邓海飞,吕艳梅,王家林,王格芳,陈卫.某型无人机伞降回收系统故障模式、 影响及危害性分析[J].装备环境工程,2012,9(3):90-93,98. DENG Hai-fei,LV Yan-mei,WANG Jia-lin,WANG Ge-fang,CHEN Wei.FMECA for Parachuted Recovery System of a Type UAV[J].Equipment Environmental Engineering,2012,9(3):90-93,98.
某型无人机伞降回收系统故障模式、 影响及危害性分析
FMECA for Parachuted Recovery System of a Type UAV
投稿时间:2011-11-14  修订日期:2012-06-15
DOI:
中文关键词:  无人机  故障模式  影响及危害性分析  严酷度  危害性
英文关键词:UAV  failure mode  effects and criticality analysis  severity  criticality
基金项目:国防科研项目 (2010530)
作者单位
邓海飞 陆军军官学院, 合肥 230031 
吕艳梅 军械技术研究所, 石家庄 050000 
王家林 陆军军官学院, 合肥 230031 
王格芳 军械技术研究所, 石家庄 050000 
陈卫 陆军军官学院, 合肥 230031 
AuthorInstitution
DENG Hai-fei Army officer Academy, Hefei 230031, China 
LV Yan-mei Institute of Ordnance Technology, Shijiazhuang 050000, China 
WANG Jia-lin Army officer Academy, Hefei 230031, China 
WANG Ge-fang Institute of Ordnance Technology, Shijiazhuang 050000, China 
CHEN Wei Army officer Academy, Hefei 230031, China 
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中文摘要:
      为提高某型无人机伞降回收系统的可靠性, 采用硬件法与功能法相结合的方法对该系统进行了故障模式及影响分析, 利用定量分析方法和危害性矩阵图对该系统的危害性进行了分析。研究结果表明,需要对 “主伞故障” 这一失效模式加以重点关注。给出了使用中应采取的预防措施, 使系统的可靠性得到了显著增长。
英文摘要:
      In order to improve the reliability of UAV parachuted recovery system, combined with the hardware and the function, the fault mode and effects was analyzed. By use of quantitative analysis and criticality matrix, the fault criticality was analyzed. It was concluded that the fault mode of parachute inaccurate furl should be focused on; the preventive measures was given, which significantly improves the system′ s reliability.
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