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我厂独家引进德国科隆(KROHNE)公司技术和设备生产的 H27系列金属浮子流量计,是采用新工艺、新结构和独特的计算方法生产的直通式流量计。因其具有独特的优点和齐全的类型已广泛应用于石油、化工、造纸和冶金等行业的流量自动检测与自动控制系统中。1 特点H27 系列金属浮子流量计具有以下的特点:a.检测、传动部件为全机械结构,长期运行稳定可靠;b.标准化设计,DN15-DN100口径的流量计,设计高度为250mm;c.浮子短行程设计,在任何位置上浮子都不会突出测量管;d.凸轮板线性修正及流量刻度为线性读数;e.利用流量转换计算方法,实现刻度为实际介质操作状态下的流量,免除了操作者进行换算的过程; 相似文献
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浮子流量计的发展介绍 总被引:2,自引:0,他引:2
介绍了目前市场流量计类型及其优势、略势,综合介绍浮子流量计,结合各国金属管浮子流量计发展的不同情况,引出金属管浮子流量计将有更广阔的发展前景、更庞大的应用市场。 相似文献
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浮子流量计又称转子流量计,是以浮子在垂直锥形管内随着流量变化而升降,改变它们之间形成的流通环隙面积作流量测量的体积流量仪表.本世纪初即盛行欧洲,取名罗托计(Rotameter);在美国、日本也有称作变而积流量计或面积流量计,实际上本类仪表只是变面积流量计的一种,因占了大部分习惯以变面积流量计称之.浮子流量计是量大而广的产品,80年代中期,日本、西欧、美国的销售金额占流量仪表的11%~17%,1990年我国约占14%;现场装用台数占装用流量仪表的15%~20%.我国产量1990年估计在12~14万台,其中95%以上为玻璃锥管浮子流量计. 相似文献
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浮子流量传感器中存在的非线性问题是影响浮子流量计测量精度的一个重要因素,为了解决这个问题,作者深入研究了浮子流量传感器的特性,利用最小二乘法拟合数据,分析浮子高度和流量之间的非线性关系.理论和实验研究结果表明,针对目前应用的短管型浮子流量计流量和浮子高度之间存在明显的非线性关系,并且发现在其他条件相同的情况下浮子行程的增加即锥管锥角的减小对浮子流量传感器线性度的改善具有重要的作用. 相似文献
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在核电站项目建设的调试及运营期间,调试及运行人员报告部分金属管浮子流量计在运行时存在卡涩情况。为应对浮子流量计卡涩的问题,基于对浮子流量计测量原理的分析,结合现场故障流量计的拆解情况进行卡涩故障的机制推演,完整分析了浮子流量计卡涩故障的环境工况因素和自身结构条件,并得出卡涩故障是管道内未吹扫干净的铁磁性杂质和浮子流量计运行机制共同作用所致的结论。根据故障机制的各作用环节提出了针对性的解决方案。在此基础上,对浮子流量计厂家提出的解决方案进行了分析,并对后续核电项目选型使用金属管浮子流量计提出了避免卡涩故障的具体应对措施。该研究结果可用于指导核电站流量测量方案的制订,对浮子流量计的设计改进和研发方向有启示作用。 相似文献
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“流量测量方法和仪表选用”讲座 第十四讲 浮子流量计的选用(二) 总被引:1,自引:0,他引:1
四、应用概况和选用考虑要点1.应用概况按用途选择合适类型,如只要现场指示,首先考虑价廉的玻璃管浮子流量计,如温度、压力不能胜任则选用就地指示金属管浮子流量计;如需要远传输出作流量控制或总量积算,一般首先选用带电信号输出的金属管浮子流量计;如环境气氛有防爆要求的,则可选用气远传仪表或防爆型电远传仪表. 相似文献
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就玻璃浮子流量计采用差动变压器检测浮子位移,实现电远传的方法进行了介绍,重点介绍了在这种方法下所产生的非线性利用转换器改变反馈电压而获得补偿。补偿后的精确度可达到2.5%。 相似文献
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Three dimensional numerical simulations of long-span bridge aerodynamics, using block-iterative coupling and DES 总被引:1,自引:0,他引:1
The design of long-span bridges often depends on wind tunnel testing of sectional or full aeroelastic models. Some progress has been made to find a computational alternative to replace these physical tests. In this paper, an innovative computational fluid dynamics (CFD) method is presented, where the fluid-structure interaction (FSI) is solved through a self-developed code combined with an ANSYS-CFX solver. Then an improved CFD method based on block-iterative coupling is also proposed. This method can be readily used for two dimensional (2D) and three dimensional (3D) structure modelling. Detached-Eddy simulation for 3D viscous turbulent incompressible flow is applied to the 3D numerical analysis of bridge deck sections. Firstly, 2D numerical simulations of a thin airfoil demonstrate the accuracy of the present CFD method. Secondly, numerical simulations of a U-shape beam with both 2D and 3D modelling are conducted. The comparisons of aerodynamic force coefficients thus obtained with wind tunnel test results well meet the prediction that 3D CFD simulations are more accurate than 2D CFD simulations. Thirdly, 2D and 3D CFD simulations are performed for two generic bridge deck sections to produce their aerodynamic force coefficients and flutter derivatives. The computed values agree well with the available computational and wind tunnel test results. Once again, this demonstrates the accuracy of the proposed 3D CFD simulations. Finally, the 3D based wake flow vision is captured, which shows another advantage of 3D CFD simulations. All the simulation results demonstrate that the proposed 3D CFD method has good accuracy and significant benefits for aerodynamic analysis and computational FSI studies of long-span bridges and other slender structures. 相似文献
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Gradient-based aerodynamic shape optimization using computational fluid dynamics (CFD), and time dependent problems in aeroelasticity, that is, coupled calculations between computational structural mechanics (CSM) and CFD, require repeated deformations of the CFD mesh.An interpolation scheme, based on radial basis functions (RBF), is devised in order to propagate the deformations from the boundaries to the interior of the CFD mesh. This method can lower the computational costs due to the deformation of the mesh, in comparison with the usual Laplace smoothing. Moreover, the algorithm is independent of the mesh connectivities. Therefore, structured and unstructured meshes are equally treated as well as hybrid meshes.The application of this interpolation scheme in problems of aerodynamic shape optimization is also carefully investigated. When the optimization is executed by a gradient-based algorithm the cost function is differentiated with respect to the design parameters in order to obtain the gradient. The gradient is most efficiently and accurately calculated by solving a certain adjoint equation derived from the discretized flow equations. The calculation of the gradient, which is detailed in this presentation, involves the Jacobian matrix of the mesh deformation.Finally, we present the results of an optimization of the ONERA M6 wing at transonic speed using the interpolation algorithm. The results are used for comparison with another technique of mesh deformation. The quality of the mesh obtained by the new algorithm, and the interpolation error, are analyzed with respect to the parameters of the interpolation scheme: the type of RBF, the RBF’s shape parameter, and the sets of control points. 相似文献
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基于CFD的集装箱船阻力性能优化 总被引:1,自引:0,他引:1
基于CFD方法实现船体型线的自动优化。应用船型参数化建模方法分析特征参数,提取设计变量,以兴波阻力最小为目标,分别采用Sobol算法和Tsearch算法实现船体型线的自动优化。将上述方法应用于5 100 TEU集装箱船的型线自动优化,运用Shipflow软件进行CFD数值计算。评估结果表明优化船型在弗劳德数Fr=0.26时总阻力减少3.62%,说明该方法可行。 相似文献
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A method is proposed to estimate the flow-induced drag on the actuator arm inside a hard disk drive. Typically, drag forces and moments on the actuator are computed as part of a computational fluid dynamics (CFD) solution of the flow field in the entire drive. Unidirectional coupling from the flow to the structure is then imposed to determine the structural response of the arm to the flow induced forcing. The methodology proposed here aims to reduce the simulation time associated with the flow calculations by directly estimating the forcing functions. The approach involves fitting a piecewise linear model (PLM) to the forcing frequency spectrum and interpolating or extrapolating the model to provide estimates of the spectrum at different points in the parameter space. A simple guideline for the formulation of such models is the conservation of energy between the CFD and PLM spectrum. Numerical experiments show that the linear models predict the behavior of arm to within 3% accuracy of the full CFD solution. The proposed technique is applied to two parameters: the disk RPM and the radial position of the arm. Clear trends are manifested for both parameters, making it possible to use this method to estimate forcing functions for a range of disk speeds and radial positions of the arm. This technique opens up the possibility of flow related design or optimization, which was previously thought to be prohibitively expensive. 相似文献
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气体转子流量计广泛应用于各行业中气体流量的测量,其准确度关系到生产过程的安全和产品质量,因此需要对现场的转子流量计进行校准。文章就使用标准表法校准过程中碰到的一些问题进行一些讨论。 相似文献