High Tc Superconductor Theoretical Models and Electromagnetic Flux Characteristics

High Tc Superconductors (HTS) have special electromagnetic characteristics and phenomena. Effort has been made in order to theoretically understand the applied HTS superconductivity and HTS behaviors for practical applications, various theoretical models related to the HTS electromagnetic properties have been developed. The theoretical models and analytic methods are summarized with regard to understanding the HTS magnetic flux characteristic which is one of the most critical issues related to HTS applications such as for HTS magnetic levitation application.     

Low-speed vehicle dynamics and ride quality using controlled D.C. electromagnets

The aim of this paper is to establish that attraction type systems, i.e. with controlled d.c. electromagnets, can be successfully employed for the suspension of urban transit vehicles, having speeds around 70 km/hr, without the aid of secondary suspension. The feasibility of the d.c. suspension systems is illustrated through the ride and track-clearance characteristics for a single-degree of freedom suspension system travelling along a ferromagnetic guideway with random roughness. Performance of the suspension system with active feedback of track-clearance, vertical velocity and vertical acceleration are discussed, and the analytical results are compared with experimental data obtained from a vibrating guideway test rig.     

Thermodynamic properties by levitation calorimetry — V. High-temperature heat content of liquid gallium

The heat content (enthalpy) of liquid gallium relative to the supercooled liquid state at 298.15 K has been measured by levitation calorimetry over the temperature range 1412–1630 K. Thermal energy increments were determined using an aluminum block calorimeter of conventional design. The sharp decrease of C _p with increasing temperature observed just above the melting point does not persist up to the high temperatures of the present work. When combined with recent laser-flash calorimetry results from the literature, the present work indicates that C _p is 26.46 ± 0.71 J · g-atom^–1 · K^–1 over the temperature range 587–1630 K.Paper presented at the Japan-United States Joint Seminar on Thermophysical Properties, October 24–26, 1983, Tokyo, Japan.     

Equipment for the Spectral Characterization of High-Temperature Particles

The spectral radiant characteristics of plume particles of a solid rocket engine are important in the design of the engine specific impulse, ablative material, and plume flame hiding. These parameters are measured from tests of the engine. Some equipment has been established to realize particle heating, uniform particle distribution, and measurements based on an FTIR spectral instrument. The equipment is based on SiC heating and is divided into a warm-up chamber and a measurement chamber to improve the particle temperature stability. A special design of uniform particle distribution combined with an acoustic levitation device is used to determine the particle falling speed. The spectral characteristics and the transmission rate of the particles have been measured by using the system including a standard blackbody, an assembled optical system, and an FTIR spectrometer. The measurements of particle concentration and temperature are given in detail. The instrument specifications are as follows: temperature range – 60–1500 °C; spectral range – 0.60–25 μm; and particle dimension range – 10–500 μm. Paper presented at the Seventh International Workshop on Subsecond Thermophysics, October 6–8, 2004, Orléans, France.     

主动电磁悬浮球系统的H_∞控制器

针对主动电磁悬浮球系统的鲁棒性问题,探讨了H∞控制器在该系统上的应用。首先建立了主动电磁悬浮球系统的线性化数学模型;然后对应H∞混合灵敏度框架,重点介绍了3个加权函数的双重意义及其对系统特性的影响,说明了H∞控制器的设计方法;并对一套实际系统设计了H∞控制器,对系统的性能进行了仿真和实验研究。研究结果表明,基于H∞控制器的主动电磁悬浮球系统具有较高的抗干扰性能和鲁棒稳定性。     

低气压下空气间隙电弧对覆冰绝缘子串直流闪络的影响

覆冰绝缘子串在直流闪络过程特别是低气压条件下中易产生空气间隙电弧形成"飘弧"现象,飘弧易桥接覆冰绝缘子串,且空气间隙电弧和冰面电弧具有不同的伏安特性,而传统的覆冰绝缘子串直流闪络模型由冰面电弧和剩余冰层电阻构成,没有考虑空气间隙电弧,在低气压下计算结果与实际情况相差较大。为了解此一现象,首先从理论上分析了飘弧对低气压下覆冰绝缘子串直流闪络电压的影响,建立了考虑和忽略空气间隙电弧的覆冰绝缘子串直流闪络模型,根据理论模型计算了相应的闪络电压,并与试验结果进行了比较分析。试验与理论计算结果表明,飘弧现象随着气压的降低和绝缘子串覆冰及污秽的程度增加而增加,低气压下进行绝缘子串直流闪络建模、预测和特性试验时应考虑空气间隙电弧及其飘弧的影响。     

A Permanent Magnet Linear Synchronous Motor Drive for HTS Maglev Transportation Systems

A permanent magnet linear synchronous motor （PMLSM） for a high temperature superconducting （HTS） maglev system has been studied, including the motor structure, control strategy, and analysis techniques. Finite element analysis （FEA） of magnetic field is conducted to accurately calculate major motor parameters. Equivalent electrical circuit is used to predict the drive＇s steady-state characteristics, and a phase variable model is applied to predict the dynamic performance. Preliminary experiment with a prototype has been made to verify the theoretical analysis and the HTS-PM synchronous driving technology.     

可变磁路式永磁悬浮系统的防跌落防吸附控制

永磁悬浮系统是一种典型的非线性系统,随着导磁体与悬浮物之间的气隙变化,控制特性发生变化,影响系统的稳定性。为防止外界干扰引起系统偏离平衡点时,悬浮物跌落或吸附到导磁体上,提出一种基于气隙变化的防跌落防吸附控制方法。在整个悬浮气隙内选取多点预设悬浮力,基于各设计点预设的悬浮力计算控制参数,并依据插值原理得到完整的防跌落防吸附控制律,有效补偿悬浮物运动时不均匀变化的悬浮力,提高系统的可控性,稳定性和鲁棒性。仿真和实验表明,防跌落防吸附控制方法能缓和冲击,提高防跌落性能,当外扰使气隙变大时悬浮力迅速变大,防止悬浮物跌落,当外扰使气隙变小时悬浮力迅速变小,防止悬浮物吸附于导磁体上。     

Photophoretic Levitation of Macroscopic Nanocardboard Plates

Scaling down miniature rotorcraft and flapping-wing flyers to sub-centimeter dimensions is challenging due to complex electronics requirements, manufacturing limitations, and the increase in viscous damping at low Reynolds numbers. Photophoresis, or light-driven fluid flow, was previously used to levitate solid particles without any moving parts, but only with sizes of 1–20 µm. Here, architected metamaterial plates with 50 nm thickness are leveraged to realize photophoretic levitation at the millimeter to centimeter scales. Instead of creating lift through conventional rotors or wings, the nanocardboard plates levitate due to light-induced thermal transpiration through microchannels within the plates, enabled by their extremely low mass and thermal conductivity. At atmospheric pressure, the plates hover above a solid substrate at heights of ≈0.5 mm by creating an air cushion beneath the plate. Moreover, at reduced pressures (10–200 Pa), the increased speed of thermal transpiration through the plate's channels creates an air jet that enables mid-air levitation and allows the plates to carry small payloads heavier than the plates themselves. The macroscopic metamaterial structures demonstrate the potential of this new mechanism of flight to realize nanotechnology-enabled flying vehicles without any moving parts in the Earth's upper atmosphere and at the surface of other planets.     

Error analysis to minimize cross-axis couplings in 6-DOF motion systems with a single moving part

In multi-axis motion control, cross-axis couplings cause error force and position disturbances in an axis when a desired motion is generated along another axis. Different from the parasitic errors that result from the imperfections of the mechanical bearings and reference surfaces, cross-axis perturbations are caused by errors that occur both statically (geometrical errors) and dynamically (in the transient responses) and are more prevalent in air-bearing and magnetic-levitation (maglev) stages. The parasitic errors are heavily dependent on the sizes of the stage's mechanical components, while the cross-axis perturbations depend significantly on the mover's speed and acceleration. For stages using permanent magnets (PMs) and Lorentz coils, the causes of off-axis forces include 1) errors in the coil turns' straightness, perpendicularity, and parallelism of the motor axes, and 2) errors in the local magnetizations and PMs' fringing effects. The purpose of this paper is to analyze the topologies of 6-degree-of-freedom (6-DOF) single-moving-part stages to minimize cross-axis couplings. The outcome is a stage configuration with reduced couplings and cross-axis perturbations. This is supported by experimental results performed on a newly developed 6-DOF maglev laser-interferometer stage. Its achieved root-mean-square (rms) positioning noise and minimum step size in XY are 3 nm and 10 nm, respectively. Its achieved resolution in out-of-plane rotations is 0.1 μrad. In addition to the analysis supported by these results, this paper introduces a new measure to represent cross-axis perturbations and to compare the effects of couplings in multi-axis positioning. This measure is entitled the cross-coupling quantity (CCQ) and calculated from the displacement of the stage in the axis of interest, the peak time of the response, and the peak-to-peak (p-p) error in the perturbed axis.