THERMAL DEMAGNETIZATION AND RANDOMNESS OF DOMAIN NUCLEATION OF SINGLE PHASE Nd_2 Fe_(14) B

Based on the observation of temperature variation of both domain structure and magnetic con-trast.the thermal demagnetization and randomness of domain nucleation was discussed.     

一种轴向风冷结构对高速永磁电机转子温升的抑制研究

在变频器驱动方式下,高速永磁电机具有较大的转子涡流损耗,由于其转子的散热能力较差,易使永磁体温升较高,而发生不可逆失磁现象。采用机壳水冷结构可以有效地带走电机定子侧的热量,但是对于高速永磁电机的转子部位,水冷结构的冷却效果有限。以一台15 kW、30 000 r/min的高速永磁电机为例,设计了一种风、水混合冷却结构,基于流固耦合的计算方法分析了水速、风向以及不同风道截面积对电机永磁体部位温升的影响,并得出了相对的最优值。与仅采用水冷结构相比,增加该风冷结构可使永磁体温升降低了18.1 K,该结构可对大功率高速永磁电机的冷却系统设计提供一定的参考。     

SAFARI engineering model 50 mK cooler

SAFARI is an infrared instrument developed by a European based consortium to be flown in SPICA, a Japanese led mission. The SAFARI detectors are transition edge sensors (TES) and require temperatures down to 50 mK for their operation. For that purpose we have developed a hybrid architecture based on the combination of a 300 mK sorption stage and a small adiabatic demagnetization stage. An engineering model has been designed to provide net heat lifts of 0.4 and 14 μW respectively at 50 and 300 mK, with an overall cycle duration of 48 h and a duty cycle objective of over 75%. The cooler is self-contained, fits in a volume of 156 × 312 × 182 mm and is expected to weigh 5.1 kg. It has been designed to withstand static loads of 120 g and a random vibration level of 21 g RMS.     

基于特高压交流变电站检修典型问题分析

本文在对于特高压交流变电站检修典型问题演技中,主要对于轮停检修感应电压问题及测量误差等问题进行分析,希望能够为其他特高压交流变电站检修工作提供一定帮助.     

Thermodynamic performance of the 3-stage ADR for the Astro-H Soft-X-ray Spectrometer instrument

The Soft X-ray Spectrometer (SXS) instrument (Mitsuda et al., 2010) [1] on Astro-H (Takahashi et al., 2010) [2] will use a 3-stage ADR (Shirron et al., 2012) to cool the microcalorimeter array to 50 mK. In the primary operating mode, two stages of the ADR cool the detectors using superfluid helium at ⩽1.20 K as the heat sink (Fujimoto et al., 2010). In the secondary mode, which is activated when the liquid helium is depleted, the ADR uses a 4.5 K Joule–Thomson cooler as its heat sink. In this mode, all three stages operate together to continuously cool the (empty) helium tank and single-shot cool the detectors. The flight instrument – dewar, ADR, detectors and electronics – were integrated in 2014 and have since undergone extensive performance testing. This paper presents a thermodynamic analysis of the ADR’s operation, including cooling capacity, heat rejection to the heat sinks, and various measures of efficiency.     

玻璃包覆钴基非晶丝巨磁阻抗的长度效应

通过测量长度不同的玻璃包覆钴基非晶丝在频率为100kHz时的GMI值,近似计算出玻璃包覆钴基非晶丝的圆周磁导率.玻璃包覆钴基非晶丝圆周磁导率下降随着长度增加而变得剧烈,导致GMI变化更剧烈.利用玻璃包覆钴基非晶丝的磁畴模型,分析不同长度时玻璃包覆钴基非晶丝的磁化过程,合理解释了GMI效应随玻璃包覆钴基非晶丝长度增加而明显的现象.     

Operating modes and cooling capabilities of the 3-stage ADR developed for the Soft-X-ray Spectrometer instrument on Astro-H

A 3-stage adiabatic demagnetization refrigerator (ADR) (Shirron et al., 2012) is used on the Soft X-ray Spectrometer instrument (Mitsuda et al., 2010) on Astro-H (Takahashi et al., 2010) [3] to cool a 6 × 6 array of X-ray microcalorimeters to 50 mK. The ADR is supported by a cryogenic system (Fujimoto et al., 2010) consisting of a superfluid helium tank, a 4.5 K Joule–Thomson (JT) cryocooler, and additional 2-stage Stirling cryocoolers that pre-cool the JT cooler and cool radiation shields within the cryostat. The ADR is configured so that it can use either the liquid helium or the JT cryocooler as its heat sink, giving the instrument an unusual degree of tolerance for component failures or degradation in the cryogenic system. The flight detector assembly, ADR and dewar were integrated into the flight dewar in early 2014, and have since been extensively characterized and calibrated. This paper summarizes the operation and performance of the ADR in all of its operating modes.     

永磁电机退磁电流的仿真与测试

受外磁场、温度场、化学反应、机械振动等因素的影响,永磁电机在运输或工作过程中可能发生不可逆退磁.论文以样机为例,通过有限元的计算和分析,给出了电机退磁电流的计算方法,仿真结果可以以图表或图形等多种方式给出,直观、简洁、易于理解.另外论文还介绍了一种退磁电流的测试方法,结合磁场的有限元分析对永磁电机的退磁电流进行分析,通过验证试验结果与有限元分析非常吻合.为了保证电机在生命周期内的正常运转,在电机设计时应保证永磁体在最严酷的工作环境中各部分的最大去磁工作点应高于拐点位置.     

低温技术在太空监测领域的应用

随着低温技术的发展,制冷机的各方面工作性能显著改进,低温技术在航天领域得到了广泛应用。介绍了低温技术在国外太空监测卫星中的应用情况,分析其发展趋势。对太空监测所需要不同温度区间的制冷方法进行了总结,最后以国外执行监测任务卫星上的制冷系统为例说明制冷系统设计过程。     

基于分形维数的PMSM局部退磁故障诊断

为了实现永磁同步电机(PMSM)永磁体局部退磁故障诊断,首先建立计及永磁体局部退磁故障的PMSM数学模型,实现永磁体局部退磁故障电气特性的定性与定量描述。在此基础上,提出了集成自适应基波提取和经验模态分解(EMD)于一体,基于分形维数的永磁体局部退磁故障诊断方法。最后,通过PMSM驱动系统稳态和动态运行工况对所提出的永磁体局部退磁故障诊断方法进行仿真测试和实验验证,综合系统仿真和实验验证结果证实了该方法的可行性和有效性。