Assessment of optimum confidence interval of reliability with three-parameter Weibull distribution using bootstrap weighted-norm method
|更新时间:2026-07-07
|
Assessment of optimum confidence interval of reliability with three-parameter Weibull distribution using bootstrap weighted-norm method
Vol. 28, Issue 3, (2013)
作者机构:
1. 河南科技大学 机电工程学院,河南,洛阳,471003
2. 西北工业大学 机电学院,西安,710072
作者简介:
基金信息:
DOI:
CLC:
Published:2013
稿件说明:
移动端阅览
XIA Xin-tao, XU Yong-zhi, JIN Yin-ping, et al. Assessment of optimum confidence interval of reliability with three-parameter Weibull distribution using bootstrap weighted-norm method[J]. 2013, 28(3).
DOI:
XIA Xin-tao, XU Yong-zhi, JIN Yin-ping, et al. Assessment of optimum confidence interval of reliability with three-parameter Weibull distribution using bootstrap weighted-norm method[J]. 2013, 28(3).DOI:
Assessment of optimum confidence interval of reliability with three-parameter Weibull distribution using bootstrap weighted-norm method
The bootstrap weighted-norm method was proposed to evaluate the optimum confidence interval of reliability with three-parameter Weibull distribution.Based on the difference between the empirical values and the theoretical values of reliability
an information vector of the optimum parameters of the Weibull distribution was structured in the light of six criterions of the minimum weighted-norm.By bootstrap resampling the information vector of the optimum parameters
a generated information vector was obtained to simulate the probability density function of the parameters.The estimated truth-value and its confidence interval of the parameters were solved and the estimated truth-value function and its optimum confidence interval function of the reliability could accordingly be established under the given confidence level.The case studies of the rolling bearing performance life
the helicopter component failure and the specimen fatigue life indicate that the estimated truth-value function is in accord with empirical values of reliability by using bootstrap weighted-norm method
and the optimum confidence interval function is able to describe true state of the test results.
Predicting method of safety life of reusable liquid rocket engine turbopump
Analysis of scrapping characteristics and reliability of civil aero engine high pressure turbine blade in dual failure modes
Reliability evaluation of bearings based on small samples and zero⁃failure life test data
Rolling bearing reliability evaluation method based on LTSA fusion dimensionality reduction method
Reliability based multidisciplinary design optimization of single turbine stage based on parameterized mesh deformation
Related Author
Shijie LIU
Dengfeng LIU
Xiaoqiu MA
Guozhu LIANG
Zheng LIU
Li XIE
Jijun ZHANG
Changjiang LONG
Related Institution
Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
Laboratory of Science and Technology on Cryogenic Liquid Propulsion,Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
School of Astronatuics,Beihang University
System Engineering Department,MTU Maintenance Zhuhai Company Limited
Shanghai Aviation Military Representative Office of;the Army Equipment Department,People's Liberation Army