中国飞机结构寿命可靠性评定技术的发展与展望

doi:10.7527/S1000-6893.2022.27869

固体力学与飞行器总体设计

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中国飞机结构寿命可靠性评定技术的发展与展望

闫楚良

北京航空航天大学航空科学与工程学院, 北京 100191

收稿日期:2022-07-29 修回日期:2022-07-31 发布日期:2022-08-03
通讯作者: 闫楚良,E-mail:yancl1360@126.com E-mail:yancl1360@126.com
基金资助:
国家自然科学基金（50135010）

Development and prospect of aircraft structural life reliability assessment technology in China

YAN Chuliang

School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China

Received:2022-07-29 Revised:2022-07-31 Published:2022-08-03
Supported by:
National Natural Science Foundation of China (50135010)

摘要/Abstract

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。

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

Abstract: 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.

Key words: 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

中图分类号:

V240.2

闫楚良. 中国飞机结构寿命可靠性评定技术的发展与展望[J]. 航空学报, 2022, 43(10): 527869-527869.

YAN Chuliang. Development and prospect of aircraft structural life reliability assessment technology in China[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(10): 527869-527869.

参考文献

[1] 高镇同, 熊峻江. 疲劳可靠性[M]. 北京:北京航空航天大学出版社, 2000. GAO Z T, XIONG J J. Fatigue reliability[M]. Beijing:Beijing University of Aeronautics & Astronautics Press, 2000 (in Chinese).
[2] 高镇同. 疲劳应用统计学[M]. 北京:国防工业出版社, 1986. GAO Z T. Fatigue applied statistics[M]. Beijing:National Defense Industry Press, 1986 (in Chinese).
[3] 闫楚良. 我国飞机寿命与结构可靠性评定技术变革与守正创新[C]//面向2050的空天创新青年科学家论坛.2021. YAN C L. Reform and innovation of aircraft life and structural reliability assessment technology in China[C]//Young Scientists Innovation Congress on Aeronautics and Astronautics for 2050.2021(in Chinese).
[4] 闫楚良. 先进复合材料在航空航天领域中的应用及展望[C]//先进复合材料与智能制造高峰论坛. 2021. YAN C L. Application and prospect of advanced composites in aeronautics and astronautics[C]//Advanced Composite Materials and Intelligent Manufacturing Summit Forum. 2021 (in Chinese).
[5] 闫楚良. 不忘初心牢记使命——加快推进我国飞机寿命与结构可靠性技术变革与守正创新[C]//第七届中国航空强度技术发展高峰论坛. 2022. YAN C L. Remaining true to our original aspiration and keeping our mission firmly in mind-accelerate reform and innovation of aircraft life and structural reliability assessment technology in China[C]//The Seventh China Aviation Strength Technology Development Summit Forum, 2022 (in Chinese).
[6] 高镇同. 飞机疲劳寿命分散系数:BH-B884[R]. 北京:北京航空学院,1982:3-9. GAO Z T. Aircraft fatigue life scatter factor:BH-B884[R]. Beijing:Beijing Institute of Aeronautics, 1982:3-9 (in Chinese).
[7] YAN C L, LIU K G. Fatigue scatter factor of whole life and reliability of aircraft structure service life[J]. Advanced Materials Research, 2008, 44-46:739-744.
[8] 闫楚良, 刘克格. 飞机结构经济寿命设计与可靠性评定[M]. 北京:航空工业出版社, 2011. YAN C L, LIU K G. Economic life design and reliability assessment of aircraft structures[M]. Beijing:Aviation Industry Press, 2011 (in Chinese).
[9] YAN C L, LIU K G. Theory of economic life prediction and reliability assessment of aircraft structures[J]. Chinese Journal of Aeronautics, 2011, 24(2):164-170.
[10] 闫楚良. 飞机载荷谱实测技术与编制原理[M]. 北京:航空工业出版社, 2011. YAN C L. Measuring technology and compilation theory of aircraft load spectrum[M]. Beijing:Aviation Industry Press, 2011(in Chinese).
[11] 闫楚良, 田兆锋. 飞机载荷谱数据库设计技术[M]. 北京:航空工业出版社, 2013. YAN C L, TIAN Z F. Airplane load spectrum database design[M]. Beijing:Aviation Industry Press, 2013 (in Chinese).
[12] 闫楚良, 苏开鑫. 飞机起落架安全寿命与损伤容限设计[M]. 北京:航空工业出版社, 2011. YAN C L, SU K X. Safety life and damage tolerance design of aircraft landing gear[M]. Beijing:Aviation Industry Press, 2011 (in Chinese).
[13] YAN C L, LIU K G. Theory of active reliability-based design for predetermined life of structures[J]. Advanced Materials Research, 2008, 44-46:745-750.
[14] 闫楚良, 高镇同. 飞机高置信度中值随机疲劳载荷谱的编制原理[J]. 航空学报, 2000, 21(2):118-123. YAN C L, GAO Z T. Compilation theory of median stochastic fatigue load spectrum with high confidence level for airplane[J]. Acta Aeronautica et Astronautica Sinica, 2000, 21(2):118-123 (in Chinese).
[15] 闫楚良, 张书明. 中值随机载荷谱数据处理专家系统[R]. 北京:北京机械结构强度研究中心, 1999. YAN C L, ZHANG S M. Data treatment expert system for median stochastic load-spectrum[R]. Beijing:Beijing Mechanical Structure Strength Research Center, 1999(in Chinese).
[16] 闫楚良, 张书明, 叶舸, 等. 中值随机载荷谱数据处理专家系统[J]. 北京航空航天大学学报, 2000, 26(4):428-431. YAN C L, ZHANG S M, YE G, et al. Data treatment expert system for Median stochastic load-spectrum[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(4):428-431 (in Chinese).
[17] 闫楚良, 高镇同. 最少空测采样飞行起落次数设计准则[J]. 航空学报, 1999, 20(6):514-517. YAN C L, GAO Z T. Design criterion of the flight takeoff landing number of minimum no loading measurement sampling[J]. Acta Aeronautica et Astronautica Sinica, 1999, 20(6):514-517 (in Chinese).
[18] 闫楚良, 张书明, 高建民,等. 大型结构部件载荷试验方法研究[R]. 北京:北京机械结构强度研究中心, 1998. YAN C L, ZHANG S M, GAO J M, et al. Study on load test methods for large structural components[R]. Beijing:Beijing Mechanical Structure Strength Research Center,1998 (in Chinese).
[19] CRAIG H. World air forces directory 2022[J]. Flight International, 2021:12-34.
[20] ZGELA M, MADLEY M W B. Durability and damage tolerance testing and fatigue life management:ACF-18 Experience[R]. Department of National Defence Ottawa (Ontario) Directorate of Aerospace Support Engineering, 1991.
[21] HEWITT R L, WEISS J P, NOR P K. Spectrum editing for a full-scale fatigue test of a fighter aircraft wing with buffet loading[C]//Symposium on Fatigue Testing & Analysis Under Variable Amplitude.2003.
[22] MAIN B, MOLENT L, SINGH R, et al. Fatigue crack growth lessons from thirty-five years of the Royal Australian Air Force F/A-18 A/B Hornet Aircraft Structural Integrity Program[J]. International Journal of Fatigue, 2020, 133:105426.
[23] HONG N. A modified rainflow counting method[J]. International Journal of Fatigue, 1991, 13(6):465-469.
[24] BEUMLER T. MoC for A380 hybrid structure[C]//Aircraft Structural Program (ASIP) Conference. 2008.
[25] KANT R, CHAUHAN P S, BHATT G, et al. Corrosion monitoring and control in aircraft:A review. Sensors for automotive and aerospace applications[M].Berlin:Springer, 2019:39-53.
[26] JIAO R, HE X F, LI Y H. Individual aircraft life monitoring:an engineering approach for fatigue damage evaluation[J]. Chinese Journal of Aeronautics, 2018, 31(4):727-739.

E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

中国飞机结构寿命可靠性评定技术的发展与展望

Development and prospect of aircraft structural life reliability assessment technology in China

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