航空学报
航空學報
항공학보
ACTA AERONAUTICA ET ASTRONAUTICA SINICA
2009年
12期
2316-2321
,共6页
模糊失效准则%疲劳%可靠性%Gauss-Legendre积分%Monte Carlo模拟
模糊失效準則%疲勞%可靠性%Gauss-Legendre積分%Monte Carlo模擬
모호실효준칙%피로%가고성%Gauss-Legendre적분%Monte Carlo모의
fuzzy failure criterion%fatigue%reliability%Gauss-Legendre integration%Monte Carlo simulation
针对常规设计中对功能函数失效状态规定与常识不符这种情况,提出了考虑模糊失效准则的结构疲劳寿命可靠性,将结构寿命视为随机变量,而设计寿命视为模糊变量,研究了设计寿命服从线性L-R分布时的结构疲劳寿命可靠度,给出了随机载荷下结构疲劳寿命概率密度函数的确定方法,并提出了随机变量与模糊变量相组合时的一种新的可靠度数值计算方法,该方法先利用Gauss-Legendre积分将模糊可靠度求解的二次积分转换成一次积分,列出与Legendre多项式零点相对应的阀值,然后在给定的阀值下,将设计寿命转化成普通的截集区间,在截集区间内假定结构疲劳寿命概率密度函数服从均匀分布,利用Monte Carlo模拟得到对应于该阀值的结构疲劳寿命可靠度值.数值结果表明,常规设计下结构的疲劳寿命可靠度偏于危险.
針對常規設計中對功能函數失效狀態規定與常識不符這種情況,提齣瞭攷慮模糊失效準則的結構疲勞壽命可靠性,將結構壽命視為隨機變量,而設計壽命視為模糊變量,研究瞭設計壽命服從線性L-R分佈時的結構疲勞壽命可靠度,給齣瞭隨機載荷下結構疲勞壽命概率密度函數的確定方法,併提齣瞭隨機變量與模糊變量相組閤時的一種新的可靠度數值計算方法,該方法先利用Gauss-Legendre積分將模糊可靠度求解的二次積分轉換成一次積分,列齣與Legendre多項式零點相對應的閥值,然後在給定的閥值下,將設計壽命轉化成普通的截集區間,在截集區間內假定結構疲勞壽命概率密度函數服從均勻分佈,利用Monte Carlo模擬得到對應于該閥值的結構疲勞壽命可靠度值.數值結果錶明,常規設計下結構的疲勞壽命可靠度偏于危險.
침대상규설계중대공능함수실효상태규정여상식불부저충정황,제출료고필모호실효준칙적결구피로수명가고성,장결구수명시위수궤변량,이설계수명시위모호변량,연구료설계수명복종선성L-R분포시적결구피로수명가고도,급출료수궤재하하결구피로수명개솔밀도함수적학정방법,병제출료수궤변량여모호변량상조합시적일충신적가고도수치계산방법,해방법선이용Gauss-Legendre적분장모호가고도구해적이차적분전환성일차적분,렬출여Legendre다항식영점상대응적벌치,연후재급정적벌치하,장설계수명전화성보통적절집구간,재절집구간내가정결구피로수명개솔밀도함수복종균균분포,이용Monte Carlo모의득도대응우해벌치적결구피로수명가고도치.수치결과표명,상규설계하결구적피로수명가고도편우위험.
In view of the fact that the failure state of the performance function in the traditional design is often inconsistent with common sense, a reliability model of fatigue life which takes into consideration the fuzzy failure criteria is presented. The fatigue life and the fatigue design life are treated respectively as a random variable and a fuzzy random variable, and reliability is analyzed when the fatigue design life obeys linear L-R distribution. The probability density function of fatigue life under random load is deduced. A new numerical algorithm for fuzzy reliability analysis with random variables and fuzzy variables is developed. The double integration to calculate fuzzy reliability is first reduced to univariate integration by use of Gauss-Legendre integration. Thresholds corresponding to Gauss-Legendre abscissas are listed, and the fatigue design life is truncated to the subset under the given threshold. Then the probability density function of fatigue life is supposed to be of uniform distribution in the truncated subset. The reliability of structure fatigue life corresponding to the threshold can be obtained using Monte Carlo simulation. Numerical results show that the fuzzy reliability analysis of fatigue life tends to provide more safety than traditional analysis does.