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本文研究了阻尼介质对刚塑性圆板在高载(冲击荷载)作用下塑性动力响应的影响,得到了解析解并对此解进行了讨论。当阻尼介质参数趋于零时,本文结果与无阻尼解一致。文中还画出了荷载与阻尼介质对圆板运动时间和板中心点残余挠度的影响曲线。 相似文献
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Yiwei WANG Christian GOGU Nicolas BINAUD Christian BES Raphael T.HAFTKA Nam H.KIM 《中国航空学报》2017,30(3)
Airframe maintenance is traditionally performed at scheduled maintenance stops.The decision to repair a fuselage panel is based on a fixed crack size threshold,which allows to ensure the aircraft safety until the next scheduled maintenance stop.With progress in sensor technology and data processing techniques,structural health monitoring (SHM) systems are increasingly being considered in the aviation industry.SHM systems track the aircraft health state continuously,lead ing to the possibility of planning maintenance based on an actual state of aircraft rather than on a fixed schedule.This paper builds upon a model-based prognostics framework that the authors developed in their previous work,which couples the Extended Kalman filter (EKF) with a first order perturbation (FOP) method.By using the information given by this prognostics method,a novel cost driven predictive maintenance (CDPM) policy is proposed,which ensures the aircraft safety while minimizing the maintenance cost.The proposed policy is formally derived based on the trade-off between probabilities of occurrence of scheduled and unscheduled maintenance.A numerical case study simulating the maintenance process of an entire fleet of aircrafts is imple mented.Under the condition of assuring the same safety level,the CDPM is compared in terms of cost with two other maintenance policies:scheduled maintenance and threshold based SHM maintenance.The comparison results show CDPM could lead to significant cost savings. 相似文献
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An Equilibrium Multi-objective Optimization Model(EMOM) with self-regulated weighting factors has been proposed for the optimum design of non-circular clearance hole on the front flange of turbine disk. In the ‘‘equilibrium design", both the stress decrease around the hole and the least hole's profile variation are considered, which balances two ambivalent design goals. Specific discrete variables are applied to realize the standardization design in the optimization process, in which a Surrogate Genetic Coding Algorithm(SGCA) is introduced, and a special check module is used to get rid of repeated fitness evaluation of the samples. The method offers an equilibrium design for the non-circular clearance hole of the turbine disk with great accuracy and efficiency. 相似文献
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The classical probabilistic reliability theory and fuzzy reliability theory cannot directly measure the uncertainty of structural reliability with uncertain variables,i.e.,subjective random and fuzzy variables.In order to simultaneously satisfy the duality of randomness and subadditivity of fuzziness in the reliability problem,a new quantification method for the reliability of structures is presented based on uncertainty theory,and an uncertainty-theory-based perspective of classical Cornell reliability index is explored.In this paper,by introducing the uncertainty theory,we adopt the uncertain measure to quantify the reliability of structures for the subjective probability or fuzzy variables,instead of probabilistic and possibilistic measures.We utilize uncertain variables to uniformly represent the subjective random and fuzzy parameters,based on which we derive solutions to analyze the uncertainty reliability of structures with uncertainty distributions.Moreover,we propose the Cornell uncertainty reliability index based on the uncertain expected value and variance.Experimental results on three numerical applications demonstrate the validity of the proposed method. 相似文献
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为深入研究分级旋流火焰特性,以分级旋流模型燃烧室为研究对象,对四个不同燃料分级比(Rf)条件下的分级旋流火焰进行了数值研究,在时均燃烧场特性分析的基础上进一步对燃料分级比为1和3两个工况进行了基于壁面建模的大涡模拟(WMLES)研究。结果表明:燃料分级比的改变会影响中心回流区(CRZ)的长度和宽度。燃烧室中截面的散点分布图能够显示出不同燃料分级比条件下的燃烧特征。燃料分级比为1时,燃烧室剪切层仅存在零散的涡破碎区;而燃料分级比为3时,伴随涡破碎区还出现了单螺旋分支进动涡核(PVC)。通过FFT变换获得的燃烧室内剪切层速度能谱主频与进动涡核的旋转频率相同,表明内剪切层速度脉动的产生与进动涡核有关。另外进动涡核会使流场内的燃料分布和燃烧模式发生周期性的变化,进而影响燃烧过程。调整燃料分级比在1附近,能够使分级火焰达到稳定燃烧降低排放的目标。 相似文献
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