IGNITER

作品数：13被引量：23H指数：3
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相关领域：理学更多>>
相关作者：李秀娟王磊更多>>
相关机构：南京理工大学乌鲁木齐职业大学更多>>
相关期刊：《Propulsion and Power Research》《Semiconductor Photonics and Technology》《Chinese Physics B》《Defence Technology（防务技术）》更多>>
相关基金：国家自然科学基金更多>>
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Characteristics of a pre-combustion plasma jet igniter
《Chinese Journal of Aeronautics》2024年第7期178-189,共12页Jinlu YU Baowen ZHANG Yang YU Bingbing ZHAO Lei ZHANG 
co-supported by the National Natural Science Foundation of China(No.52306123);the Postdoctoral Science Foundation,China(No.2023M734277);the Natural Science Basic Research Program of Shaanxi,China(No.2021JQ-046)。
Plasma ignition technology has delivered good performance in the aerospace industry. In this study, a pre-combustion plasma jet igniter was designed, and its characteristics were examined from three aspects: the morph...
关键词：Pre-combustion plasma igniter PLASMA Jet temperature field Ignition process ARC FLAME 
Predicting the electromechanical properties of small caliber projectile impact igniter using PZT dynamic damage constitutive model considering crack propagation被引量：1
《Defence Technology（防务技术）》2023年第10期121-135,共15页Rui-zhi Wang Zhi-qiang Wang En-ling Tang Lei Li Guo-lai Yang Chun Cheng Li-ping He Ya-fei Han 
supported by the National Natural Science Foundation of China(Grant No.12172232);the project of Key Laboratory of Impact and Safety Engineering(Ningbo University,China);Ministry of Education(CJ202206);supported by the scientific research support plan of introducing high-level talents from Shenyang Ligong University。
Block piezoelectric ceramics(PZTs)are often used in impact igniters to provide activation energy for electric initiators.Under the action of strong impact stress,PZTs release electric energy accompanied by crack initi...
关键词：Piezoelectric ceramics IMPACT IGNITER Dynamic damage constitutive model Electromechanical response 
Discharge and jet characteristics of gliding arc plasma igniter driven by pressure difference
《Plasma Science and Technology》2022年第11期93-105,共13页Xinyao CHENG Huimin SONG Shengfang HUANG Yifei ZHU Zhibo ZHANG Zhenyang LI Min JIA 
supported by National Science and Technology Major Project (No. 2017-Ⅲ-0007-0033)
Stable combustion in an afterburner can help increase the thrust of the engine in a short time,thereby improving the maneuverability of a fighter.To improve the ignition performance of an afterburner,a twin-duct ignit...
关键词：PLASMA IGNITION gliding arc 
Experimental investigation of a gliding discharge plasma jet igniter被引量：3
《Chinese Journal of Aeronautics》2022年第6期116-124,共9页Min JIA Zhibo ZHANG Wei CUI Huimin SONG Zhangkai HUANG 
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)
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 combu...
关键词：Gliding Arc Plasma Jet Igniter(GAPJI) Arc evolution Flame kernel Ignition process Gliding arc Lean ignition limit 
Experimental study on energy characteristics and ignition performance of recessed multichannel plasma igniter被引量：3
《Chinese Physics B》2020年第6期339-348,共10页Bang-Huang Cai Hui-Min Song Min Jia Yun Wu Wei Cui Sheng-Fang Huang 
National Natural Science Foundation of China(Grant No.91641204).
In the extreme conditions of high altitude,low temperature,low pressure,and high speed,the aircraft engine is prone to flameout and difficult to start secondary ignition,which makes reliable ignition of combustion cha...
关键词：high altitude extreme condition recessed multichannel plasma igniter discharge energy lean ignition boundary 
基于PHP+CSS框架的学生公共信息服务平台的设计与实现被引量：5
《智库时代》2020年第8期218-219,共2页李秀娟 王磊 
乌鲁木齐职业大学重点课题-乌鲁木齐职业大学多语言学生公共信息服务平台的设计与实现(2015XZ003)。
本论文针对校园公共信息服务平台的关键技术进行研究,采用MVC开发框架,结合Code Igniter与Bootstrap的开发模式,完成系统前端、后台以及接口的开发,使用MySQL作为系统的数据库,使用集成服务器软件Apache搭建本地服务器,设计并实现了公...
关键词：CODE IGNITER BOOTSTRAP PHP 公共信息服务平台 
Ignition characteristics of pre-combustion plasma jet igniter被引量：3
《Chinese Physics B》2019年第11期227-237,共11页Si-Bo Wang Jin-Lu Yu Jing-Feng Y Guo-Hua Li Zhao Chen Lu-Yun Jiang Chen-Li Gu 
Project supported by the National Natural Science Foundation of China(Grant Nos.51776223 and 91741112)
At present, aero-engines face a major need to widen the ignition envelope. In order to provide a technical support to expand the high altitude ignition envelope of aero-engines, in this article we propose a novel igni...
关键词：pre-combustion DISCHARGE stability IGNITION DELAY time IGNITION BOUNDARY 
Experimental studies of explosion energy output with different igniter mass被引量：2
《Defence Technology（防务技术）》2019年第5期808-814,共7页Heyang Xu Weibing Li Wenbin Li Yajun Wang 
funded by the National Natural Science Foundation of China No.11202103;Postgraduate Research&Practice Innovation Program of Jiangsu Province No.KYCX18_0472
For study the energy output law of cylindrical charge with shell induced by different input energies,four different black powder masses were selected to ignite the main charge.Fragmentation degree of the shell was qua...
关键词：analysis  ENERGY MASS 
Experimental investigation on electrical characteristics and ignition performance of multichannel plasma igniter被引量：1
《Chinese Physics B》2018年第3期327-334,共8页Sheng-Fang Huang Hui-Min Song Yun Wu Min Jia Di Jin Zhi-Bo Zhang Bing-Xuan Lin 
Project supported by the National Natural Science Foundation of China(Grant Nos.91541120,11472306,51336011,and 91641204)
Relighting of jet engines at high altitudes is very difficult because of the high velocity, low pressure, and low tempera- ture of the inlet airflow. Successful ignition needs sufficient ignition energy to generate a ...
关键词：multichannel plasma igniter high-speed inlet airflow ignition energy ignition performance 
A Steam-Plasma Igniter for Aluminum Powder Combustion被引量：2
《Plasma Science and Technology》2015年第5期392-401,共10页Sanghyup LEE Kwanyoung NOH Jihwan LIM Woongsup YOON 
supported by the Defense Acquisition Program Administration and Agency for Defense Development under the contract UD110095CD;supported by the Advanced Research Center Program(NRF-2013R1A5A1073861) through the National Research Foundation of Korea(NRF) grant funded by the Korean government(MSIP) contracted through the Advanced Space Propulsion Research Center at Seoul National University
High-temperature ignition is essential for the ignition and combustion of energetic metal fuels, including aluminum and magnesium particles which are protected by their high- melting-temperature oxides. A plasma torch...
关键词：steam plasma igniter aluminum emission spectroscopy energetic metal fuels powder ignition and combustion optical 
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