|本期目录/Table of Contents|

[1]王伟,广才,尹莉萍.燃油流量对防火试验火焰特征的影响[J].中国安全生产科学技术,2017,13(11):41-47.[doi:10.11731/j.issn.1673-193x.2017.11.007]
 WANG Wei,GUANG Cai,YIN Liping.Influence of fuel flow rate on flame characteristics in fire test[J].JOURNAL OF SAFETY SCIENCE AND TECHNOLOGY,2017,13(11):41-47.[doi:10.11731/j.issn.1673-193x.2017.11.007]
点击复制

燃油流量对防火试验火焰特征的影响
分享到:

《中国安全生产科学技术》[ISSN:1673-193X/CN:11-5335/TB]

卷:
13
期数:
2017年11期
页码:
41-47
栏目:
学术论著
出版日期:
2017-11-30

文章信息/Info

Title:
Influence of fuel flow rate on flame characteristics in fire test
文章编号:
1673-193X(2017)-11-0041-07
作者:
王伟广才尹莉萍
(中国民航大学 天津市民用航空器适航与维修重点实验室,天津 300300)
Author(s):
WANG Wei GUANG Cai YIN Liping
(Tianjin Key Laboratory of Civil Aircraft Airworthiness and Maintenance, Civil Aviation University of China, Tianjin 300300, China)
关键词:
防火试验NexGen燃烧器燃油流量火焰形状温度热流密度
Keywords:
fire test NexGen burner fuel flow rate flame shape temperature heat flux
分类号:
V235
DOI:
10.11731/j.issn.1673-193x.2017.11.007
文献标志码:
A
摘要:
为了研究燃油流量对防火试验火焰特征的影响,为防火试验方案的设计提供参考和指导,采用Ansys Fluent软件对NexGen燃烧器进行三维定常数值模拟,分析了不同燃油流量条件下的火焰特征。结果表明:燃油流量对火焰最高温度和火焰形状几乎没有影响,但对火焰长度、监测面上温度分布、7个测量点的平均温度和热流密度有很大影响,通过分析各燃油流量条件下的火焰特征,发现当空气流量为35.8 g/s时,燃油流量在2.0~2.11 g/s——即余气系数为1.15~1.22时,能够用于防火试验。
Abstract:
In order to study the influence of fuel flow rate on the flame characteristics in fire test, so as to provide the reference and guidance for the design of fire test scheme, the three-dimensional steady numerical simulation on the NexGen burner was carried out by using the Ansys Fluent software, and the flame characteristics under different conditions of fuel flow rate were analyzed. The results showed that the fuel flow rate had almost no effect on the maximum temperature and shape of flame, but had great effect on the flame length, the temperature distribution on the monitoring surface, and the average temperature and heat flux of seven measuring points. Through analyzing the flame characteristics under different fuel flow rates, it showed that the air flow rate of 35.8 g/s combining with the fuel flow rate of 2.0 to 2.11 g/s, namely the excess air coefficient of 1.15 to 1.22, can be used for the fire tests.

参考文献/References:

[1]孙瑞山,刘露. 中美两国民航事故发展趋势对比分析[J]. 中国安全生产科学技术,2012,8(9):154-158. SUN Ruishan, LIU Lu.Comparative analysis on accident trend of civil aviation between China and America[J].Journal of Safety science and Technology,2012,8(9):154-158.
[2]中国民用航空局. 中国民用航空规章第33部航空发动机适航规定:CCAR-33-R2[S].北京:中国民航出版社,2011.
[3]De Florio F.Airworthiness: An introduction to aircraft certification and operations[M].London,Butterworth-Heinemann,2016.
[4]US Department of Transportation,Federal Aviation Administration. Advisory circular 20-135: Powerplant Installation and Propulsion System Component FireProtection Test Methods [R].Washington DC:FAA, 1990.
[5]FAA Fire Safety Branch. Next Generation (NexGen) Fire Test Burner[EB/OL].(2016-04).[2017-8-23]. http://www.fire.tc.faa.gov/pdf/materials/NexGenPlans_4_2016.pdf
[6]US Department of Transportation,Federal Aviation Administration.Power Plant Engineering Report No.3A: Standard Fire Test Apparatus and Procedure (For Flexible Fose Assemblies ) [R].Washington D.C:FAA,1978.
[7]严传俊. 燃烧学[M]. 西安:西北工业大学出版社, 2008.
[8]Robert Ochs, Development of a Next-Generation Burner for Use in Testing Thermal Acoustic Insulation Burnthrough Resistance[R]. London, UK: Proceeding of IASFPWG,May , 2009.
[9]Yi-Huan Kao. Experimental Investigation of NexGen and Gas Burner for FAA Fire Test[D] .Cincinnati:University of Cincinnati , 2012.
[10]Ochs R. Development of the next generation fire test burner for powerplant fire testing applications[R]. Proceeding of IASFPWG, London, UK, May 18, 2010.
[11]Kreuder J, Kirkpatrick A T, Gao X. Computation of Heat Transfer from an Impinging Flame Jet to a Plane Surface[A].51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition[C].Texas,2013.
[12]Ochs R I. Design and Analysis of the Federal Aviation Administration Next Generation Fire Test Burner[M]. New Jersey: Rutgers University, 2013.
[13]杨世铭,陶文栓. 传热学[M]. 北京:高等教育出版社,2006.
[14]The International Organization for Standardization (ISO). Aircraft Environmental Conditions and Test Procedures for Airbone Equipment - Resistance to Fire in Designated Fire Zones: ISO2685:1998(E)[S]. Switzerland:ISO,1998.
[15]Bai Jie, Liu Shuai, WangWei. Effects of Initial Temperature on the Formation Mechanisms of Nitrogen Dioxide[A]. 10th Asia-Pacific Conference on Combustion[C], Beijing, China, July 19-22, 2015.

相似文献/References:

备注/Memo

备注/Memo:
中央高校基本科研业务费专项基金(ZXH2012J003);中国民航大学科研启动基金项目(2014QD06X)
更新日期/Last Update: 2017-12-27