摘要
研究了单侧容限系数法中子样容量n、置信度γ及名义存活率P与实际存活率α之间的定量关系,导出了α的预测公式。计算结果表明:在n较小,γ与P搭配不当时,将出现α小于P的不合理情况。此时,名义存活率P将过高地表示了安全性,从而使人盲目乐观。本文指出:在飞机或直升机结构可靠性分析中,子样容量n通常远小于43,因此,某些文献中建议取γ=90%,P=0.999999是不合理的,本文提出了新的建议。
n the structural reliability analysis one-sided tolerance limit X-KS is usually used hrthe lower limit of a normally distributed population X with unknown mean μand unknown standard deviation σ In the above expression k is called ont-sided tolerance limit factor and X and S are the sample estimates of μand σ,respectively. The tolerance interval(X-KS,+∞)is required to be such that the probability is equal to a preassigned valueγ(which is called confidenee) that the tolerance interval includes at least a given proportion Pof the population(which is called nominal survival probability).There is an important q uestion:what is the true survival probability a corresponding to the one-sided tolerance limil?In the present paper the formula for predictingois derived.From the numerical results,in some instances the true surviv- al probability a may be less than the nominal survival probability P. For example,when γ=90%,P=0.999 999,if the sample size n is less than 43 then α< P.In the aircraft or helicopter struc- tural reliability analysis the sample size n is usually much less than 43.Therefore,γ=90% and P=0.999 999 recommended in some literature are unreasonable.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1994年第3期331-335,共5页
Acta Aeronautica et Astronautica Sinica
关键词
可靠性分析
疲劳寿命
容限
reliability analysis,fatigue life,tolerances(mechanism)