Experimental investigation of a gliding discharge plasma jet igniter  

作　　者：Min JIA Zhibo ZHANG Wei CUI Huimin SONG Zhangkai HUANG 

机构地区：[1]Science and Technology on Plasma Dynamics Laboratory,Air Force Engineering University,Xi’an 710038,China [2]Key Laboratory of Physical Electronics and Devices of Ministry of Education,Xi’an Jiaotong University,Xi’an 710038,China

出　　处：《Chinese Journal of Aeronautics》2022年第6期116-124,共9页中国航空学报（英文版）

基　　金：co-supported by the National Natural Science Foundation of China (Nos. 51807204 and 91941301);the Postdoctoral Research Foundation of China (No. 2019M663719);the National Science and Technology Major Project, China (No. 2017-Ⅲ-0007-0033)

摘　　要：Relight of jet engines at high altitude is difficult due to the relatively low pressure and temperature of inlet air.The penetration of initial flame kernel affects the ignition probability in the turbine engine combustor greatly.In order to achieve successful ignition at high altitude,a deeper penetration of initial flame kernel should be generated.In this study,a Gliding Arc Plasma Jet Igniter(GAPJI)is designed to induce initial flame kernel with deeper penetration to achieve successful ignition at high altitude.The ignition performance of the GAPJI was demonstrated in a model combustor.It was found that GAPJI can generate plasma with deeper penetration up to 30.5 mm than spark igniter with 22.1 mm.The discharge power of GAPJI was positively correlated with flow rate of the carrier gas,approaching 200 W in average.Ignition experiments show that GAPJI has the advantage of extending the lean ignition limit.With GAPJI,the lean ignition limit of the combustor is 0.02 at 0 km,which is 55.6%less than that with spark igniter(0.045).The evolution of flame morphology was observed to explore the development of the flame kernel.It is shown that the advantage of a high penetration and continuous releasing energy can accelerate the ignition process and enhance combustion.

关 键 词：Gliding Arc Plasma Jet Igniter(GAPJI) Arc evolution Flame kernel Ignition process Gliding arc Lean ignition limit 

分 类 号：TK473[动力工程及工程热物理—动力机械及工程]