期刊文献+

燃料裂解特性对供油系统稳定性的影响 被引量:3

Effects of Fuel Cracking Characteristic on Stability of Fuel Supply System
下载PDF
导出
摘要 通过实验研究发现了超临界吸热型碳氢燃料供油系统的压力降型不稳定现象。为了研究稳定机理和超临界吸热型碳氢燃料裂解特性对供油系统稳定性的影响,建立了零维平衡流模型,并针对不同裂解特性的燃料进行了对比仿真。研究结果表明,由于裂解反应的发生,超临界碳氢燃料供油系统存在临界区和裂解区两个不稳定区间。基于零维平衡流模型较好地复现不稳定实验现象,不稳定机理得到了详细的解释。密度随温度的变化是系统正反馈的重要环节之一,其剧烈的变化率是导致系统不稳定的主要原因,燃油裂解速率越快,其裂解产物密度相对变化率随温度变化越大,越容易引起供油系统的不稳定。 Pressure drop type instability of supercritical endothermic hydrocarbon fuel supply system was founded in an experiment. In order to analyze the instability mechanism and the effects of fuel cracking characteristic on the stability of the fuel supply system, a zero-dimension homogeneous model was established. Instability simulation results of fuel with different cracking characteristic were compared. The results show that there exist two instable region in the supercritical hydrocarbon fuel supply system, namely, criti- cal temperature region and cracking temperature region. Based on the excellent agreement between the ex- periment data and the simulation results calculated by the zero-dimension homogeneous model, the instable mechanism is interpreted. As a link in the positive feedback loop, the acute decrease of the fuel density is a main factor resulting in the instable phenomenon. Based on the compared simulation results, the more a- cute the density changes with temperature while the fuel is cracking, the more instable the system will be.
出处 《推进技术》 EI CAS CSCD 北大核心 2013年第12期1702-1707,共6页 Journal of Propulsion Technology
关键词 冷却系统 碳氢燃料 不稳定 裂解 Cooling system Hydrocarbon fuel Instability Cracking
  • 相关文献

参考文献14

  • 1Bates RW, Edwards T, Meyer ML. Heat Transfer and Deposition Behavior of Hydrocarbon Rocket Fuels [ R ]. AIAA 2003-123.
  • 2Huang H, Sobel D R, Spadacinni L J. Endothermic Heat-Sink of Hydrocarbon Fuels for Scramjet Cooling [ R]. A1AA 2002-3871.
  • 3Robert Mercier, Charles McClinton. Hypersonic Propul- sion Transforming the Furture of Flight [ R ]. AIAA 2003- 2732.
  • 4VioliA, Yan S, Eddings E G, et al. Experimental For- mulation and Kinetic Model for JP28 Surrogate Mixtures [J]. Combustion Science and Technology, 2002, 174: 399-417.
  • 5Zhaohui Liu, Qincheng Bi, Yong Guo, et al. Convective Heat Transfer and Pressure Drop Characteristics of Near- Critical-Pressure Hydrocarbon Fuel in A Minichannel. [J]. Applied Thermal Engineering,2013, 51 : 1047-1054.
  • 6Linne D L, Meyer M L, Edwards T,et al. Evaluation of Heat Transfer and Thermal Stability of Supercritical JP-7 Fuel[ R]. AIAA 97-3041.
  • 7Diane L Linne, Michael L Meyer. Investigation of Insta- bilities and Heat Transfer Phenomena in Supercritical Fu- els at High Heat Flux and Temperatures[ R]. AIAA 2000- 3128.
  • 8Brad Hitch. Enhancement of Heat Transfer and Elimina- tion of Flow Oscillations in Supercritical Fuels[ R]. A1AA 98 -3759.
  • 9Ledinegg M. Instability of Flow During Natural and Forced Circulation[J]. Die Waerme, 1938,61 (8):891- 898.
  • 10Boure J A,Bergles A E, Tong L S. Review of Two-Phase Flow Instability[ J]. Nuclear Energy Design, 1973 , 25: 165-192.

同被引文献51

引证文献3

二级引证文献33

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部