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N_2O/C_3H_8点火器初步实验
引用本文:王栋,郭红杰,梁国柱,刘尹.N_2O/C_3H_8点火器初步实验[J].北京航空航天大学学报,2010,36(10):1162-1165.
作者姓名:王栋  郭红杰  梁国柱  刘尹
作者单位:北京航空航天大学,宇航学院,北京,100191;北京航空航天大学,宇航学院,北京,100191;北京航空航天大学,宇航学院,北京,100191;北京航空航天大学,宇航学院,北京,100191
摘    要:为了研究氧化亚氮与丙烷的点火特性,首次提出了N2O/C3H8火炬式点火方案,设计、加工了点火器,并组建了点火实验系统,在不同的流量和余氧系数下进行了点火实验.结果表明:点火方案可行,喷嘴设计合理,雾化效果和余氧系数是决定点火器能否点燃的关键,余氧系数在0.222~0.321内点火器能可靠地被重复点燃并形成稳定的点火火炬.实验为N2O/C3H8点火器的进一步研究提供了参考,并为以后实现该点火器对发动机的成功点火奠定了基础.

关 键 词:氧化亚氮  丙烷  旋流  点火系统
收稿时间:2009-08-20

Preliminary experimental investigation on nitrous oxide/propane igniter
Wang Dong,Guo Hongjie,Liang Guozhu,Liu Yin.Preliminary experimental investigation on nitrous oxide/propane igniter[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(10):1162-1165.
Authors:Wang Dong  Guo Hongjie  Liang Guozhu  Liu Yin
Institution:School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:To investigate the ignition characteristics of nitrous oxide/propane, the torch igniter scheme of N2O/C3H8 was proposed initially. An igniter was designed and manufactured, and the experimental system was designed. The hot-tests under different condition of mass flow and excess-oxidizer coefficient show that the scheme is feasible, injector structure is reasonable, the spray quality and the excess-oxidizer coefficient are the key for successful ignition, and the igniter is able to generate multiple ignition and produce ignition torch successfully within the excess-oxidizer coefficient range 0.222~0.321. The experiment offers reference for the further study and establishes the foundation for achieving N2O/C3H8 motor ignition directly by this igniter.
Keywords:Nitrogen oxides  propane  swirling flow  ignition system
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