期刊文献+

中国飞机结构寿命可靠性评定技术的发展与展望 被引量:2

Development and prospect of aircraft structural life reliability assessment technology in China
原文传递
导出
摘要 首先,在中国40余年的飞机结构定寿与延寿研究成果的基础上,结合中国国情、试验条件和科技发展水平,探讨了机群个体寿命可靠性评定体系与单机寿命监控技术。该技术包括建立新机结构寿命可靠性验证体系,发展大子样载荷谱实测技术、大子样全尺寸飞机疲劳试验技术、试验装置模块化与智能化、以及中子光视觉监控技术等。然后,对中国飞机大数据智能监控平台建设进行了展望。该平台将中国飞机寿命可靠性评定技术提升至机群个体寿命可靠性评定与实时监控的国际先进水平,在保障飞行安全的同时,成倍延长机群使用寿命,改变中国与美国目前相对飞机数量少和寿命短的格局。 Based on the research achievements of aircraft life prediction and life extension for more than forty years, considering national conditions, test conditions, and development of science and technology in China, this paper discusses the individual aircraft of fleet life reliability prediction system and individual aircraft life monitoring technology, including establishing a structure reliability verification system of new aircraft, developing large sample load spectrum flight measurement technology, large sample full-scale aircraft fatigue test technology, modularization and intellectualization of test devices and visual detection devices, and neutron light vision monitoring technology and presents the prospects of establishing aircraft intelligent monitoring platform based on big data to develop the life reliability assessment of aircraft fleet in China into individual life reliability assessment of each aircraft in fleet which is advanced in the world. At the same time ensuring flight safety, the safe service life of aircraft fleet will be extended exponentially. The current situation of small quantity and short life of Chinese aircraft compared to American aircraft will be changed.
作者 闫楚良 YAN Chuliang(School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China)
出处 《航空学报》 EI CAS CSCD 北大核心 2022年第10期149-159,共11页 Acta Aeronautica et Astronautica Sinica
基金 国家自然科学基金(50135010)。
关键词 飞机寿命 新机结构验证 大子样测试 试验装置智能化 中子光视觉技术 单机实时监控 飞行安全 aircraft life new aircraft structure verification large sample test intellectualization of test device neutron light vision technology real-time monitoring of individual aircraft flight safety
  • 相关文献

参考文献9

二级参考文献31

  • 1高镇同.疲劳应用统计学[M].北京:国防工业出版社,1986.365-381. 被引量:113
  • 2高镇同.航空金属材料疲劳性能手册[M].北京:北京航空材料研究所,1981.. 被引量:9
  • 3傅惠民.疲劳强度概率分布[M].北京:北京航空学院研究生院,1986.. 被引量:1
  • 4Gao Z T, Xiong J J. Fatigue reliability. Beijing: Beihang University Press, 2000. 被引量:1
  • 5Pook L. Metal fatigue. Netherlands: Springer, 2007. 被引量:1
  • 6Stephens R I, Fatemi A, Stephens R R. Metal fatigue in engineering. 2nd ed. New York: Wiley Interscience, 2001. 被引量:1
  • 7Tong Y C. Literature review on aircraft structural risk and reliability analysis. DSTO-TR-1110. Melbourn, Australia: Aeronautical and Maritime Research Labo- ratory Defence Science and Technology Organisation, 2001. 被引量:1
  • 8Grooteman F. A stochastic approach to determine life-time and inspection schemes or aircraft components. International Journal of Fatigue 2008; 30(1): 138-149. 被引量:1
  • 9Nesterenko G I, Nesterenko B G.Ensuring structural damage tolerance of Russian aircraft. International Journal of Fatigue 2009; 31(6): 1054-1061. 被引量:1
  • 10Boiler C, Ihn J B, Staszewski W J, et al. Design principles and inspection techniques for long life endurance of aircraft structures. The 3rd International Workshop on Structural Health Monitoring. 2001. 被引量:1

共引文献106

同被引文献17

引证文献2

二级引证文献6

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部