推进技术 ›› 1998, Vol. 19 ›› Issue (1): 95-98.

• • 上一篇    下一篇

多孔毛细陶瓷试棒燃油蒸发与渗透性能的实验研究

杜声同,孙惠贤,陈建和,陈炳录   

  1. 西北工业大学航空动力与热力工程系;西北工业大学航空动力与热力工程系;西北工业大学航空动力与热力工程系;西北工业大学航空动力与热力工程系
  • 发布日期:2021-08-15

AN EXPERIMENTAL STUDY OF SOME FUNDAMENTAL PROPERTIES FOR IMPROVING COMBUSTION IN CERAMIC COMBUSTOR

  1. Dept of Aeroengine engineering,Northwestern Polytechnical Univ ,Xi′an,710072;Dept of Aeroengine engineering,Northwestern Polytechnical Univ ,Xi′an,710072;Dept of Aeroengine engineering,Northwestern Polytechnical Univ ,Xi′an,710072;Dept of Aeroengine engineering,Northwestern Polytechnical Univ ,Xi′an,710072
  • Published:2021-08-15

摘要: 研究了多孔毛细陶瓷试棒的燃油渗透、蒸发性能与温度、气孔率及气流速度的关系,并对单直毛细孔的渗透、蒸发及裂解等模型作了分析。

关键词: 陶瓷;孔隙率;推进剂蒸发;渗透率

Abstract: The properties of permeation and evaporation of fuel through porous capillary ceramic rod is investigated The relation between the permeation,evaporation of fuel and the porosity,air velocity of test rod is studied The model of permeation evaporation and cracking in a single straight capillary is presented It is suggested that a new injector or flame stabilizer can be made of porous capillary ceramic material

Key words: Ceramic material;Porosity;Propellant evaporation;Permeability