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Impinging Jet Ignition Studies of Hydrogen Peroxide with Gelled Fuel Rendered Hypergolic by Addition of Reactive Particles

机译:通过添加反应性颗粒的胶凝燃料制成的高双螺旋撞击过氧化氢的喷气点火研究

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Impinging jet experiments were conducted using doublet, triplet, and quintuplet injector configurations to measure ignition delay of hydrogen peroxide (H_2O_2) with gelled hydrocarbon fuel containing reactive particles. The addition of this material, sodium borohydride, renders the reactants hypergolic. Variation of fuel chemical properties (reactive particle size), and impinging jet characteristics (equivalence ratio, impingement velocity, velocity ratio, momentum ratio, and momentum flux ratio) were investigated to determine their effect on ignition delay. Cold flow and impinging jet ignition experiments were coupled to develop an understanding of system startup transient effects as well. Gelled fuels containing sieved particles indicate first light times are independent of particle size, while average ignition onset times decreased when the particle size was reduced. Increasing the target flow velocity range (the ratio of fuel/oxidizer velocities being held constant) from approximately 0.8 to 14.6 m/s (fuel velocity), indicated first light tunes consistently decreased while ignition delay decreased with increasing velocity until a plateau was achieved around 5 m/s. Investigation of global equivalence ratio effects, and experiments in which the oxidizer flow conditions were varied relative to the fuel conditions (at a fixed target equivalence ratio) also showed a relative independence of such conditions on the ignition delay time. Doublet and triplet injector configurations produced comparable first light and ignition onset times, while the average ignition time for the quintuplet injector configuration was nearly doubled. The quintuplet injector configuration produced a conical flow structure down stream of impingement, while the doublet and triplet configurations produced fans. Transition of flow conditions downstream of impingement may have detrimentally influenced ignition for the quintuplet configuration by affecting the overall reactive surface area and volume in which the reactants are distributed, reducing the local volumetric energy density. These results indicate more complex multi-injector geometries are not necessary to achieve short ignition delay times for this system.
机译:使用双峰,三峰和五重峰喷射器配置进行了冲击喷射实验,以测量含反应性颗粒的胶凝烃燃料中过氧化氢(H_2O_2)的点火延迟。该材料硼氢化钠的添加使反应物具有高配伍性。研究了燃料化学性质(反应性粒径)和撞击喷射特性(当量比,撞击速度,速度比,动量比和动量通量比)的变化,以确定它们对点火延迟的影响。结合冷流和冲击射流点火实验也可以增进对系统启动瞬态效应的了解。包含筛分颗粒的胶凝燃料表明,初次点火时间与颗粒大小无关,而当减小颗粒大小时,平均起燃时间减少。将目标流速范围(燃料/氧化剂速度的比率保持恒定)从大约0.8增至14.6 m / s(燃料速度),表明第一光调谐始终减小,而点火延迟则随速度增加而减小,直到达到平稳状态为止。 5 m / s。对整体当量比影响的研究以及氧化剂流量条件相对于燃料条件(以固定的目标当量比)变化的实验也表明,这种条件对点火延迟时间具有相对的独立性。双联和三联喷油器配置产生了可比的首次点火和点火开始时间,而五联喷油器配置的平均点火时间几乎增加了一倍。五重喷射器配置在撞击的下游产生了圆锥形的流动结构,而双联和三联配置则产生了风扇。撞击下游流动条件的转变可能会通过影响反应物分布的总反应表面积和体积,降低局部体积能量密度,从而对五联体构型的燃烧产生不利影响。这些结果表明,对于该系统而言,不需要更复杂的多喷射器几何形状即可实现较短的点火延迟时间。

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