主管部门: 中国航天科技集团有限公司
主办单位: 中国航天空气动力技术研究院
中国宇航学会
中国宇航出版有限责任公司

火箭上面级氢氧内燃机燃烧性能

Combustion Performance of Upper Stage Hydrogen-Oxygen Internal Combustion Engines

  • 摘要: 流体集成系统(integrated vehicle fluids, IVF)中氢氧内燃机起着关键作用, 以进气道喷射氢气(port fuel injection-hydrogen, PFI-H2)喷注策略为研究目标, 研究该喷射方式下缸内燃烧特性、输出功率等参数, 从多角度分析氢内燃机燃烧性能, 建立用于IVF系统氢氧内燃机的PFI-H2燃烧策略。为此, 基于GT-power仿真软件, 搭建PFI-H2一维仿真模型, 并通过点火性能数据对仿真模型进行校核。结果表明, 一维燃烧性能仿真分析可以得到不同工况下氢氧内燃机输出功率, 功率在6~8 kW符合设计要求, 有效热效率为29.17%~30.08%, 且此区间的排气能量占比变化不大, 集中在46%~48%。

     

    Abstract: In the integrated vehicle fluids (IVF) system, hydrogen-oxygen internal combustion engines play a crucial role, with a focus on the port fuel injection-hydrogen (PFI-H2) strategy into the intake manifold. The research aims to study cylinder combustion characteristics, output power, and other parameters under this injection strategy, analyzing hydrogen internal combustion engine performance from multiple perspectives. In order to establish a PFI-H2 combustion strategy for hydrogen-oxygen internal combustion engines used in IVF systems, a one-dimensional simulation model for PFI-H2 was constructed using GT-power simulation software. The simulation model was validated using ignition performance data. The results indicate that the one-dimensional combustion performance simulation can provide output power of hydrogen-oxygen internal combustion engines under different operating conditions. The power ranges from 6 to 8 kW, which meets design requirements. The effective thermal efficiency ranges from 29.17% to 30.08%, and the proportion of exhaust energy in this region has little change, concentrated in 46%~48%.

     

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