检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:胡静[1] 刘勇[1] 杨国凯 李志宝 束伟伟 司晓亮 HU Jing;LIU Yong;YANG Guokai;LI Zhibao;SHU Weiwei;SI Xiaoliang(School of Aeronautical Engineering,Civil Aviation University of China,Tianjin 300300,China;Anhui Province Key Laboratory of Aircraft Lightning Protection,Hefei 230031,China;Aviation Key Laboratory of Science and Technology on High Intensity Electromagnetic Environment Protection,Hefei 230031,China;Hefei Hangtai Electrophysics Technology Co.,Ltd.,Hefei 230031,China)
机构地区:[1]中国民航大学航空工程学院,天津300300 [2]安徽省飞机雷电防护省级重点实验室,安徽合肥230031 [3]强电磁环境防护技术航空科技重点实验室,安徽合肥230031 [4]合肥航太电物理技术有限公司,安徽合肥230031
出 处:《合肥工业大学学报(自然科学版)》2024年第5期620-627,共8页Journal of Hefei University of Technology:Natural Science
基 金:国家科技重大专项资助项目(J2019-Ⅷ-0009-0170)。
摘 要:文章对典型民用飞机油箱通气口飞机火焰抑制器火焰传播特性开展试验研究。根据SAEARP5416中规定的H_(2)、O_(2)、Ar3种混合气体的燃爆方案,借鉴ISO16852标准下的试验方法,自建燃爆试验台,并分别在不同H_(2)体积分数、阻火芯体内部孔径和芯体长度的情况下开展系列试验,并与现行商用阻火器特性进行对比,同时使用高速摄像机获得爆燃阻火现象及规律并开展仿真对比。试验结果表明,使用体积分数为5.0%~10.0%的H_(2)进行飞机火焰抑制器火焰传播试验时,试验阻火成功率极低,并得到H_(2)体积分数升高对火焰传播速度的影响规律。研究表明,H_(2)与航空煤油蒸气的特性差异是阻火失效的关键因素。该文对此次试验的混合气体局限性进行分析,试验结果也为H2类阻火器的研究提供一定的参考。The flame propagation characteristics of flame arrestor for typical civil aircraft fuel tank vent were studied.According to the combustion and explosion scheme of mixture gas of H_(2),O_(2)and Ar stipulated in SAE ARP5416,and referring to the test method under ISO 16852 standard,the combustion and explosion test platform was built,and a series of tests were carried out under the conditions of different H_(2)concentration ratios,internal apertures and lengths of flame suppression core.The characteristics of the flame arrestor were compared with those of current commercial flame arrestor.The phenomenon and law of deflagration flame arrestor were also obtained by using high-speed camera and the simulation was carried out.The results show that the flame propagation test of aircraft flame arrestor using H_(2)with a concentration ratio of 5.0%-10.0%has a very low success rate of flame suppression,and the influence rule of increasing H_(2)concentration on the flame propagation velocity is obtained.The results show that the difference between H_(2)and aviation kerosene vapor is the key factor in the failure of flame suppression.The limitations of mixture gas in this test were explained.The test results can provide reference for the research on H_(2)-type flame arrestor.
关 键 词:飞机火焰抑制器 混合气体 燃爆过程 阻火测试 气体适用性
分 类 号:V264.3[航空宇航科学与技术—航空宇航制造工程]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:3.133.83.123