RP-3航空煤油/O_(2)的氧化与着火特性试验  

Experiment on the oxidation and ignition delay characteristics of RP-3 kerosene/oxygen

作　　者：张鑫炜 曾文 胡斌[2] 殷阁媛 张英佳[3] 马宏宇 ZHANG Xinwei;ZENG Wen;HU Bin;YIN Geyuan;ZHANG Yingjia;MA Hongyu(School of Aero-engine,Shenyang Aerospace University,Shenyang 110136,China;Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China;State Key Laboratory of Multiphase Flow in Power Engineering,School of Energy and Power Engineering,Xi’an Jiaotong University,Xi’an 710049,China;Shenyang Engine Research Institute,Aero Engine Corporation of China,Shenyang 110015,China)

机构地区：[1]沈阳航空航天大学航空发动机学院,沈阳110136 [2]中国科学院工程热物理研究所,北京100190 [3]西安交通大学能源与动力工程学院动力工程多相流国家重点实验室,西安710049 [4]中国航发沈阳发动机研究所,沈阳110015

出　　处：《航空动力学报》2024年第5期129-137,共9页Journal of Aerospace Power

基　　金：国家科技重大专项(2017-Ⅲ-0006-0031)。

摘　　要：在流动管反应器中对当量比分别为0.5、1.0、2.0、温度范围为550~1200 K、压力分别为0.1、3.0MPa条件下RP-3航空煤油/O_(2)的氧化特性进行了试验测试。结果表明:当量比由0.5增加到2.0时,RP-3航空煤油/O_(2)氧化过程中各组分生成的起始温度以及出现摩尔分数峰值时的温度均升高;压力由0.1 MPa升高到3.0 MPa时,RP-3航空煤油/O_(2)氧化过程中各组分生成的起始温度以及出现摩尔分数峰值时的温度均降低,烷烃的摩尔分数峰值升高,而烯烃的摩尔分数峰值则降低。同时,在激波管中对当量比分别为0.8、3.5、压力分别为0.2、1.0、5.0 MPa、温度范围为950~1500 K条件下RP-3航空煤油/O_(2)的着火延迟特性进行了试验测试。结果表明,RP-3航空煤油/O_(2)的着火延迟时间随压力与温度的升高、当量比由3.5减小到0.8时逐渐缩短。The oxidation characteristics of RP-3 kerosene/O2 were experimentally tested in the flow reactor under the conditions of the equivalence ratios of 0.5,1.0 and 2.0,the temperature range of 550−1200 K,the pressure of 0.1,3.0 MPa.The results showed that,with the increase of equivalent ratio from 0.5 to 2.0,the starting temperature of each species formation and the corresponding temperature of the peak mole fraction of each species increased.With the increase of pressure from 0.1 MPa to 3.0 MPa,the starting temperature of each species formation and the corresponding temperature of the peak mole fraction of each species decreased,and the peak mole fraction of alkanes increased while that of alkenes decreased.Meanwhile,the ignition delay characteristics of RP-3 kerosene/O2 were experimentally tested in the shock tube under the conditions of the equivalent ratios of 0.8,and 3.5,the pressure of 0.2,1.0,and 5.0 MPa,the temperature range of 950−1500 K.The results showed that,with the increase of the pressure and temperature or the decrease of equivalent ratio from 3.5 to 0.8,the ignition delay time of RP-3 kerosene/O2 was shortened.

关 键 词：RP-3航空煤油 氧化特性 流动管反应器 激波管 着火延迟时间 

分 类 号：V231.2[航空宇航科学与技术—航空宇航推进理论与工程] TK401[动力工程及工程热物理—动力机械及工程]