Thermal Decomposition Kinetics of Jet A-1, HEFA-SAF and Jet A-1/HEFA-SAF Blends under Oxidative Atmosphere for Aeronautical Applications

IF 5.3 3区 工程技术 Q2 ENERGY & FUELS
Abdulwasiu Muhammed Raji*, Brady Manescau, Khaled Chetehouna, Christelle Roudaut*, Laurent Lemee and Mehrad Tarighi, 
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Abstract

This study investigates the thermal decomposition and kinetic behavior of pure Jet A-1, hydroprocessed esters and fatty acids sustainable aviation fuel (HEFA-SAF), and their volumetric blends (50/50, 30/70, and 10/90) under oxidative conditions and heating rates (5, 10, and 15 °C/min) using thermogravimetric analysis (TGA) and model-free kinetic models in NETZSCH Neo Kinetics software. Both Jet A-1 and HEFA-SAF exhibit single-step mass loss events, but HEFA-SAF decomposes at higher temperatures (onset >160 °C, DTGmax up to 203 °C at 15 °C/min), indicating superior thermal stability. Among the blends, the Jet A-1/HEFA-SAF 10/90 blend demonstrated the highest thermal stability with the highest peak decomposition and burnout temperatures. Increasing the HEFA-SAF content reduced the mass loss rates and enhanced oxidative resistance. Kinetic modeling validated a single-step degradation mechanism across all samples. HEFA-SAF consistently showed higher activation energies (up to 93 kJ/mol), high pre-exponential factors (A = 2.95 × 1020 s–1) and stronger regression coefficient (R2 = 0.998), confirming its enhanced bond strength and stability. The Friedman model proved to be the most appropriate to describe the decomposition behavior of all the samples tested due to its sensitivity to conversion-dependent reactions. This permits more precise tracking of changes in Ea in the decomposition process, particularly in thermally complex fuel systems such as Jet A-1/HEFA-SAF blends. The combined use of the KAS and Friedman models improved the interpretation accuracy. These findings underscore HEFA-SAF’s potential as a thermally stable, sustainable aviation fuel with improved combustion efficiency and long-term storage performance compared to those of conventional Jet A-1.

Abstract Image

航空用Jet A-1、HEFA-SAF及Jet A-1/HEFA-SAF共混物在氧化气氛下的热分解动力学
本研究利用热重分析(TGA)和NETZSCH Neo Kinetics软件中的无模型动力学模型,研究了纯Jet A-1、加氢加工酯和脂肪酸可持续航空燃料(HEFA-SAF)及其体积混合物(50/50、30/70和10/90)在氧化条件和加热速率(5、10和15°C/min)下的热分解和动力学行为。Jet A-1和HEFA-SAF均表现为单步质量损失事件,但HEFA-SAF在更高的温度下分解(起始温度>;160°C, DTGmax在15°C/min下高达203°C),表明具有更好的热稳定性。在共混物中,Jet A-1/HEFA-SAF 10/90共混物表现出最高的热稳定性,其峰值分解温度和燃尽温度最高。增加HEFA-SAF含量降低了质量损失率,增强了抗氧化能力。动力学模型验证了所有样品的单步降解机制。HEFA-SAF具有较高的活化能(最高可达93 kJ/mol)、较高的指前因子(A = 2.95 × 1020 s-1)和较强的回归系数(R2 = 0.998),表明其具有较好的结合强度和稳定性。弗里德曼模型被证明是最适合描述所有样品的分解行为,因为它对依赖于转化的反应很敏感。这可以更精确地跟踪分解过程中Ea的变化,特别是在热复杂的燃料系统中,如Jet A-1/HEFA-SAF混合物。KAS和Friedman模型的联合使用提高了解释精度。这些发现强调了HEFA-SAF作为一种热稳定、可持续的航空燃料的潜力,与传统的Jet a -1相比,HEFA-SAF具有更高的燃烧效率和长期储存性能。
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来源期刊
Energy & Fuels
Energy & Fuels 工程技术-工程:化工
CiteScore
9.20
自引率
13.20%
发文量
1101
审稿时长
2.1 months
期刊介绍: Energy & Fuels publishes reports of research in the technical area defined by the intersection of the disciplines of chemistry and chemical engineering and the application domain of non-nuclear energy and fuels. This includes research directed at the formation of, exploration for, and production of fossil fuels and biomass; the properties and structure or molecular composition of both raw fuels and refined products; the chemistry involved in the processing and utilization of fuels; fuel cells and their applications; and the analytical and instrumental techniques used in investigations of the foregoing areas.
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