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多循环脉冲爆震发动机工作过程中的延迟时间研究
引用本文:张义宁,王家骅,刘鸿,张靖周.多循环脉冲爆震发动机工作过程中的延迟时间研究[J].航空动力学报,2007,22(2):228-232.
作者姓名:张义宁  王家骅  刘鸿  张靖周
作者单位:1.南京航空航天大学 能源与动力学院 南京 210016
摘    要:为了提高两相脉冲爆震发动机(PDE)工作的协调性, 运用离子传感器、动态压力传感器, 对爆震燃烧的几个延迟时间以及供油电磁阀工作性能进行研究.研究表明:以汽油为燃料、空气为氧化剂的气动阀式PDE, 点火延迟时间为3.0-4.5 ms, 气动阀关闭滞后点火信号发出4.9-6.4 ms, 供油电磁阀开、关延迟分别为2.4ms和3.4 ms左右.缓燃向爆震转捩时间为3.0-3.8 ms.PDE工作频率大于20 Hz时, 电磁阀不能按设定时间工作.研究成果对PDE工作过程的协调及有效控制具有参考价值. 

关 键 词:航空、航天推进系统    脉冲爆震发动机(PED)    延迟时间    控制    气动阀
文章编号:1000-8055(2007)02-0228-05
收稿时间:1/4/2006 12:00:00 AM
修稿时间:2006年1月4日

Investigation of several delay times in operation process of multi-cycle pulse detonation engine
ZHANG Yi-Ning,WANG Jia-Hu,LIU Hong and ZHANG Jing-zhou.Investigation of several delay times in operation process of multi-cycle pulse detonation engine[J].Journal of Aerospace Power,2007,22(2):228-232.
Authors:ZHANG Yi-Ning  WANG Jia-Hu  LIU Hong and ZHANG Jing-zhou
Institution:1.College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China2.Jiangsu Polytechnic University, Changzhou 213016, China
Abstract:In order to promote the operating coordination of a two-phase pulse detonation engine(PDE),the delay time of detonation and operating performance of the solenoid valve were experimentally studied by using ion-sensors and pressure transducers of high-frequency response.The detonation tube is of 58mm inner diameter and 1 270 mm long.Liquid gasoline/air mixture is filled for the engine multi-cycle operations.According to the research,the mixture ignition delay is 3~4.5 ms,the aero-valve closing delay is 4.9~6.4 ms,and the solenoid electric valve on/off delay time is 2.4 ms and 3.4 ms respectively.The transition time from deflagration-to-detonation is about 3.0~3.8 ms.The solenoid electric valve cannot operate orderly when the engine operating frequency is higher than 20 Hz.These data obtained are helpful to coordinate PDE operation process. 
Keywords:aerospace propulsion system  pulse detonation engine(PDE)  delay time  control  aero-valve
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