航空汽油高能化改性:JP-10调合策略和ReaxFF分子动力学模拟
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    摘要:

    为提升航空活塞式无人机续航能力,本文提出基于高密度烃类燃料JP-10的能量密度提升策略。以100LL航空汽油为基础油,通过调合体积分数30%的JP-10制备新型高能航空汽油(GR-1)。研究表明,GR-1的体积热值达33.51 MJ.L?1,较100LL航空汽油提升11.50%,且其他理化指标基本满足《航空活塞式发动机燃料》(GB 1787-2018)标准要求。进一步采用反应力场分子动力学模拟(ReaxFF MD)揭示了GR-1的氧化燃烧机理:燃烧过程分为分子活化、燃料热解、小分子氧化和深度氧化四阶段;JP-10的加入使燃料初始裂解温度降至1300 K,低于100LL航空汽油的2000 K,同时未显著影响最终氧化路径。本研究为高能航空燃料设计及无人机续航能力提升提供了理论和实验依据。

    Abstract:

    To enhance the endurance of aviation piston-powered unmanned aerial vehicles (UAVs), this study proposes an energy density enhancement strategy utilizing the high-density hydrocarbon fuel JP-10. A novel high-energy aviation gasoline (designated as GR-1) was synthesized by blending the 100LL aviation gasoline with 30 vol% JP-10. Experimental characterization demonstrates that GR-1 presented a volumetric heating value of 33.51 MJ·L?1, achieving an 11.50% increase over that of the base 100LL fuel, and its essential physicochemical specifications met the requirements outlined in the Chinese National Standard Aviation Piston Engine Fuels (GB 1787-2018). Furthermore, Reactive Force Field Molecular Dynamics (ReaxFF MD) simulations elucidated the oxidation mechanism of GR-1, revealing a four-stage combustion process: molecular activation, fuel pyrolysis, small-molecule oxidation, and deep oxidation. The incorporation of JP-10 significantly reduced the initial fuel cracking temperature to 1300 K, 700 K lower than that observed for the 100LL aviation gasoline (2000 K), while maintaining unaltered final oxidation pathways. This work provides fundamental theoretical and experimental foundations for the design of high-energy aviation fuels and the advancement of UAV endurance capabilities.

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  • 收稿日期:2025-08-17
  • 最后修改日期:2025-09-12
  • 录用日期:2025-10-16
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