共查询到20条相似文献,搜索用时 62 毫秒
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文章针对二级斜齿圆柱齿轮减速传动,建立了一个包含时变啮合刚度、齿轮侧隙、齿轮偏心、轴承刚度、轴弯扭刚度和动态传递误差的42个自由度斜齿轮转子耦合传动系统,利用Runge-Kutta法对系统方程进行了求解,分析了输入转速、输入转矩和齿轮螺旋角变化对系统动态特性的影响。研究结果表明:由于存在陀螺效应,齿轮转子系统的高频模态频率随转速变化较大,螺旋角增大会导致模态频率减小,高速传动中轮齿啮合力较大,而且在高速传动中或者较小外载荷作用时齿轮转子更易出现脱齿和背冲现象。 相似文献
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采用计算机模拟方法对舰用大功率二级斜齿轮传动的振动进行分析研究.在研究单级斜齿轮传动振动中,建立了齿面坐标系,引入了局部啮合刚度的概念,给出了在齿轮啮合过程中单齿啮合刚度和总啮合刚度的一般计算公式.对加工、安装误差引起的激振力,则采用刚度加权法进行处理.在单级斜齿轮传动振动模型的基础上,建立了两级十二自由度的斜齿轮传动振动模型.在模型中进行了线性化处理,用RungeKutta法进行方程的求解,并比较了计算结果与实验结果. 相似文献
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采用计算机模拟方法对舰用大功率二级斜齿轮传动的振动进行分析研究,在研究单级斜齿轮传动振动中,建立了齿面坐标系,引入了局部啮合刚度的概念,给出了齿轮啮合过程中单啮合刚度和总啮合刚度的一般计算公式,对加工,安装误差引起的激振力,则采用刚度加权法进行处理,在单级斜齿轮传动振动模型的基础上,建立了两级十二自由度的斜齿轮传动振动模型。在模型中进行了线性化处理,用RangeKutta法进行方程的求解,并比较了 相似文献
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齿轮啮合是一个比较复杂的过程,由于渐开线齿廓的固有特性使得齿轮在啮合过程中会产生许多非线性的影响,这些非线性影响对于齿轮啮合特性的分析和优化有着举足轻重的意义。文章首先基于先进的有限元理论,提出一种能够准确计算齿轮啮合刚度,并可模拟齿轮啮合动态过程的有限元模型。其次将应用此模型考虑摩擦的影响对直齿轮齿根应力进行分析,并对直齿轮轮齿的齿根应力在啮合过程中的变化趋势以及相应的摩擦影响进行讨论和总结。 相似文献
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舰船武器系统海上航行精度测试[1]需要真航向进行系统误差分析,而舰船在没有装备真航向测量系统情况下,如何提供真航向测量数据一直是需要解决的难题。论文采用舰船高精度光电跟踪仪、有源岸标和差分GPS定位设备,对舰船瞬时真航向测量方法及其可行性进行了深入细致的分析与研究,最终确定出系统瞬时航向测量精度是否满足使用要求。 相似文献
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该文从几何精度系数出发给出了导航定位误差的一般分析方法,从而得出导航定位误差的简单估计和分析所造物标的最佳配置。 相似文献
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通过分析和推导船用天文测姿系统的各项误差源,建立各项误差与测量误差之间的数学模型,为航姿测量误差的定量计算提供理论基础,并对系统测量误差进行计算,绘制相应的影响曲线. 相似文献
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统计能量分析方法能够有效预示舰船和车辆等结构的高频振动及噪声。本文通过建立两子结构耦合模型,利用差分法研究了瞬态统计能量分析中参数误差对子结构响应能量的影响,同时给出了参数误差与所导致能量误差的关系函数。结果表明:对于外载荷直接激励的子结构,内损耗因子和耦合损耗因子的误差都会导致被预示总能量的减小。对于外载荷间接激励的子结构,内损耗因子的误差会导致峰值能量的减小,而耦合损耗因子的误差会导致峰值能量的增加。本文内容对改进动力学系统数值模型以及提高结构振动和噪声预示精度有一定的帮助。 相似文献
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舰用高精度激光陀螺惯导内杆臂误差分析及补偿方法研究 总被引:1,自引:0,他引:1
对于高精度激光陀螺旋转惯导系统,大部分惯性器件误差都能够通过惯性测量单元( IMU)旋转而调制掉,内杆臂误差不仅不能够被调制掉,反而因为 IMU旋转将误差引入到系统对准和导航过程中。基于此,本文对内杆臂误差进行分析与建模,推导内杆臂误差与导航速度误差之间的数学表达式,通过分析确定内杆臂长度和振动频率是影响内杆臂误差的2个因素,并提出基于内杆臂长度的误差补偿方法。最后,通过试验对内杆臂误差模型和补偿方法进行了验证。 相似文献
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This article presents a study on the accuracy of the numerical determination of the friction and pressure resistance coefficients
of ship hulls. The investigation was carried out for the KVLCC2 tanker at model- and full-scale Reynolds numbers. Gravity
waves were neglected, i.e., we adopted the so-called double-model flow. Single-block grids with H–O topology were adopted
for all the calculations. Three eddy viscosity models were employed: the one-equation eddy viscosity and the two-equation
models proposed by Menter and the TNT version of the two-equation k-ω model. Verification exercises were performed in sets of nearly geometrically similar grids with different densities in the
streamwise, normal, and girthwise directions. The friction and pressure resistance coefficients were calculated for different
levels of the iterative error and for computational domains of different size. The results show that on the level of grid
refinement used, it is possible to calculate the viscous resistance coefficients in H–O grids that do not match the ship contour
with a numerical uncertainty of less than 1%. The differences between the predictions of different turbulence models were
larger than the numerical uncertainty; however, these differences tended to decrease with increases in the Reynolds number.
The pressure resistance was remarkably sensitive to domain size and far-field boundary conditions. Either a large domain or
the application of a viscous–inviscid interaction procedure is needed for reliable results.
This work was presented in part at the International Conference on Computational Methods in Marine Engineering—MARINE 2007,
Barcelona, June 3–4, 2007. 相似文献
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系统观测目标误差渗透着系统误差和随机误差,系统误差和随机误差的分离与溯源理论和应用一直是误差分析的难点和热点。文中基于系统误差和随机误差的互相关系与传递特征,提出了以传递函数为基础的误差传递模型,并基于该模型,将复杂系统划分为若干个子系统,分析了各子系统在观测目标误差中的主次作用( primary and secondary position a-nalysis,PSPA)。算例表明,该理论能够分析得出引起观测误差灵敏度较高的子系统,这对于误差溯源、分析和控制误差,提高观测目标的精度具有一定的指导意义。 相似文献
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This paper presents a study on the numerical calculation of the friction resistance coefficient of an infinitely thin plate
as a function of the Reynolds number. Seven eddy-viscosity models have been selected: the one-equation turbulence models of
Menter and Spalart–Allmaras; the k-ω two-equation model proposed by Wilcox and its TNT, BSL and SST variants and the two-equation model. The flow has been computed at 14 Reynolds numbers in sets of seven geometrically similar Cartesian grids
to allow a reliable estimation of the numerical uncertainty. The effect of the computational domain size has been reduced
to negligible levels (below the numerical uncertainty). And the same holds for the iterative and round-off errors. In the
finest grids of each set, the numerical uncertainty of the friction resistance coefficient is always below 1%. Special attention
has further been given to the solution behaviour in the laminar-to-turbulent transition region. Curve fits have been applied
to the data obtained at the 14 Reynolds numbers and the numerical friction lines are compared with four proposals from the
open literature: the 1957 ITTC line, the Schoenherr line and the lines suggested by Grigson and Katsui et al. The differences
between the numerical friction lines obtained with the seven turbulence models are smaller than the differences between the
four lines proposed in the open literature. 相似文献