期刊文献+
共找到385篇文章
< 1 2 20 >
每页显示 20 50 100
Evolution of Electron Phase Orbits Based on Multi-photon Nonlinear Compton Scattering 被引量:5
1
作者 HAO Dong-shan, HAO Xiao-fei (Dept.of Phys.,Zhumadian Teachers College, Zhumadian 463000,CHN) 《Semiconductor Photonics and Technology》 CAS 2003年第3期196-200,共5页
The electron movement based on the multi-photon nonlinear Compton scattering with the extra-intense stationary laser field is discussed by using KMR (Kroll-Morton-Rosenbluth) theory.We find that there exists only an e... The electron movement based on the multi-photon nonlinear Compton scattering with the extra-intense stationary laser field is discussed by using KMR (Kroll-Morton-Rosenbluth) theory.We find that there exists only an evolution from periodicity to non-periodicity of the un-captured electron phase orbits after the energy exchange between the electron beam and laser fields.With the increase of the absorbed photon number n by an electron, this evolution will be more and more faster, while it is rapidly decreased with the enhancement of the collision non-flexibility ξ of the electrons and photons; When the electrons are captured by the laser fields, the evolution is finished, the electrons will stably transport,and the photons dont give up the energy to these electrons. 展开更多
关键词 multi―photon nonlinear compton scattering electron phase orbits EVOLUTION
在线阅读 下载PDF
Evolution of Electron Phase Orbits of Multi-photon Nonlinear Compton Scattering in High Power Laser-plasma 被引量:1
2
作者 HAODong-shan LüJian 《Semiconductor Photonics and Technology》 CAS 2005年第2期107-110,共4页
The evolution of the electron phase orbits based on the multi-photon nonlinear Compton scattering with the high power laser-plasma is discussed by using Kroll-Morton-Rosenbluth theory. The random evolution of the un-c... The evolution of the electron phase orbits based on the multi-photon nonlinear Compton scattering with the high power laser-plasma is discussed by using Kroll-Morton-Rosenbluth theory. The random evolution of the un-captured electron phase orbits from periodicity to non-periodicity is found after the energy has been exchanged between the electron and photons. With the increase of the absorbed photon number n by an electron,this evolution will be more and more intense, while which is rapidly decreased with the enhancement of the collision non-flexibility ξ and their initial speeds of the electrons and photons,but this evolution is lower than that in the high power laser field. When the electrons are captured by the laser field,the evolution is finished,and the electrons will stably transport,and the photons don’t provide the energy for these electrons any more. 展开更多
关键词 multi-photon nonlinear compton scattering electron phase orbits EVOLUTION
在线阅读 下载PDF
Phase Residual Estimations for PCVs of Spaceborne GPS Receiver Antenna and Their Impacts on Precise Orbit Determination of GRACE Satellites 被引量:4
3
作者 TU Jia GU Defeng +1 位作者 WU Yi YI Dongyun 《Chinese Journal of Aeronautics》 SCIE EI CSCD 2012年第4期631-639,共9页
In-flight phase center systematic errors of global positioning system(GPS) receiver antenna are the main restriction for improving the precision of precise orbit determination using dual-frequency GPS.Residual appro... In-flight phase center systematic errors of global positioning system(GPS) receiver antenna are the main restriction for improving the precision of precise orbit determination using dual-frequency GPS.Residual approach is one of the valid methods for in-flight calibration of GPS receiver antenna phase center variations(PCVs) from ground calibration.In this paper,followed by the correction model of spaceborne GPS receiver antenna phase center,ionosphere-free PCVs can be directly estimated by ionosphere-free carrier phase post-fit residuals of reduced dynamic orbit determination.By the data processing of gravity recovery and climate experiment(GRACE) satellites,the following conclusions are drawn.Firstly,the distributions of ionosphere-free carrier phase post-fit residuals from different periods have the similar systematic characteristics.Secondly,simulations show that the influence of phase residual estimations for ionosphere-free PCVs on orbit determination can reach the centimeter level.Finally,it is shown by in-flight data processing that phase residual estimations of current period could not only be used for the calibration for GPS receiver antenna phase center of foretime and current period,but also be used for the forecast of ionosphere-free PCVs in future period,and the accuracy of orbit determination can be well improved. 展开更多
关键词 global positioning system precise orbit determination phase center variations phase residual estimation GRACE
原文传递
Effect of normalized plasma frequency on electron phase-space orbits in a free-electron laser 被引量:2
4
作者 吉驭嫔 王时建 +5 位作者 徐竟跃 徐勇根 刘晓旭 卢宏 黄小莉 张世昌 《Chinese Physics B》 SCIE EI CAS CSCD 2014年第2期242-246,共5页
Irregular phase-space orbits of the electrons are harmful to the electron-beam transport quality and hence deteriorate the performance of a free-electron laser (FEL). In previous literature, it was demonstrated that... Irregular phase-space orbits of the electrons are harmful to the electron-beam transport quality and hence deteriorate the performance of a free-electron laser (FEL). In previous literature, it was demonstrated that the irregularity of the electron phase-space orbits could be caused in several ways, such as varying the wiggler amplitude and inducing sidebands. Based on a Hamiltonian model with a set of self-consistent differential equations, it is shown in this paper that the electron- beam normalized plasma frequency functions not only couple the electron motion with the FEL wave, which results in the evolution of the FEL wave field and a possible power saturation at a large beam current, but also cause the irregularity of the electron phase-space orbits when the normalized plasma frequency has a sufficiently large value, even if the initial energy of the electron is equal to the synchronous energy or the FEL wave does not reach power saturation. 展开更多
关键词 free-electron laser electron phase-space orbit normalized plasma frequency IRREGULARITY
原文传递
Multiferroic phase transitions in manganites RMnO_3:A two-orbital double exchange simulation 被引量:1
5
作者 陶永梅 林林 +1 位作者 董帅 刘俊明 《Chinese Physics B》 SCIE EI CAS CSCD 2012年第10期456-461,共6页
The semi-quantum two-orbital exchange model is used to investigate the effect of small rare-earth ion substitution on orthorhombic RMnO 3 with A-type antiferromagnetic order,using the Monte Carlo algorithm,exact diago... The semi-quantum two-orbital exchange model is used to investigate the effect of small rare-earth ion substitution on orthorhombic RMnO 3 with A-type antiferromagnetic order,using the Monte Carlo algorithm,exact diagonalization,and zero-temperature optimization approaches.It is revealed that the substitution results in a rich multiferroic phase diagram where the coexisting A-type antiferromagnetic phase and spiral spin phase,pure spiral spin phase,coexisting spiral spin phase,the E-type antiferromagnetic phase,and the pure E-type antiferromagnetic phase emerge in sequence.The multiferroic phase transitions modulate substantially the electric polarization,which is consistent qualitatively with recent experiments. 展开更多
关键词 multiferroic phase R-site doping two-orbital exchange model
原文传递
Orbital Phase Theory and the Diastereoselectivity of Some Organic Reactions
6
作者 Yuji Naruse 《Journal of Materials Science and Chemical Engineering》 2018年第7期35-42,共8页
The orbital phase refers to the relationship between orbitals that originates from their wave character. We show here that the orbital phase essentially determines the diastereoselectivity of the following three organ... The orbital phase refers to the relationship between orbitals that originates from their wave character. We show here that the orbital phase essentially determines the diastereoselectivity of the following three organic reactions. 1) Torquoselectivity of the electrocyclicring-opening reaction of 3-substituted cyclobutenes;2) Contradictory torquoselectivity of the retro-Nazarov reaction;3) Diastereoselectivity in electrophilic addition to substituted ethylenes. 展开更多
关键词 orbitAL phase Theory DIASTEREOSELECTIVITY orbitAL phase CONTINUITY BOND Model Analysis
在线阅读 下载PDF
Reduced Dynamic Orbit Determination Using Differenced Phase in Adjacent Epochs for Spaceborne Dual-frequency GPS 被引量:4
7
作者 GU Defeng YI Dongyun 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2011年第6期789-796,共8页
We study on reduced dynamic orbit determination using differenced phase in adjacent epochs for spacebome dual-frequency GPS. This method not only overcomes the shortcomings that the epoch-difference kinematic method c... We study on reduced dynamic orbit determination using differenced phase in adjacent epochs for spacebome dual-frequency GPS. This method not only overcomes the shortcomings that the epoch-difference kinematic method cannot be used when observation geometry is poor or observations are insufficient, but also avoids solving the ambiguity in the zero-difference reduced dynamic method. As the epoch-difference method is not sensitive to the impact of phase cycle slips, it can lower the difficulty of slip detection in phase observation preprocessing. In the solution strategies, we solve the high-dimensional matrix computation problems by decomposing the long observation arc into a number of short arcs. By gravity recovery and climate experiment (GRACE) satellite orbit determination and compared with GeoForschungsZentrum (GFZ) post science orbit, for epoch-difference reduced dynamic method, the root mean squares (RMSs) of radial, transverse and normal components are 1.92 cm, 3.83 cm and 3.80 cm, and the RMS in three dimensions is 5.76 cm. The solution's accuracy is comparable to the zero-difference reduced dynamic method. 展开更多
关键词 dual-frequency GPS phase difference in adjacent epochs SATELLITE reduced dynamic orbit determination
原文传递
APPLICATION OF MOLECULAR ORBITAL THEORY TO ANALYSIS OF PHASE STABILITY FOR ALLOYS
8
作者 YIN Hong TAO Kun PAN Jinsheng LI Hengde Tsinghua University,Beijing,China professor.Department of Materials Science and Engineering,Tsinghua University,Beijing 100084,China 《Acta Metallurgica Sinica(English Letters)》 SCIE EI CAS CSCD 1993年第3期145-152,共8页
The critical _d vahues ( _ ) of the γ/(γ+σ).γ/(γ+μ) and γ/(γ+γ') phase boundaries in some ternar alloy phase diagrams at various temperatures are calculated by averaging the _d values of sererai selecte... The critical _d vahues ( _ ) of the γ/(γ+σ).γ/(γ+μ) and γ/(γ+γ') phase boundaries in some ternar alloy phase diagrams at various temperatures are calculated by averaging the _d values of sererai selected characteristic points at the phase boundaries.Approxmate equations for the temperature dependence of the critical _d of γ/(γ+σ).γ/(γ+μ) and γ/(γ+γ') phase boundaries are established.The accuracy of the analysis is discussed in detail. It is found for the first time that the average value of the bond order _ at the phase boundaries ts also approximatelr a constant and therefore a critical average bond order _ like - can be introduced for the analysts of phase stability 展开更多
关键词 molecular orbital theory allov phase stabilitv
在线阅读 下载PDF
天舟货运飞船全相位自主快速交会对接及在轨实现
9
作者 陈长青 张强 +3 位作者 解永春 刘宗玉 王曦 郝慧 《空间控制技术与应用(中英文)》 北大核心 2026年第1期103-110,共8页
文章描述天舟货运飞船全相位自主快速交会对接技术和在轨飞行结果.先介绍天舟货运飞船全相位自主快速交会对接方案,全相位自主交会对接由远距离导引段和近距离自主控制段组成,通过远距离导引终端精度的提高,可以配置不同的交会对接模式... 文章描述天舟货运飞船全相位自主快速交会对接技术和在轨飞行结果.先介绍天舟货运飞船全相位自主快速交会对接方案,全相位自主交会对接由远距离导引段和近距离自主控制段组成,通过远距离导引终端精度的提高,可以配置不同的交会对接模式,典型的有6.5 h快速交会对接、2 h快速交会对接和3 h快速交会对接.接着介绍天舟货运飞船交会对接方案研制和在轨任务的进化过程.最后给出天舟货运飞船快速交会对接在轨任务概况.天舟货运飞船交会对接方案设计过程和在轨表现表明其不断地朝着快速性、稳定性、标准型方向发展. 展开更多
关键词 天舟货运飞船 全相位 自主 快速交会对接 在轨
在线阅读 下载PDF
航天器泵驱单相流体回路在轨数据分析及预测
10
作者 郭嘉 郑红阳 +3 位作者 王德伟 车邦祥 徐侃 曹剑峰 《航天器工程》 北大核心 2026年第1期98-106,共9页
针对航天器热控单相流体回路直接采集的数据白噪声多、波动严重、难以直接提取有效信息的问题,文章提出赫斯特(Hurst)指数驱动的时序分解-滤波-预测三级在轨数据处理方法。通过Hurst指数量化数据特性,结合时间序列分解分离趋势项、周期... 针对航天器热控单相流体回路直接采集的数据白噪声多、波动严重、难以直接提取有效信息的问题,文章提出赫斯特(Hurst)指数驱动的时序分解-滤波-预测三级在轨数据处理方法。通过Hurst指数量化数据特性,结合时间序列分解分离趋势项、周期项与残差项,并应用傅里叶变换滤除白噪声与离散突变,构建调节分数积分模型进行未来趋势预测。经在轨数据分析,表明:航天器热控在轨数据会因为轨道运动引发的温度变化呈现周期性波动;泵转速呈现强回归性,液位呈现线性泄漏趋势,年泄漏量约0.6 mm;压力与液位显著线性相关。该方法可为航天器热控系统在轨安全运行提供支持。 展开更多
关键词 航天器 在轨数据 泵驱单相流体回路 时间序列分析 傅里叶变换
在线阅读 下载PDF
星载飞轮用双稳态抑振俘能一体化装置动力学特性研究
11
作者 刘庆生 刘海平 +2 位作者 张俊 周诗坤 江凌宇 《振动工程学报》 北大核心 2026年第3期666-676,共11页
为有效抑制星载飞轮系统振动响应并实现振动能量的收集利用,提出一种基于压电型欧拉屈曲梁非线性能量阱的抑振俘能一体化装置,采用标准能量收集电路,通过调整其设计参数,实现非线性系统的单/双稳态转换。针对卫星飞轮实际载荷工况,建立... 为有效抑制星载飞轮系统振动响应并实现振动能量的收集利用,提出一种基于压电型欧拉屈曲梁非线性能量阱的抑振俘能一体化装置,采用标准能量收集电路,通过调整其设计参数,实现非线性系统的单/双稳态转换。针对卫星飞轮实际载荷工况,建立有/无重力场耦合系统动力学模型,利用数值方法重点分析主动发射工况、在轨定速工况及在轨变速工况下,双稳态一体化装置的动力学特性。研究表明,相比于单稳态一体化装置,双稳态一体化装置在不同工况下均表现出更好的抑振性能和能量收集效果。试验证明了一体化装置的有效性。相关研究为星载高精度仪器设备振动抑制及能量收集提供了参考。 展开更多
关键词 星载飞轮 双稳态 振动控制 能量收集 主动发射阶段 在轨工作阶段
在线阅读 下载PDF
地月空间NRHO两脉冲调相轨道优化与分析
12
作者 李少峰 王有亮 +1 位作者 于锡峥 李明涛 《空间科学学报》 北大核心 2026年第1期175-188,共14页
Artemis任务建造与运行月球轨道门户空间站期间,将在近直线晕轨道(Near-Rectilinear Halo Orbit,NRHO)实施大量货运、载人飞行交会对接任务.针对NRHO调相轨道优化问题,基于圆型限制性三体问题模型,通过信赖域算法对转移时间进行遍历,采... Artemis任务建造与运行月球轨道门户空间站期间,将在近直线晕轨道(Near-Rectilinear Halo Orbit,NRHO)实施大量货运、载人飞行交会对接任务.针对NRHO调相轨道优化问题,基于圆型限制性三体问题模型,通过信赖域算法对转移时间进行遍历,采用非线性优化算法局部优化来修正位置误差,进而迭代求解非线性方程组降低速度增量,实现了低燃料消耗的NRHO调相优化;针对调相代价问题,对NRHO上不同转移时间和不同相位关系的调相进行了分析.结果表明,该算法计算效率较高,相比遗传算法减少了53.2%的计算时间;转移时间越长(转移轨道圈数越多),消耗的速度增量越小;目标航天器相位滞后时,选择绕NRHO外圈的调相方式更省燃料,反之,相位超前则选择绕内圈更省燃料;追踪航天器从近月点出发时燃料消耗更低. 展开更多
关键词 地月空间 圆型限制性三体问题 近直线晕轨道 调相轨道 信赖域算法
在线阅读 下载PDF
考虑单元相关性的多态多阶段任务系统可靠性评估
13
作者 詹凯 李翔宇 熊晓燕 《机械设计与制造》 北大核心 2026年第4期253-259,共7页
由于多阶段任务系统在工程领域的广泛应用,尤其是在航空航天领域,其可靠性分析受到了广泛关注。在以往的研究中,大多数研究都假设所有元件相互独立,这不符合工程实际。而在PMS中,系统结构会随着阶段的变化而变化,因此元件之间的依赖关... 由于多阶段任务系统在工程领域的广泛应用,尤其是在航空航天领域,其可靠性分析受到了广泛关注。在以往的研究中,大多数研究都假设所有元件相互独立,这不符合工程实际。而在PMS中,系统结构会随着阶段的变化而变化,因此元件之间的依赖关系也可能发生变化。为了解决这一问题,提出基于Copula函数的方法对具有相关元件的多态多阶段任务系统进行了可靠性研究分析。首先,利用不同的Copula函数对具有相关元件的多状态PMS系统的可靠度进行评估,其次使用RMSE、AIC、BIC等方法选择不同阶段的最佳Copula函数。最后使用航天器姿态轨道控制系统来说明该方法的正确性和有效性。 展开更多
关键词 系统可靠性 多态多阶段任务系统 相关元件 COPULA 姿态轨道控制系统
在线阅读 下载PDF
Multi-spacecraft Intelligent Orbit Phasing Control Considering Collision Avoidance 被引量:1
14
作者 LI Jian ZHANG Gang 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2022年第4期379-388,共10页
This paper proposes an intelligent low-thrust orbit phasing control method for multiple spacecraft by simultaneously considering fuel optimization and collision avoidance. Firstly,the minimum-fuel orbit phasing contro... This paper proposes an intelligent low-thrust orbit phasing control method for multiple spacecraft by simultaneously considering fuel optimization and collision avoidance. Firstly,the minimum-fuel orbit phasing control database is generated by the indirect method associated with the homotopy technique. Then,a deep network representing the minimum-fuel solution is trained. To avoid collision for multiple spacecraft,an artificial potential function is introduced in the collision-avoidance controller. Finally,an intelligent orbit phasing control method by combining the minimum-fuel neural network controller and the collision-avoidance controller is proposed. Numerical results show that the proposed intelligent orbit phasing control is valid for the multi-satellite constellation initialization without collision. 展开更多
关键词 orbit phasing control low thrust deep neural networks collision avoidance
在线阅读 下载PDF
An improved frequency shift method for ATI-SAR flat earth phase removal 被引量:1
15
作者 Yubin Zhang Jie Zhang +1 位作者 Junmin Meng Chenqing Fan 《Acta Oceanologica Sinica》 SCIE CAS CSCD 2019年第8期94-100,共7页
An improved frequency shift method is proposed to remove the flat earth phase in ATI-SAR ocean surface motion detection in this study. First, two conventional flat earth effect removal methods(i.e., the frequency shif... An improved frequency shift method is proposed to remove the flat earth phase in ATI-SAR ocean surface motion detection in this study. First, two conventional flat earth effect removal methods(i.e., the frequency shift method and the orbital parameter method) are introduced and compared. Then, two improvements to frequency shift method are suggested. In the first improvement, the phase diagram is divided into several sub-blocks to calculate the phase fringe frequency. In the second improvement, a function between the phase of land regions and position is fitted to correct the residual flat earth phase based on the phase of the land regions that tend toward zero in an along-track interferogram. It is found that the improved frequency shift method is greatly improved;and it agrees well with the orbital parameter method, and achieves similar accuracy. 展开更多
关键词 FLAT EARTH phase ATI-SAR frequency SHIFT orbitAL PARAMETER
在线阅读 下载PDF
Method for Collision Avoidance in Spacecraft Rendezvous Problems with Space Objects in a Phasing Orbit
16
作者 Danhe Chen A.A.Baranov +2 位作者 Chuangge Wang M.O.Karatunov N.Yu.Makarov 《Computer Modeling in Engineering & Sciences》 SCIE EI 2021年第6期977-991,共15页
As the number of space objects(SO)increases,collision avoidance problem in the rendezvous tasks or reconstellation of satellites with SO has been paid more attention,and the dangerous area of a possible collision shou... As the number of space objects(SO)increases,collision avoidance problem in the rendezvous tasks or reconstellation of satellites with SO has been paid more attention,and the dangerous area of a possible collision should be derived.In this paper,a maneuvering method is proposed for avoiding collision with a space debris object in the phasing orbit of the initial optimal solution.Accordingly,based on the plane of eccentricity vector components,relevant dangerous area which is bounded by two parallel lines is formulated.The axises of eccentricity vector system pass through the end of eccentricity vector of phasing orbit in the optimal solution,and orientation of axis depends on the latitude argument where a collision will occur.The dangerous area is represented especially with the graphical dialogue,and it allows to find a compromise between the SO avoiding and the fuel consumption reduction.The proposed method to solve the collision avoidance problem provides simplicity to calculate rendezvous maneuvers,and possibility to avoid collisions from several collisions or from“slow”collisions in a phasing orbit,when the protected spacecraft and the object fly dangerously close to each other for a long period. 展开更多
关键词 SPACECRAFT collision avoidance rendezvous problem space objects phasing orbit
在线阅读 下载PDF
Topological phase in one-dimensional Rashba wire
17
作者 汪萨克 汪军 刘军丰 《Chinese Physics B》 SCIE EI CAS CSCD 2016年第7期393-400,共8页
We study the possible topological phase in a one-dimensional(1D) quantum wire with an oscillating Rashba spin–orbital coupling in real space. It is shown that there are a pair of particle–hole symmetric gaps formi... We study the possible topological phase in a one-dimensional(1D) quantum wire with an oscillating Rashba spin–orbital coupling in real space. It is shown that there are a pair of particle–hole symmetric gaps forming in the bulk energy band and fractional boundary states residing in the gap when the system has an inversion symmetry. These states are topologically nontrivial and can be characterized by a quantized Berry phase ±π or nonzero Chern number through dimensional extension. When the Rashba spin–orbital coupling varies slowly with time, the system can pump out 2 charges in a pumping cycle because of the spin flip effect. This quantized pumping is protected by topology and is robust against moderate disorders as long as the disorder strength does not exceed the opened energy gap. 展开更多
关键词 one-dimensional topological phase Rashba spin–orbit interaction spatial modulation quantized pump
原文传递
Ground state of rotating ultracold quantum gases with anisotropic spin orbit coupling and concentrically coupled annular potential
18
作者 王鑫 谭仁兵 +3 位作者 杜志静 赵文宇 张晓斐 张首刚 《Chinese Physics B》 SCIE EI CAS CSCD 2014年第7期288-292,共5页
MotiVated by recent experimental realization of synthetic spin-orbit coupling in neutral quantum gases, we consider the quasi-two-dimensional rotating two-component Bose-Einstein condensates with anisotropic Rashba sp... MotiVated by recent experimental realization of synthetic spin-orbit coupling in neutral quantum gases, we consider the quasi-two-dimensional rotating two-component Bose-Einstein condensates with anisotropic Rashba spin-orbit cou- pling subject to concentrically coupled annular potential. For experimentally feasible parameters, the rotating condensate exhibits a variety of rich ground state structures by varying the strengths of the spin-orbit coupling and rotational frequency. Moreover, the phase transitions between different ground state phases induced by the anisotropic spin-orbit coupling are obviously different from the isotropic one. 展开更多
关键词 Bose-Einstein condensate spin-orbit coupling quantum phase transition
原文传递
航天器用机械泵驱动两相流体回路在轨测试性能分析 被引量:1
19
作者 孟庆亮 韦广朗 +3 位作者 于峰 杨涛 赵振明 朱许 《中国空间科学技术(中英文)》 北大核心 2025年第4期70-78,共9页
机械泵驱动两相流体回路(Mechanically Pumped Two-phase Loop,MPTL)是通过流动沸腾过程中气液相变潜热的释放而具有极强传热能力的两相传热装置,其在航天器热控领域具有广泛的研究前景。为研究MPTL产品的在轨微重力环境下的工作性能和... 机械泵驱动两相流体回路(Mechanically Pumped Two-phase Loop,MPTL)是通过流动沸腾过程中气液相变潜热的释放而具有极强传热能力的两相传热装置,其在航天器热控领域具有广泛的研究前景。为研究MPTL产品的在轨微重力环境下的工作性能和稳定性,设计并研制了一套包含屏蔽式离心泵、两相控温型储液器和微小流道蒸发器的MPTL,并在某卫星上对其启动特性、相变传热特性、控温特性进行了测试。测试结果表明,微重力下MPTL展现了良好的传热特性。微重力下两相控温型储液器的控温性能达到±0.1K精度,被动冷却功能得到验证,降温速率达到1℃/min。微泵运转时,储液器气相和液相两个测点形成的温差在0.3~1.0K区间内。两个转速下,蒸发器的控温精度在±0.1~±0.3K区间内。回路发生相变过程时会出现过热现象,并导致蒸发器出口测温点温度高于储液器控温点7~8K。通过对比两个转速下的结果,发现过热时间和过热温度与转速相关。采用毛细结构的两相控温型储液器可以有效保证微重力下MPTL的高精度控温和高效两相流管控功能,气液两相转变特性与回路流量大小相关,蒸发器温度稳定性与其内部流体干度大小相关。 展开更多
关键词 航天器热控 机械泵驱动两相流体回路(MPTL) 在轨测试 对流换热 微重力
在线阅读 下载PDF
Orbital magnetization in semiconductors
20
作者 方诚 王志刚 +1 位作者 李树深 张平 《Chinese Physics B》 SCIE EI CAS CSCD 2009年第12期5431-5436,共6页
This paper theoretically investigates the orbital magnetization of electron-doped (n-type) semiconductor het-erostructures and of hole-doped (p-type) bulk semiconductors, which are respectively described by a two-... This paper theoretically investigates the orbital magnetization of electron-doped (n-type) semiconductor het-erostructures and of hole-doped (p-type) bulk semiconductors, which are respectively described by a two-dimensional electron/hole Hamiltonian with both the included Rashba spin-orbit coupling and Zeeman splitting terms. It is the Zeeman splitting, rather than the Rashba spin-orbit coupling, that destroys the time-reversal symmetry of the semiconductor systems and results in nontrivial orbital magnetization. The results show that the magnitude of the orbital magnetization per hole and the Hall conductance in the p-type bulk semiconductors are about 10^-2-10^-1 effective Bohr magneton and 10^-1-1 e^2/h, respectively. However, the orbital magnetization per electron and the Hall conductance in the n-type semiconductor heterostructures are too small to be easily observed in experiment. 展开更多
关键词 orbital magnetization Zeeman splitting Berry phase effect SEMICONDUCTOR
原文传递
上一页 1 2 20 下一页 到第
使用帮助 返回顶部