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781.
鲁世强 《南昌航空工业学院学报》1995,(1):64-71
在文献[1]的基础上论述了有摩擦、有间隙的三维弹性接触问题接触状态有限元解法,并通过理论考题进行了验证。最后,在应用部分对汽轮机汽缸法兰连接汽密性进行了计算。 相似文献
782.
标准转台等旋转体在转动时产生的角速度波动对被标定设备的数据可信度有很大影响。本文主要论述了角速度波动检测的重要性和可能性,并对检测的方法进行了介绍,用时域等信号处理方法对角速度波动数据进行了分析。 相似文献
783.
For structural systems with both epistemic and aleatory uncertainties, research on quantifying the contribution of the epistemic and aleatory uncertainties to the failure probability of the systems is conducted. Based on the method of separating epistemic and aleatory uncertainties in a variable, the core idea of the research is firstly to establish a novel deterministic transition model for auxiliary variables, distribution parameters, random variables, failure probability, then to propose the improved importance sampling(IS) to solve the transition model. Furthermore,the distribution parameters and auxiliary variables are sampled simultaneously and independently;therefore, the inefficient sampling procedure with an ‘‘inner-loop' for epistemic uncertainty and an‘‘outer-loop' for aleatory uncertainty in traditional methods is avoided. Since the proposed method combines the fast convergence of the proper estimates and searches failure samples in the interesting regions with high efficiency, the proposed method is more efficient than traditional methods for the variance-based failure probability sensitivity measures in the presence of epistemic and aleatory uncertainties. Two numerical examples and one engineering example are introduced for demonstrating the efficiency and precision of the proposed method for structural systems with both epistemic and aleatory uncertainties. 相似文献
784.
The damage and fracture in hot spinning of titanium alloy is a very complex process under the combined effects of microstructure evolution and stress state. In this study, their dependences on processing parameters were investigated by an integrated FE model considering microstructure and damage evolution, and revealing the effects of microstructure and stress states on damage evolution. The results show that the inner surface of workpiece with the largest voids volume fraction is the place with... 相似文献
785.
786.
787.
The elliptical cross-section spiral equal-channel extrusion (ECSEE) process is simulated by using Deform-3D finite element software. The ratio m of major-axis to minor-axis length for ellipse-cross-section, the torsion angle u, the round-ellipse cross-section transitional channel L1, the elliptical rotation cross-section transitional channel L2 and the ellipse-round cross-section transitional channel L3 are destined for the extrusion process parameters. The average effective strain eave on cross-section of blank, the deformation uniformity coefficient a and the value of maximum damage dmax are chosen to be the optimize indexes, and the virtual orthogonal experiment of L16 (45) is designed. The correlation degree of the process factors affecting eave, a and dmax is analyzed by the numerical simulation results using the weights and grey association model. The process parameters are optimized by introducing the grey situation decision theory and the ECSEE optimal combination of process parameters is obtained: u of 120 , m of 1.55, L1 of 7 mm, L2 of 10 mm, and L3 of 10 mm. Simulation and experimental results show that the material can be refined with the optimized structural parameters of die. Therefore, the optimization results are satisfactory. 相似文献
788.
Yongxin Hu Panfeng Huang Zhongjie Meng Dongke Wang Yingbo Lu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(9):2344-2351
Approaching control is a key mission for the tethered space robot to perform the task of removing space debris. But the uncertainties of the TSR such as the change of model parameter have an important effect on the approaching mission. Considering the space tether and the attitude of the gripper, the dynamic model of the TSR is derived using Lagrange method. Then a disturbance observer is designed to estimate the uncertainty based on STW control method. Using the disturbance observer, a controller is designed, and the performance is compared with the dynamic inverse controller which turns out that the proposed controller performs better. Numerical simulation validates the feasibility of the proposed controller on the position and attitude tracking of the TSR. 相似文献
789.
针对模拟电路故障不易被检测、不易被精确定位且现场情况复杂的特点,本文以基本共射放大电路为例重点研究了基于BP神经网络的模拟电路故障诊断方法。首先,提取待测电路特征值,对可能出现的电路故障编号,随机测量多组电路正常情况下和各故障状态下的电路特性,包括输入、输出电阻,上限、下限截止频率,增益等。随后,将测量得到的多组电路特征值用于故障检测模型的训练。接着,根据模型输出值与目标值的误差,调整模型参数,直至误差满足要求。最后,将模型参数固化于诊断系统微控制器的Flash中。经实验验证,依据该方法设计的便携式故障诊断系统具有较高准确率和较低的成本,切合社会生产实际。另外,由于其结合了深度学习算法和电子线路分析方法,也可用于电子信息类本科教育课程实践。 相似文献
790.
The two line elements(TLEs),released by the North American Aerospace Defense Command(NORAD),are chosen for CubeSats' mission operators.Unfortunately,they have errors and other accompanied problems,which cause large deviations in the in-track component.When a TLE value is available at a certain epoch,the dominant error is the angular error.It is proposed to correct the angular error by solving-for the mean argument of latitude at the desired epoch.A batch least squares technique and range rate measurements are used for the correction process.With the assistance of satellite tool kit(STK)software and Matlab,a simulation to verify the orbit determination(OD)technique is implemented.This paper provides an angular correction low cost OD method and presents a complete analysis for various test cases.This approach maintains high accuracy in cross-track and radial and makes great improvement in in-track at the same time,but it is exclusive for circular orbits.When it is applied to an elliptical orbit,the error will be unacceptable.Therefore,the angular error is corrected using the longitude of periapsis which totally mitigates the error at the epoch under consideration.For inclinations less than 20 o,the mean longitude is preferred for the angular correction as it provides more accuracy compared with the mean argument of latitude. 相似文献