脉冲爆震发动机气动阀性能分析

范育新; 王家骅; 李建中; 张义宁

脉冲爆震发动机气动阀性能分析

南京航空航天大学能源与动力学院, 江苏南京 210016

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出版历程
- 收稿日期: 2005-11-09
- 修回日期: 2006-03-01
- 刊出日期: 2007-01-28

Performance analysis of aero-valve in pulse detonation engine

College of Engergy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

摘要

摘要: 通过数值模拟和试验对两种不同结构的脉冲爆震发动机(PDE)气动阀进行了研究.结果表明, 两种气动阀都能在PDE工作中起到单向阀功能, 双旋流气动阀由于切向旋流作用, 其雾化、掺混作用优于锥形气动阀, 而锥形气动阀阻力损失小.同时, 还数值模拟了锥形气动阀关闭后的流场结构, 得到了进气过程中及气动阀关闭后PDE内的流场分布, 结果显示, 气动阀关闭后, 大涡很快脱落形成一系列小涡, 大大增强了流场内的紊流度.
- 航空、航天推进系统 /
- 脉冲爆震发动机(PDE) /
- 气动阀 /
- 流场 /
- 油雾场 /
- 性能分析
Abstract: Two types of aero-valve including bi-swirl and blunt type were designed incorporated with air-blast atomization mechanism.Results of experiments and numerical simulation show that integrate design of aero-valve with air-blast atomizer can improve the distribution of the fuel spray field effectively,and reduce the distance of engendering detonable mixture.Although bi-swirl aero-valve is superior to blunt aero-valve due to its fine atomization and mixing,thrust loss is higher.Numeric simulations results of the process with inlet closed show that large eddies fall off and break into small eddies which increase turbulence intensity greatly.
- aerospace propulsion system /
- pulse detonation engine(PDE) /
- aero-valve /
- flow field /
- fuel concentration field /
- performance analysis

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参考文献(10)

[1]	Fon J V.Elements of flight propulsion[M].New York,1960,261-273.
[2]	Kentifield J A C.The noise-producing characteristics of highly loaded valvelessl pulse combustor[R],ASME 86-WA Dec.80.
[3]	Bertin J H.Aerodynamic valve[Z].U.S.Patent No.2 670 011 54.
[4]	Wislicenus G F.Flow control means for pulsejet combustion units[Z].U.S.Patent No.2,618 925 52.
[5]	Brophy C M,Netzer D W.Effect of ignition characteristics and geometry on the performance of a JP-10/O2fueled pulse detonation engines[R].AIAA 99-2635,July 1999.
[6]	Smirnov N N,Nikitin V F,et al.Control of detonation onset in combustible gases[A].High-speed deflagration and detonation:Fundamentals and control[C].edited by Roys G D,Frolov M,et al.ELEX-KM Publishers,Moscow,2001,3-30.
[7]	Achasov O V,Penyazkov O G.Some gasdynamic methods for control of detonation initiation and propagation[A].High-speed deflagration and detonation:Fundamentals and control[C].edited by Roys G D,Frolov S M,et al.ELEX-KM Publishers,Moscow,2001,31-44.
[8]	郑殿峰,王家骅,王波,等.脉冲爆震发动机旋流式气动阀工作机理和扰流器阻力特性的实验研究[J].南京航空航天大学学报,2005,36(1):101-105.ZHEN Dianfeng,WANG Jiahua,WANG bo,et al.Experimental investigation on mechanism of swirling aerovalve and drag coefficient of turbulence generation in PDE[J].Journal of Nanjing University of Aeronautics & Astronautics,2005,36(1)1:101-105.
[9]	Smagorinsky J.General circulation experiments with primitive equations[R].Mon.Weather Rev,1963,91(3):99-164.
[10]	范育新,王家骅,李建中,等.脉冲爆震发动机(PDE)引射增推装置研究[J].航空动力学报,2005,20(6):983-988.FAN Yuxin,WANG Jiahua,LI Jianzhong,Experimental investigationgs on thrust augmentation of pulsed detonation engine (PDE)[J].Journal of Aerospace Power,2005,20(6):983-988.