Experimental Investigation on Detonation Devices Induce Detonation in Two-Phases Mixed Gas

Journal of Propulsion Technology ›› 2013, Vol. 34 ›› Issue (7): 997-1001.

• New Propulsion System • Previous Articles Next Articles

Experimental Investigation on Detonation Devices Induce Detonation in Two-Phases Mixed Gas

College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016;Science and Technology on Scramjet Laboratory,The 31st Research Institute of CASIC, Beijing 100074;Science and Technology on Scramjet Laboratory,The 31st Research Institute of CASIC, Beijing 100074

Published:2021-08-15

助爆装置影响两相混气中爆震波触发特性实验

孙健¹,韩启祥¹,王家骅¹,张义宁²,孙孔倩²

南京航空航天大学能源与动力学院,江苏南京 210016;南京航空航天大学能源与动力学院,江苏南京 210016;南京航空航天大学能源与动力学院,江苏南京 210016;中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室,北京 100074;中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室,北京 100074

作者简介:孙健(1987—),男,硕士生,研究领域为脉冲爆震发动机。 E-mail:1987sunjian@sina.com
基金资助:
高超声速冲压发动机重点实验室开放基金(20110101009)。

Abstract

Abstract: The investigation of detonation devices induce detonation was performed in order to optimize the detonation devices in two-phases mixed gas. This paper thesis analyzed the velocity of flame transmission and the changeable process of pressure in the detonation tube which were affected by various detonation devices, such as circular obstacle, spiral obstacle, serrated obstacle, vaporized-detonator and reflector, and the performance of the detonation devices was obtained. The investigation shows that ,firstly, the spiral obstacle has the best performance while the circular obstacle performance is the worst. Secondly, the improvement of fuel evaporation is helpful for inducing detonation no matter what obstacle is used. Thirdly, reflector can improve the velocity of flame transmission and the pressure of detonation wave in a way. 

Key words: Detonation devices; Obstacle; Vaporized-detonator; Reflector; Velocity of flame

摘要： 为了优化汽油/空气两相PDE中的助爆装置,通过试验研究了助爆装置对爆震波触发特性的影响,重点分析了在锯齿型扰流器、环型扰流器、螺旋型扰流器、多管蒸发器和半球型激波反射器等助爆装置作用下爆震管内的火焰传播速度及压力变化历程,确定了助爆装置的助爆性能。研究结果表明:锯齿型、环型及螺旋型三种扰流器中螺旋型扰流器的助爆性能最佳,环型扰流器最差；无论哪种扰流器下,改善燃油蒸发均有助于爆震波触发；使用激波反射器对提高火焰传播速度和爆震波压力具有一定作用。 

关键词: 助爆装置;扰流器;蒸发器;激波反射器;火焰传播速度 

SUN Jian¹, HAN Qi-xiang¹, WANG Jia-hua¹, ZHANG Yi-ning², SUN Kong-qian². Experimental Investigation on Detonation Devices Induce Detonation in Two-Phases Mixed Gas[J]. Journal of Propulsion Technology, 2013, 34(7): 997-1001.

孙健,韩启祥,王家骅,张义宁,孙孔倩. 助爆装置影响两相混气中爆震波触发特性实验[J]. 推进技术, 2013, 34(7): 997-1001.

References

[1] 严传俊,范玮,黄希桥,等.脉冲爆震发动机原理及关键技术[M].西安:西北工业大学出版社,2005.
[2] Roy G D, Frolov S M, Borisov A A,et al.Pulse Detonation Propulsion:Challenges,Current Status,and Future Perspective[R].Progress in Energy and Combustion Science,2004,(30):54626721.
[3] Kasahara J,Takazawa K,Arai T.Experimental Study of Impulse and Heat Transfer on Pulse Detonation Engines[R].AIAA 2002-4071.
[4] Lee S Y,Conrad C, Watts J,et al.Deflagration to Detonation Transition Study Using Simultaneous Schlieren and OH PLIF Images[R].AIAA 2000-3217.
[5] Meyer T R,Hoke J L,Brown M S.Experimental Study of Deflagration-To-Detonation Enhancement Techniques in a H₂/Air Pulse Detoantion Engine[R].AIAA 2002-3720.
[6] 何小民,张彭岗,王家骅.爆震管内爆燃到爆震转捩过程的实验研究[J].推进技术,2005,26(3):252-255.(HE Xiao-min,ZHANG Peng-gang,WANG Jia-hua.Experimental Investigation of Deflagration to Detonation Transition in Two -Phase Mixture Combustion[J].Journal of Propulsion Technology,2005,6(3):252-255.)
[7] 韩启祥.预混气爆震管中爆燃到爆震转捩距离的研究[J].推进技术,2003,24(1):63-66.(HAN Qi-xiang.Investigation of Deflagration to Detonation Transition Distance in a Tube with Mixture[J].Journal of Propulsion Technology,2003,24(1):63-66.)
[8] 张义宁,王家骅.汽油/空气两相脉冲爆震发动机触发爆震的研究[J].航空动力学报,2006,8(4).
[9] 刘鸿.六管气动阀式两相脉冲爆震发动机试验研究[D].南京:南京航空航天大学,2010.
[10] 范育新,王家骅.脉冲爆震发动机的蒸发助爆器试验[J].航空动力学报,2006,4(2):308-315.
[11] 李建中.煤油/空气脉冲爆震发动机激波反射起爆研究[J].工程热物理学报,2007,8(2):347-350.
[12] 李建中.煤油/空气脉冲爆震发动机强化燃烧装置[J].航空动力学报,2007,2(4):547-553.
[13] 李建中.煤油/空气气动阀式脉冲爆震发动机研究[D].南京:南京航空航天大学, 2006.
[14] 韩启祥,王家骅.测量爆燃到爆震转捩距离的离子探针技术研究[J].航空动力学报,2003,8(1):97-100.
[15] 郑殿峰.扰流片对汽油/空气脉冲爆震发动机爆震波压力的影响[J].推进技术,2004,25(6):549-552.(ZHENG Dian-feng.Effects of Parameters of Turbulence Generator on the Detonation Wave in Air-Breathing Gasoline-Air Pulse Detonation Engine[J].Journal of Propulsion Technology,2004,5(6):549-552.)

Experimental Investigation on Detonation Devices Induce Detonation in Two-Phases Mixed Gas

助爆装置影响两相混气中爆震波触发特性实验

PDF

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 0

Recommended Articles

Metrics

Comments