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�������պ����ѧѧ�� 2010, Vol. 36 Issue (10) :1162-1165    DOI:
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Preliminary experimental investigation on nitrous oxide/propane igniter
Wang Dong, Guo Hongjie, Liang Guozhu, Liu Yin*
School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

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ժҪ Ϊ���о������ǵ������ĵ������,�״������N2O/C3H8���ʽ��𷽰�,��ơ��ӹ��˵����,���齨�˵��ʵ��ϵͳ,�ڲ�ͬ������������ϵ���½����˵��ʵ��.�������:��𷽰�����,������ƺ���,��Ч��������ϵ���Ǿ���������ܷ��ȼ�Ĺؼ�,����ϵ����0.222~0.321�ڵ�����ܿɿ��ر��ظ���ȼ���γ��ȶ��ĵ����.ʵ��ΪN2O/C3H8������Ľ�һ���о��ṩ�˲ο�,��Ϊ�Ժ�ʵ�ָõ�����Է������ijɹ����춨�˻���.
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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     
Received 2009-08-20; published 2010-11-12
About author: �� ��(1983-),��,����������,��ʿ��,wdjxsscx@163.com.
����, �����, ������, ����.N2O/C3H8���������ʵ��[J]  �������պ����ѧѧ��, 2010,V36(10): 1162-1165
Wang Dong, Guo Hongjie, Liang Guozhu, Liu Yin .Preliminary experimental investigation on nitrous oxide/propane igniter[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2010,V36(10): 1162-1165
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