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Technical gazette, Vol. 25 No. 6, 2018

Original scientific paper
https://doi.org/10.17559/TV-20180807223114

Research on Combustion Chamber Structure Improvement and Ignition System of Missile Turbojet Engine for Diesel Fuel

Lei Qiu ; Key Laboratory of E&M, Ministry of Education & Zhejiang Province, Hangzhou, China / Zhejiang University of Technology, Hangzhou, China
Xi Zeng ; Key Laboratory of E&M, Ministry of Education & Zhejiang Province, Hangzhou, China / Zhejiang University of Technology, Hangzhou, China
Shiming Ji ; Key Laboratory of E&M, Ministry of Education & Zhejiang Province, Hangzhou, China
Fengfei Xi ; Key Laboratory of E&M, Ministry of Education & Zhejiang Province, Hangzhou, China
Wenbin Qiu ; Key Laboratory of E&M, Ministry of Education & Zhejiang Province, Hangzhou, China
Qianqian Zheng ; Key Laboratory of E&M, Ministry of Education & Zhejiang Province, Hangzhou, China

Fulltext: english, pdf (3 MB) pages 1792-1800 downloads: 33* cite
APA 6th Edition
Qiu, L., Zeng, X., Ji, S., Xi, F., Qiu, W. & Zheng, Q. (2018). Research on Combustion Chamber Structure Improvement and Ignition System of Missile Turbojet Engine for Diesel Fuel. Tehnički vjesnik, 25 (6), 1792-1800. https://doi.org/10.17559/TV-20180807223114
MLA 8th Edition
Qiu, Lei, et al. "Research on Combustion Chamber Structure Improvement and Ignition System of Missile Turbojet Engine for Diesel Fuel." Tehnički vjesnik, vol. 25, no. 6, 2018, pp. 1792-1800. https://doi.org/10.17559/TV-20180807223114. Accessed 23 Feb. 2019.
Chicago 17th Edition
Qiu, Lei, Xi Zeng, Shiming Ji, Fengfei Xi, Wenbin Qiu and Qianqian Zheng. "Research on Combustion Chamber Structure Improvement and Ignition System of Missile Turbojet Engine for Diesel Fuel." Tehnički vjesnik 25, no. 6 (2018): 1792-1800. https://doi.org/10.17559/TV-20180807223114
Harvard
Qiu, L., et al. (2018). 'Research on Combustion Chamber Structure Improvement and Ignition System of Missile Turbojet Engine for Diesel Fuel', Tehnički vjesnik, 25(6), pp. 1792-1800. doi: https://doi.org/10.17559/TV-20180807223114
Vancouver
Qiu L, Zeng X, Ji S, Xi F, Qiu W, Zheng Q. Research on Combustion Chamber Structure Improvement and Ignition System of Missile Turbojet Engine for Diesel Fuel. Tehnički vjesnik [Internet]. 2018 [cited 2019 February 23];25(6):1792-1800. doi: https://doi.org/10.17559/TV-20180807223114
IEEE
L. Qiu, X. Zeng, S. Ji, F. Xi, W. Qiu and Q. Zheng, "Research on Combustion Chamber Structure Improvement and Ignition System of Missile Turbojet Engine for Diesel Fuel", Tehnički vjesnik, vol.25, no. 6, pp. 1792-1800, 2018. [Online]. doi: https://doi.org/10.17559/TV-20180807223114

Abstracts
To meet the conditions of diesel ignition, this paper presents several structural improvements of a small missile turbojet engine for diesel fuel. The engine starts motor-assisted, and its fuel is ignited by silicon nitride ceramic ignitor. Theoretical analysis is performed by establishing a mathematical model of the combustion model and combustion conditions. The feasibility of diesel used as a small turbojet fuel is analyzed by using numerical simulation software. Research is carried out based on the following points: the improvement of combustion chamber and evaporator, selection of ignitor position and sustainability of fire. This paper proposed the method of linking the engine-assisting startup system and selected the right type of ignitor, and on the advanced experimental platform several groups ignition tests were carried out.

Keywords
combustion chamber; diesel; ignition system; missile; turbojet

Hrčak ID: 212836

URI
https://hrcak.srce.hr/212836

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