综合应力加速贮存试验方案优化设计

doi:10.7527/S1000-6893.2014.0201

Abstract

Abstract:

In allusion to the complexity of environmental stresses electronic products encountered in the process of storage and the phenomenon that single stress is being used to conduct accelerated storage test currently, an optimum design method of temperature and humidity step-down-stress accelerated storage test based on the cumulative damage method is proposed. The minimum asymptotic variance of product's medium life estimated value at normal working stresses is taken as optimum target, each accelerated stress level as design variable. Meanwhile, combined with maximum likelihood estimation theory for parameter estimation, the mathematic model for multiple stresses accelerated storage test plan's optimal design is built. When genetic algorithm is employed to solve the optimum design result of accelerated storage test plan under multiple stresses of a meter, it is determined that the scheme is best when k equals 5. To improve the credibility, the Monte Carlo simulation is employed to compare the volatility of each scheme about minimum asymptotic variance and mean minimum asymptotic variance, which further proves that the scheme is optimal when k equals 5. The optimized test plan can not only solve optimization design for small sample accelerated storage test, but also ensure the accuracy of evaluation, reduce test times, shorten test time and save cost.

Key words: electronic equipment, multiple stresses, accelerated storage test, optimum design, step-down-stress

CLC Number:

V443
TB114.3

ZHOU Jie, YAO Jun, SU Quan, HU Honghua. Optimum design of accelerated storage test plan under multiple stresses[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(4): 1202-1211.

References

[1] Nelson W. Accelerated life testing step-stress models and data analysis[J]. IEEE Transaction on Reliability, 1980, R-29(2): 103-108.
[2] Nelson W. Accelerated testing-statistical model, test plans anddata analysis[M]. New York: John Wiley & Sons, 1990: 496-502.
[3] Hannaman D J, Zamani N, Dhiman J, et al. Error analysis for optimal design of accelerated tests[C]//Proceedings of the 1990 Re1iability Physics Symposium. New York: IEEE, 1990: 55-60.
[4] Escobar L A, Meeker W Q, Jr. Planning accelerated life tests with two or more experimental factors[J]. Technometrics, 1995, 37(4): 411-427.
[5] Chen W H, Li H S, Lian W Z, et al. Accelerated life test and statistical analysis of aerospace electrical connecters under multiple environmental stresses[J]. Journal of Zhejiang University: Engineering Science, 2006, 40(2): 348-351 (in Chinese). 陈文华, 李红石, 连文志, 等. 航天电连接器环境综合应力加速寿命试验与统计分析[J]. 浙江大学学报: 工学版, 2006, 40(2): 348-351.
[6] Chen W H, Feng H Y, Qian P, et al. Theory & method for optimum design of accelerated life test plan under multiple stresses[J]. Chinese Journal of Mechanical Engineering, 2006, 42(12): 101-105 (in Chinese). 陈文华, 冯红艺, 钱萍, 等. 综合应力加速寿命试验方案优化设计理论与方法[J]. 机械工程学报, 2006, 42(12): 101-105.
[7] Chen W H, Qian P, Ma Z K, et al. Optimum design of multiple stress accelerated life test plan under periodic inspection[J]. Chinese Journal of Scientific Instrument, 2009, 30(12): 2544-2550 (in Chinese). 陈文华, 钱萍, 马子魁, 等. 基于定时测试的综合应力加速寿命试验方案优化设计[J]. 仪器仪表学报, 2009, 30(12): 2544-2550.
[8] Meng Y F, Han R L, Pan G, et al. Optimal design of multiple stress accelerated life test with competing risks base on simulation[J]. China Measurement & Test, 2014, 40(1): 123-127 (in Chinese). 孟亚峰, 韩荣利, 潘刚, 等. 基于仿真的竞争失效产品综合应力加速寿命试验优化设计[J]. 中国测试, 2014, 40(1): 123-127.
[9] Zhang C H. Theory and method of step-down-stress accelerated life testing[D]. Changsha: National University of Defense Technology, 2002 (in Chinese). 张春华. 步降应力加速寿命试验的理论和方法[D]. 长沙: 国防科学技术大学, 2002.
[10] Li X S. Method and application of step-down-stress accelerated testing[J]. Structure & Environment Engineering, 2012, 39(6): 59-62 (in Chinese). 李宪珊. 步降应力加速试验方法及其应用[J]. 强度与环境, 2012, 39(6): 59-62.
[11] Feng W H, Hu C H, Hu J T, et al. Optimal design of simple step-down-stress accelerated life test[J]. Control Engineering of China, 2007, 14(S1): 50-52 (in Chinese). 冯文晖, 胡昌华, 胡锦涛, 等. 简单步降应力加速寿命试验的最优设计[J]. 控制工程, 2007, 14(S1): 50-52.
[12] Meng Y F, Han R L, Pan G. Optimal design of multiple step-down-stress accelerated life test with competing risks base on Monte-Carlo simulation[J]. Instrument Technique and Sensor, 2014, 1(3): 92-95 (in Chinese). 孟亚峰, 韩荣利, 潘刚. 竞争失效产品综合应力步降加速寿命试验优化设计Monte-Carlo仿真[J]. 仪表技术与传感器, 2014, 1(3): 92-95.
[13] Mao S S, Tang Y C, Wang L L. Reliability statistics [M]. Beijing: Higher Education Press, 2008: 334-342 (in Chinese). 茆诗松, 汤银才, 王玲玲. 可靠性统计[M]. 北京: 高等教育出版社, 2008: 334-342.
[14] Nasser F, Chen H L. Optimal simple step stress accelerated life test design for reliability prediction[J]. Journal of Statistical Planning and Inference, 2009, 139(1): 1799-1808.
[15] Preeti W S, Nidhi J. Optimum ramp-stress accelerated life test for m identical repairable systems[J]. Applied Mathematical Modelling, 2011, 35(1): 786-793.
[16] Peck D S. Comprehensive model for humidity testing correlation[C]//Proceedings of the 24th Annal in Reliability Physics Symposium. 1986: 44-50.
[17] Yao J, Xu M G, Zhong W Q. The research of step-down stress accelerated degradation data assessment method of a certain type of missile tank[J]. Chinese Journal of Aeronautics, 2012, 25(6): 917-924.
[18] Elsayed E A, Zhang H. Design of PH-based accelerated life testing plans under multiple-stress-type[J]. Reliability Engineering and System Safety, 2007, 92(1): 286-292.
[19] Elsayed E A, Zhang H. Design of optimum reliability test plans under multiple stresses[J]. Quality and Dependability, 2005, 3(1): 16-18.
[20] Fang K T, Ma C X. Orthogonal and uniform design[M]. Beijing: Science Press, 2001: 25-30 (in Chinese). 方开泰, 马长兴. 正交与均匀试验设计[M]. 北京: 科学出版社, 2001: 25-30.
[21] Lei Y J, Zhang S W. Genetic algorithm toolbox and its application[M]. Xi'an: Xidian University Press, 2014: 23-25 (in Chinese). 雷英杰, 张善文. 遗传算法工具箱及应用[M]. 西安: 西安电子科技大学出版社, 2014: 23-25.

Optimum design of accelerated storage test plan under multiple stresses

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Siyuan LIU, Yongqi XIE, Jian SU, Hongxing ZHANG, Guoguang LI. Steady-state working performance of loop heat pipes in acceleration environment: Comparative study [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(4): 126803-126803.
[2]	MA Zhenyang, ZUO Jing, SHI Chunlei, FENG Jiacheng, LIU Xuhong. Test and optimization of shield effectiveness for airborne electronic equipment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(7): 323538-323538.
[3]	LYU Kehong, CHENG Xianzhe, LI Huakang, ZHANG Yong, QIU Jing, LIU Guanjun. New developments of prognostic and health management technology for electronic equipment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(11): 23285-023285.
[4]	JIN Qichao, WANG Wenhu, JIANG Ruisong, ZHAO Dezhong, CUI Kang, XIONG Yifeng. Forward slip compensation method for designing rolling mold cavity of compressor blade [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(1): 420173-420173.
[5]	ZHANG Guolong, CAI Jinyan, LIANG Yuying, PAN Gang, LI wei. Research on Reliability Assessment Method of Electronic Equipment Based on Multi-stress ADT [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(12): 2815-2822.
[6]	XU Yuliang, SUN Jizhe, CHEN Xihong, WANG Guangming. Electronic Equipment Fault Prediction Method Based on Accelerated Degradation Testing and Particle Filter [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(8): 1483-1490.
[7]	ZHANG Yong, ZHU Zengwei, GAO Hong, ZHU Di. New Design Method of Electroforming Anode Profile [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(1): 182-188.
[8]	CHE Lu-feng;XIONG Bin;WANG Yue-lin. OPTIMUM DESIGN AND ELECTRICAL SIMULATION OF COMB-GIMBAL MICROMACHINED GYROSCOPE [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2002, 23(3): 211-214.
[9]	Chen Lin-gen;Cao Yue-yun. MULTIOBJECTIVE OPTIMIZATION PROCEDURE OF MULTISTAGE GAS TURBINE DESIGN [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(12): 653-656.
[10]	Ding Yun-liang;Liu Yi. FINITE ELEMENT ANALYSIS AND OPTIMUM DESIGN FOR THE FRONT-FUSELAGE WITH SANDWICH CONSTRUCTION [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(10): 510-514.
[11]	Chen Wei-dong;Gu Zhong-quan. ROBUST CONTROLLER DESIGN FOR STRUCTURAL VIBRATION BASED ON TOLERANCE CONTROL STRATEGY [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1992, 13(9): 522-527.
[12]	Wang Li-jun;Zhao Ling-cheng. EFFECTS OF THE PYLON PITCHING STIFFNESS ON WING-STORE FLUTTER [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1992, 13(9): 560-563.
[13]	Xi Zhongqin. A COMPUTATIONAL METHOD FOR DISTRIBUTING AIRCONDITIONING FLOW IN ELECTRONIC EQUIPMENT CABIN OF AIRPLANES [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(6): 304-307.
[14]	Yang Ling;Ma Zukang. OPTIMUM PLY DESIGN OF COMPOSITE LAMINATE SATISFYING RELIABILITY CONSTRAINTS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(2): 83-86.
[15]	Yang Bingxian . OPTIMUM DESIGN OF COMPOSITE LAMINATES CONSIDERING INTERLAMINA STRESS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1988, 9(8): 324-329.