow></msub></mrow></math></span> compared to <span><math><mrow><msub><mrow><mtext>CO</mtext></mrow><mrow><mtext>2</mtext></mrow></msub><mo>+</mo><msub><mrow><mtext>H</mtext></mrow><mrow><mtext>2</mtext></mrow></msub></mrow></math></span> and, second, <span><math><mrow><msub><mrow><mtext>SiO</mtext></mrow><mrow><mtext>2</mtext></mrow></msub><mo>+</mo><msub><mrow><mtext>H</mtext></mrow><mrow><mtext>2</mtext></mrow></msub></mrow></math></span> being entropically favored and therefore populating higher energies when forming oxosilanol. The research further explores the impact of non-Boltzmann energy distributions on well-skipping, demonstrating how these distributions can enhance reactivity in low-pressure environments. Through rigorous computational methods, including Master Equation simulations, this study provides insights into optimizing hydrogen-based silica reduction processes and suggests potential temperature reductions of up to 240 K when utilizing non-Boltzmann effects. Compared to a thermally enhanced reactivity, i.e., by increasing the temperature, the selective depositing of energy through non-Boltzmann energy distributions gives up to five orders of magnitude stronger chemical activation of the intermediate, oxosilanol. These findings lay foundation for future investigations into sustainable silicon production techniques that could contribute to carbon-neutral technologies in chemical engineering and materials science.</div><div><em>Novelty and significance statement:</em> This work presents a novel investigation of reactions involving chemically activated oxosilanol, formed via the reduction of silicon dioxide (SiO<sub>2</sub>) with hydrogen (H<sub>2</sub>). By comparing its kinetics and potential energy surfaces to the carbon analog formic acid, significantly faster well-skipping to the corresponding monoxide and water is revealed. The impact of non-Boltzmann energy distributions is explored, demonstrating potential temperature reductions in hydrogen-based silica reduction. By highlighting the enhanced kinetics under non-thermal conditions, this study paves the way for alt
本研究研究了通过氢还原二氧化硅(SiO2)形成的化学活化氧化硅醇的反应,重点研究了其作为传统碳基工艺的绿色替代品的潜力。该研究强调了理解氧硅醇势能表面(PES)及其动力学的理论框架,并将其与已被充分研究的甲酸进行了比较。研究发现,氧硅醇生成一氧化硅(SiO)和水(H2O)的反应路径明显快于甲酸,尽管氧硅醇的反应活性顺序是颠倒的。这是由于,首先,SiO2+H2的势垒高度比CO2+H2小,其次,SiO2+H2在熵上更有利,因此在形成氧硅醇时占据更高的能量。该研究进一步探讨了非玻尔兹曼能量分布对跳井的影响,证明了这些分布如何增强低压环境下的反应性。通过严格的计算方法,包括主方程模拟,本研究提供了优化氢基二氧化硅还原工艺的见解,并建议在利用非玻尔兹曼效应时,潜在的温度降低高达240 K。与热增强反应性(即通过提高温度)相比,通过非玻尔兹曼能量分布选择性沉积能量可使中间体氧硅醇的化学活性提高5个数量级。这些发现为未来对可持续硅生产技术的研究奠定了基础,这些技术可能有助于化学工程和材料科学中的碳中和技术。新颖性和意义声明:这项工作提出了一项新的研究,涉及化学活性氧化硅醇的反应,通过氢(H2)还原二氧化硅(SiO2)形成。通过将其动力学和势能表面与碳类似物甲酸进行比较,揭示了明显更快地跳井到相应的一氧化碳和水。探讨了非玻尔兹曼能量分布的影响,证明了氢基二氧化硅还原的潜在温度降低。通过强调非热条件下的增强动力学,本研究为替代气相化学过程和改进能量分布对反应速率影响的建模铺平了道路。重要的是,它说明了燃烧化学的方法如何重新用于可持续的硅生产,为绿色化学和设计更高效、更环保的工业过程提供了有价值的见解。
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引用次数: 0
A novel early detection method for ignition of flammable gases heated by a hot surface 一种由热表面加热的可燃气体着火的新型早期检测方法
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-06-19 DOI: 10.1016/j.proci.2026.106003
Tomohiko Imamura, Keita Yamada, Jun-ichi Suematsu, Masato Nakazawa, Kazunori Kuwana
This study aims to develop an early detection method for ignition based on the framework of bifurcation theory in dynamical systems. The proposed method exploits the characteristic feature of critical slowing down, namely the decrease in the recovery rate of temperature perturbations near the equilibrium between heat-release and heat-loss rates. A series of governing equations describing the temperature evolution near the ignition threshold was derived from the thermal balance, leading to a discrete-time representation of the Ornstein-Uhlenbeck (OU) process. However, the OU process assumes fluctuations around a fixed equilibrium point. In contrast, in the present system, the equilibrium temperature slowly evolves due to continuous heating. To account for this non-stationarity, we employed the measured temperature itself to compute the autocorrelation coefficient, standard deviation, and dynamic marker (DM). This formulation captures not only the local stochastic fluctuations but also the gradual drift of the equilibrium temperature. As ignition approached, the time evolution of the autocorrelation coefficient and standard deviation exhibited a transition from decreasing to increasing behavior in the ignition cases. This distinction became more pronounced when using the dynamic marker, defined as the product of the autocorrelation coefficient and the normalized standard deviation. The thresholds of DM, its temporal derivative, and the required number of consecutive detections were determined using receiver operating characteristic (ROC) analysis and probability density function (PDF) analysis. Using the optimized thresholds, ignition was detected with a lead time on the order of minutes before the actual event with an accuracy exceeding 90% for the present ignition problem. These results demonstrate that the proposed method provides sufficient lead time for early fire-response actions and offers a practical framework for ignition-risk mitigation in fire safety engineering.
Novelty and significance statement: This study presents a novel framework that treats ignition as a nonlinear bifurcation phenomenon. The key contribution of this work is the development of an early-ignition detection system based on early-warning signal (EWS) theory, implemented through statistical analysis of measured temperature data. Conventional EWS theory assumes fluctuations around a stationary equilibrium point and has therefore not been directly applicable to systems in which the equilibrium state slowly drifts. Extending the framework to accommodate such non-stationary behavior represents a significant theoretical advancement. The developed system provides a lead time on the order of minutes prior to ignition, offering sufficient time for initial fire-response actions. These results demonstrate the high practical significance and performance of the proposed ignition-detection method.
本研究旨在建立一种基于动力系统分岔理论框架的点火早期检测方法。所提出的方法利用了临界慢化的特征,即在热释放率和热损失率之间的平衡附近温度扰动的恢复速率降低。从热平衡中导出了一系列描述点火阈值附近温度演变的控制方程,从而得到了Ornstein-Uhlenbeck (OU)过程的离散时间表示。然而,OU过程假设在一个固定的平衡点周围波动。相反,在目前的系统中,平衡温度由于持续加热而缓慢变化。为了解释这种非平稳性,我们使用测量温度本身来计算自相关系数、标准差和动态标记(DM)。这个公式不仅捕捉到了局部的随机波动,而且也捕捉到了平衡温度的逐渐漂移。随着点火的临近,自相关系数和标准差的时间演化呈现出由减小到增大的变化趋势。当使用动态标记时,这种区别变得更加明显,动态标记被定义为自相关系数和标准化标准差的乘积。采用受试者工作特征(ROC)分析和概率密度函数(PDF)分析确定DM的阈值、时间导数和连续检测所需的次数。利用优化的阈值,在实际事件发生前几分钟检测到点火,对于当前的点火问题,精度超过90%。这些结果表明,该方法为早期火灾响应行动提供了足够的提前时间,并为消防安全工程中的火灾风险缓解提供了一个实用的框架。新颖性和意义声明:本研究提出了一种将点火视为非线性分岔现象的新框架。这项工作的关键贡献是基于预警信号(EWS)理论的早燃检测系统的开发,该系统通过对测量温度数据的统计分析来实现。传统的EWS理论假定在一个平稳的平衡点周围有波动,因此不能直接适用于平衡状态缓慢漂移的系统。扩展框架以适应这种非平稳行为是一个重要的理论进步。开发的系统提供了点火前几分钟的提前时间,为初始火灾响应行动提供了足够的时间。结果表明,该方法具有较高的实际意义和性能。
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引用次数: 0
A dual-criterion model for predicting LDPE electrical wire flammability limits in diluent gas environments 预测LDPE电线在稀释气体环境下可燃性极限的双准则模型
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-06-26 DOI: 10.1016/j.proci.2026.106098
Yuxuan Ma, Shiyu Ding, Zhengda Guo, Yan Gu, Longhua Hu
<div><div>Nitrogen (N₂), argon (Ar), and carbon dioxide (CO₂) are commonly used as diluent gases to reduce electrical fire risks in unattended environments and as clean agents in fire-suppression. This work investigated the limiting oxygen concentrations (LOCs) of low-density polyethylene (LDPE) electrical wires in N₂, Ar, and CO₂ diluted opposed flows. The results showed that CO₂ exhibited the strongest suppression effect, yielding the highest LOC, whereas Ar produced the lowest. Molten LDPE droplets formed and periodically detached from the wire surface, which may quench the flame on NiCr-core wires. The critical droplet volume, and the heat rate required to initiate droplet motion and prevent flame quenching, were quantified. A dual-criterion model was developed by coupling the stable solutions of the gas- and solid-phase energy balance equations. The gas criterion (LOC<sub>g</sub>) defines the minimum oxygen concentration required to sustain flame thermal equilibrium, while the solid criterion (LOC<sub>s</sub>) describes the balance among flame heat feedback, sensible heating, solid-surface re-radiation, and droplet cooling. The global limit is defined as LOC = max [LOC<sub>g</sub>, LOC<sub>s</sub>], and the omission of either criterion may cause errors. The predicted LOC curves and flame temperatures agreed well with experiments, validating both the overall model and its sub-models. Extinction-regime maps show that, under normal gravity, NiCr-core wires are mainly limited by droplet-induced quenching, while Cu-core wires are strongly affected by solid-surface re-radiation. Under microgravity, radiative losses become more important: NiCr-core wires shift from blowoff at high flow velocities to solid-surface re-radiation at low velocities, whereas Cu-core wires remain strongly influenced by solid-surface re-radiation over a broad velocity range. These findings provide a physics-based basis for improving flammability-limit prediction of solid materials, and for selecting and screening clean suppressants by linking each diluent gas to a distinct extinction pathway in normal- and microgravity.</div></div><div><h3>Novelty and significance statement</h3><div>This study establishes a dual-criterion model to predict the LOCs of electrical wires in diluent-gas environments. Unlike conventional scaling models based only on solid-phase energy balance, the model couples the stable solutions of gas- and solid-phase energy equations. It captures both flame thermal equilibrium and solid-surface heat balance, and introduces a thermal-inertia term to represent droplet-motion effects. Model parameters are trained and validated against experiments. The extinction-regime maps clearly show why classical models may miss the true minimum LOC (MLOC), where gas-phase radiation, flame stretch, and chemical kinetics decouple from the solid response. The model reproduces LOC trends across environments and guides fire-safety design for electrical and spacecraft systems.<
氮气(N₂)、氩气(Ar)和二氧化碳(CO₂)通常用作稀释气体,以减少无人值勤环境中的电气火灾风险,并在灭火中用作清洁剂。本文研究了低密度聚乙烯(LDPE)电线在N₂、Ar和CO₂稀释的反向流动中的极限氧浓度(LOCs)。结果表明,CO₂的抑制作用最强,LOC最高,Ar最低。熔融的LDPE液滴形成并周期性地从导线表面脱落,这可能会熄灭nicr芯线上的火焰。量化了临界液滴体积,以及启动液滴运动和防止火焰淬火所需的热速率。通过耦合气固两相能量平衡方程的稳定解,建立了双准则模型。气体判据(LOCg)定义了维持火焰热平衡所需的最低氧浓度,而固体判据(LOCs)描述了火焰热反馈、显热、固体表面再辐射和液滴冷却之间的平衡。全局限制定义为LOC = max [log, los],遗漏任何一个标准都可能导致错误。预测的LOC曲线和火焰温度与实验结果吻合较好,验证了整体模型及其子模型的正确性。消光状态图显示,在正常重力下,nicr芯线主要受液滴诱导淬火的限制,而cu芯线则受固体表面再辐射的强烈影响。在微重力条件下,辐射损失变得更加重要:nicr芯导线从高流速下的吹散转向低速下的固体表面再辐射,而cu芯导线在较宽的流速范围内仍然受到固体表面再辐射的强烈影响。这些发现为改善固体材料的可燃性极限预测,以及通过将每个稀释气体连接到正常和微重力下不同的熄灭途径来选择和筛选清洁抑制剂提供了物理基础。新颖性和意义声明本研究建立了一种双准则模型来预测稀释气体环境下电线的loc。与传统的仅基于固相能量平衡的标度模型不同,该模型耦合了气相和固相能量方程的稳定解。它捕获了火焰热平衡和固体表面热平衡,并引入了热惯性项来表示液滴运动效应。对模型参数进行了训练,并通过实验进行了验证。消光状态图清楚地显示了为什么经典模型可能会错过真正的最小LOC (MLOC),其中气相辐射,火焰拉伸和化学动力学与固体响应分离。该模型再现了各种环境的LOC趋势,并指导电气和航天器系统的防火安全设计。
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引用次数: 0
An improved critical velocity gradient model for laminar boundary layer flashback of NH3/H2/air flames 改进的NH3/H2/空气火焰层流边界层闪回临界速度梯度模型
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-06-19 DOI: 10.1016/j.proci.2026.106042
Zhaofan Zhu, Haiou Wang, Evatt R. Hawkes, Shibo Gu, Haiwang Li, Kun Luo, Jianren Fan
<div><div>Accurately predicting the boundary layer flashback limit is crucial for the safety of combustion systems. In the present study, two-dimensional numerical simulations of laminar boundary layer flashback are conducted for a series of <span><math><msub><mrow><mi>NH</mi></mrow><mrow><mn>3</mn></mrow></msub></math></span>/<span><math><msub><mrow><mi>H</mi></mrow><mrow><mn>2</mn></mrow></msub></math></span>/air mixtures with varying equivalence ratios and hydrogen blending ratios. The critical velocity gradient for flashback is efficiently determined using an inlet velocity gradient active-control approach, which significantly reduces the computational cost compared to previous methods. The flow and flame characteristics at the flashback limit are examined. It is observed that the streamwise velocity upstream of the flame decreases due to the combustion-induced local pressure rise. The streamlines bend upward ahead of the flame under the influence of the adverse pressure gradient. In the cases with large penetration distances, the streamlines noticeably bend downward within the penetration distance as they approach the flame, further amplifying the reduction in streamwise velocity. The flame speed at the penetration distance is influenced by differential diffusion, flame stretch, and wall heat loss. The discrepancy between the flame speed at the penetration distance and the flame speed predicted by the linear stretch model is found to be negatively correlated with the ratio of the penetration distance to the flame diffusion thickness, <em>i.e</em>, <span><math><mrow><msub><mrow><mi>δ</mi></mrow><mrow><mi>p</mi></mrow></msub><mo>/</mo><msub><mrow><mi>δ</mi></mrow><mrow><mi>D</mi></mrow></msub></mrow></math></span>. An improved critical velocity gradient model is therefore proposed, which accounts for the flow velocity reduction ahead of the flame, and the variation in flame speed at the flame leading point. Compared to the classical criterion, the proposed model significantly improves the accuracy of flashback limit prediction.</div><div><em>Novelty and significance statement:</em> Accurately predicting the boundary layer flashback is a critical challenge in the combustion applications of <span><math><msub><mrow><mi>NH</mi></mrow><mrow><mn>3</mn></mrow></msub></math></span>/<span><math><msub><mrow><mi>H</mi></mrow><mrow><mn>2</mn></mrow></msub></math></span> mixtures. This study investigates the boundary layer flashback limit for a series of laminar <span><math><msub><mrow><mi>NH</mi></mrow><mrow><mn>3</mn></mrow></msub></math></span>/<span><math><msub><mrow><mi>H</mi></mrow><mrow><mn>2</mn></mrow></msub></math></span>/air flames with varying equivalence ratios and <span><math><msub><mrow><mi>H</mi></mrow><mrow><mn>2</mn></mrow></msub></math></span> blending ratios. An inlet velocity gradient active-control approach is proposed to obtain the critical velocity gradient for flashback, significantly reducing the computational cost compared to pre
准确预测边界层闪回极限对燃烧系统的安全至关重要。在本研究中,对一系列不同当量比和氢气混合比的NH3/H2/空气混合物进行了层流边界层闪回的二维数值模拟。采用入口速度梯度主动控制方法有效地确定了闪回的临界速度梯度,与以前的方法相比,显著降低了计算成本。研究了闪回极限下的流动和火焰特性。观察到,由于燃烧引起的局部压力升高,火焰上游的流向速度减小。在逆压梯度的影响下,流线在火焰前方向上弯曲。在大侵彻距离的情况下,流线在接近火焰的侵彻距离内明显向下弯曲,进一步放大了沿流速度的减小。穿透距离处的火焰速度受微分扩散、火焰拉伸和壁面热损失的影响。发现穿透距离处的火焰速度与线性拉伸模型预测的火焰速度之差与穿透距离与火焰扩散厚度之比δp/δD呈负相关。因此,提出了一种改进的临界速度梯度模型,该模型考虑了火焰前方的流速降低和火焰导点处的火焰速度变化。与经典准则相比,该模型显著提高了闪回极限预测的准确性。新颖性和意义声明:在NH3/H2混合物的燃烧应用中,准确预测边界层闪回是一个关键的挑战。本文研究了一系列具有不同当量比和H2混合比的层流NH3/H2/空气火焰的边界层闪回极限。提出了一种进口速度梯度主动控制方法来获得回闪的临界速度梯度,与以往的方法相比,显著降低了计算成本。揭示了在闪回极限处壁面附近流动与火焰的相互作用,有助于理解边界层闪回的潜在机制。对临界速度梯度模型进行了两种修正,考虑了火焰上游流动速度的减小和火焰导点处火焰速度的变化。与经典模型相比,改进模型显著提高了闪回极限预测的准确性。
{"title":"An improved critical velocity gradient model for laminar boundary layer flashback of NH3/H2/air flames","authors":"Zhaofan Zhu,&nbsp;Haiou Wang,&nbsp;Evatt R. Hawkes,&nbsp;Shibo Gu,&nbsp;Haiwang Li,&nbsp;Kun Luo,&nbsp;Jianren Fan","doi":"10.1016/j.proci.2026.106042","DOIUrl":"10.1016/j.proci.2026.106042","url":null,"abstract":"&lt;div&gt;&lt;div&gt;Accurately predicting the boundary layer flashback limit is crucial for the safety of combustion systems. In the present study, two-dimensional numerical simulations of laminar boundary layer flashback are conducted for a series of &lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;NH&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;3&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt;/&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;H&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt;/air mixtures with varying equivalence ratios and hydrogen blending ratios. The critical velocity gradient for flashback is efficiently determined using an inlet velocity gradient active-control approach, which significantly reduces the computational cost compared to previous methods. The flow and flame characteristics at the flashback limit are examined. It is observed that the streamwise velocity upstream of the flame decreases due to the combustion-induced local pressure rise. The streamlines bend upward ahead of the flame under the influence of the adverse pressure gradient. In the cases with large penetration distances, the streamlines noticeably bend downward within the penetration distance as they approach the flame, further amplifying the reduction in streamwise velocity. The flame speed at the penetration distance is influenced by differential diffusion, flame stretch, and wall heat loss. The discrepancy between the flame speed at the penetration distance and the flame speed predicted by the linear stretch model is found to be negatively correlated with the ratio of the penetration distance to the flame diffusion thickness, &lt;em&gt;i.e&lt;/em&gt;, &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;δ&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;p&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;mo&gt;/&lt;/mo&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;δ&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;D&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;. An improved critical velocity gradient model is therefore proposed, which accounts for the flow velocity reduction ahead of the flame, and the variation in flame speed at the flame leading point. Compared to the classical criterion, the proposed model significantly improves the accuracy of flashback limit prediction.&lt;/div&gt;&lt;div&gt;&lt;em&gt;Novelty and significance statement:&lt;/em&gt; Accurately predicting the boundary layer flashback is a critical challenge in the combustion applications of &lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;NH&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;3&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt;/&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;H&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt; mixtures. This study investigates the boundary layer flashback limit for a series of laminar &lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;NH&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;3&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt;/&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;H&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt;/air flames with varying equivalence ratios and &lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;H&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt; blending ratios. An inlet velocity gradient active-control approach is proposed to obtain the critical velocity gradient for flashback, significantly reducing the computational cost compared to pre","PeriodicalId":408,"journal":{"name":"Proceedings of the Combustion Institute","volume":"42 ","pages":"Article 106042"},"PeriodicalIF":4.6,"publicationDate":"2026-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148567574","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Surface nitridation of nickel by NH3/H2 rich flames at elevated temperature 高温富NH3/H2火焰对镍的表面氮化
IF 4.6 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2026-01-01 Epub Date: 2026-06-19 DOI: 10.1016/j.proci.2026.106020
Yupan Bao, Liang Ji, Raphael Vogeley, Kaii Ri, Wenbin Xu, Zhiyuan Zhang, Yijie Xu, Bowen Mei, Huixin He, Christian Brackmann, Tao Li, Yiguang Ju
Surface nitridation induced by ammonia combustion can alter material properties, reducing lifetime and performance of a practical combustor. Although ammonia-induced surface nitriding has been studied at low and moderate temperatures, its behavior at temperatures above 1200 K in flames remains unexplored. This study investigates high-temperature nitriding and the impact of NH radical of nickel rods exposed to NH3/H2 flames above 1500 K. The presence of abundant radicals and complex chemical reactions in NH3/H2 flames, together with flame–wall interactions between reactive gases and metal surfaces, impose great challenges in understanding the underlying nitridation mechanism. In this work, gas-phase characterization was performed using in-situ planar laser-induced fluorescence (PLIF) for NH radical distribution and Rayleigh scattering for temperature, while surface morphology and chemical composition were analyzed by scanning electron microscopy (SEM) and high-resolution X-ray photoelectron spectroscopy (HRXPS). The results show that nickel nitridation can occur within minutes of flame exposure and is strongly dependent on NH concentration at a same flame temperature. In addition, no distinct nitride layer was observed after more than one hour of flame exposure, while pore structures beneath the nickel surface were detected using ion-beam cutting under high vacuum. These observations suggest that high-temperature nitridation under ammonia combustion conditions may proceed through mechanisms that differ from those typically reported at lower temperatures.

Novelty and significance statement

This study presents the first high-temperature experimental investigation of nickel nitridation under ammonia/hydrogen combustion conditions exceeding 1500 K, moving beyond the moderate-temperature (<1200 K) and non-flame studies that dominate existing literature. By combining operando planar laser-induced fluorescence (PLIF) for NH radicals with ex-situ high-resolution X-ray photoelectron spectroscopy (HRXPS) and scanning electron microscopy (SEM) analysis, the study directly links radical chemistry in the reacting flow to surface phase evolution and microstructural transformation. The findings, characterized by rapid nitride formation, radical-mediated nitrogen incorporation, and lattice instability, highlight that the flame-wall interactions at 1600 K are different from low and moderate temperatures. These insights are essential for predicting material degradation in ammonia-based energy systems and for guiding the design of high-temperature metal components with improved resistance to nitridation and/or oxidation.
氨燃烧引起的表面氮化会改变材料的性能,降低燃烧器的使用寿命和性能。虽然氨诱导的表面氮化已经在低温和中温下进行了研究,但其在1200 K以上的火焰中的行为仍未被探索。研究了1500 K以上NH3/H2火焰对镍棒高温氮化及nhh自由基的影响。NH3/H2火焰中存在丰富的自由基和复杂的化学反应,以及反应气体与金属表面之间的火焰壁相互作用,给理解潜在的氮化机制带来了巨大的挑战。本研究采用原位平面激光诱导荧光(PLIF)和瑞利散射(Rayleigh散射)对nhh自由基分布进行气相表征,并通过扫描电镜(SEM)和高分辨率x射线光电子能谱(HRXPS)分析表面形貌和化学成分。结果表明,在相同的火焰温度下,镍氮化反应可以在几分钟内发生,并且强烈依赖于NH浓度。此外,在火焰照射1小时以上后,没有观察到明显的氮化物层,而在高真空下使用离子束切割可以检测到镍表面下的孔隙结构。这些观察结果表明,在氨燃烧条件下的高温氮化可能通过不同于在较低温度下通常报道的机制进行。该研究首次提出了在超过1500 K的氨/氢燃烧条件下镍氮化的高温实验研究,超越了现有文献中占主导地位的中温(<1200 K)和非火焰研究。通过对nhh自由基的操作平面激光诱导荧光(PLIF)与离地高分辨率x射线光电子能谱(HRXPS)和扫描电镜(SEM)分析相结合,该研究将反应流中的自由基化学与表面相演化和微观结构转变直接联系起来。研究结果以快速氮化物形成、自由基介导的氮掺入和晶格不稳定性为特征,强调了1600 K下的火焰壁相互作用不同于低温和中温。这些见解对于预测氨基能源系统中的材料降解以及指导设计具有更好的抗氮化和/或氧化性的高温金属部件至关重要。
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引用次数: 0
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Proceedings of the Combustion Institute
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