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Conceptual design of high-speed underwater jet engine using high concentration of hydrogen peroxide

机译:高浓度过氧化氢高速水下喷气发动机的概念设计

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摘要

The conceptual design of high-speed underwater jet engine was conducted and demonstrated using high concentration of hydrogen peroxide as a green propellant. On the basis of the principles of steam jet ejector, the central water jet configuration was applied for the engine where a central water jet was surrounded by an annular steam flow. The annular steam flow as the primary fluid was the decomposition gas of hydrogen peroxide and cold water was the secondary fluid. The catalyst pack was composed of the alumina pellets doped with manganese oxides. The performance evaluation of the engine was performed without the flow field of the secondary fluid. The demonstrator successfully generated a practical propulsive force, which could be applied for the systems of unmanned underwater vehicles. For design of experiments, the nozzle exit areas were dealt with. It should be ensured that the exit area of nozzle was sufficiently large to prevent thrust instabilities due to the disturbance in the high-speed flows. In contrast, the excessively large area of the nozzle exit might decrease the efficiency of the engine performance in that the geometry of the engine failed to encourage the heat energy transfer between the primary and the secondary fluids.
机译:进行了高速水下喷气发动机的概念设计,并使用高浓度的过氧化氢作为绿色推进剂进行了演示。根据蒸汽喷射器的原理,将中央水喷射配置应用于发动机,其中中央水喷射被环形蒸汽流包围。作为主要流体的环形蒸汽流是过氧化氢的分解气体,而冷水是辅助流体。催化剂包由掺杂有锰氧化物的氧化铝粒料组成。在没有二次流体的流场的情况下进行了发动机的性能评估。演示者成功地产生了一种实用的推进力,该推进力可用于无人水下航行器的系统。为了进行实验设计,处理了喷嘴出口区域。应确保喷嘴的出口面积足够大,以防止由于高速流动的干扰而引起推力不稳定性。相反,喷嘴出口的过大面积可能降低发动机性能的效率,因为发动机的几何形状无法促进热能在一次和二次流体之间传递。

著录项

  • 来源
    《Ocean Engineering 》 |2018年第1期| 193-200| 共8页
  • 作者单位

    Korea Inst Machinery & Mat, 156 Gajeongbuk Ro, Daejeon 34103, South Korea;

    Korea Adv Inst Sci & Technol, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea;

    Korea Adv Inst Sci & Technol, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea;

    Korea Adv Inst Sci & Technol, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea;

    Korea Adv Inst Sci & Technol, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Hydrogen peroxide; Decomposition; Catalyst; Steam ejector; Jet propulsion;

    机译:过氧化氢;分解;催化剂;蒸汽喷射器;喷射推进;

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