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霍尔元件自激场的计算与分析
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作者 曲国福 《陕西工学院学报》 2001年第1期29-30,53,共3页
针对霍尔式传感器的核心敏感部件———霍尔元件在通入工作电流后其自身产生的磁场 (自激场 )的磁感应强度进行计算 。
关键词 霍尔元件 自激场 计算 磁感应强度 高斯汁 霍尔式传感器
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飞利浦彩显场自激的检修
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作者 蔡珂 《家电维修》 2002年第7期39-39,共1页
关键词 彩色显示器 故障 飞利浦牌 自激 检修
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电动蔗叶还田机刀辊部件的创新设计
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作者 唐艳芹 程思创 +1 位作者 方俊鑫 王玉兴 《农业装备与车辆工程》 2023年第9期21-25,共5页
为解决单刀辊电动蔗叶还田机中蔗叶易缠绕、易产生自激风场吹跑蔗叶导致切断不完全等问题,对还田机刀辊部件包括结构、尺寸、材料等进行创新优化设计。新刀辊设计有套筒,通过增大刀辊直径减小蔗叶缠绕概率,通过MATLAB多目标规划方法对... 为解决单刀辊电动蔗叶还田机中蔗叶易缠绕、易产生自激风场吹跑蔗叶导致切断不完全等问题,对还田机刀辊部件包括结构、尺寸、材料等进行创新优化设计。新刀辊设计有套筒,通过增大刀辊直径减小蔗叶缠绕概率,通过MATLAB多目标规划方法对刀辊的主要设计尺寸进行了优化,利用ANSYS Workbench对新刀辊的高速旋转工作状态进行模态分析。分析结果表明,新刀辊在工作状态下不会发生共振,能够满足农艺要求;在新刀辊的基础上创新提出了前、后双轴刀辊联动布置设计。新刀辊拥有刀具长度可调节、不易缠绕、使用灵活的特点;双刀辊联动设计中刀辊之间形成的自激风场相互抵消,同时能对蔗叶进行二次切割,有效减缓了蔗叶缠绕和切断不充分的问题,提升了还田机工作的可靠性和蔗叶还田的效率。 展开更多
关键词 还田机 缠绕 自激 刀辊 多目标规划 模态分析
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Gravitational Field Excitation from the First Term of Quantum Wilson Loop
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作者 SHAO Liang SHAO Dan +2 位作者 SHAO Chang-Gui H. Noda CHEN Yi-Han 《Communications in Theoretical Physics》 SCIE CAS CSCD 2006年第1X期77-86,共10页
In 4-dimensional R-gravity, using the linear and square terms of the expanding expression of the space-time connection, we calculate the possible curvature excitation (order k^4) of gravitational field, which is giv... In 4-dimensional R-gravity, using the linear and square terms of the expanding expression of the space-time connection, we calculate the possible curvature excitation (order k^4) of gravitational field, which is given by the first term of quantum Wilson loop (w) through two-point Green's function of the connection. At the same time using the tree diagram propagators of gravitons, the lowest order (k^4) correction to (w) is also calculated through the graviton self-energy in the term. Under the accuracy condition up to order k^4, we have obtained a complete expression of the excitation contributed from the leading term (w^(2))of (w). 展开更多
关键词 excitation of gravitational field graviton self-energy correction complete expression of excitation of order k^4 in (w^(2))
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Manipulation of Spontaneous Emission via Quantum Interference in an Elliptically Polarized Laser Field
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作者 丁春玲 李家华 +2 位作者 余荣 张多 杨晓雪 《Communications in Theoretical Physics》 SCIE CAS CSCD 2013年第5期603-614,共12页
Manipulation of spontaneous emission from an atom confined in three kinds of modified reservoirs has been investigated by means of an elliptically polarized laser field. Some interesting phenomena such as the multi-pe... Manipulation of spontaneous emission from an atom confined in three kinds of modified reservoirs has been investigated by means of an elliptically polarized laser field. Some interesting phenomena such as the multi-peak structure, extreme spectral narrowing, and cancellation of spontaneous emission can be observed by adjusting controllable system parameters. Moreover, these phenomena depend on the constructive or destructive quantum interference between multiple decay channels and which can be changed appreciably by varying the phase difference between the two circularly polarized components of the probe field. These results demonstrate the importance of an elliptially polarized laser field in controlling the spontaneous emission and its potential applications in high-precision spectroscopy. 展开更多
关键词 spontaneous emission elliptically polarized laser field quantum interference
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Unsteady Transonic Flow Control around an Airfoil in a Channel
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作者 Md.Abdul Hamid A.B.M.Toufique Hasan +3 位作者 Mohammad Ali Yuichi Mitsutake Toshiaki Setoguchi Shen Yu 《Journal of Thermal Science》 SCIE EI CAS CSCD 2016年第2期117-122,共6页
Transonic internal flow around an airfoil is associated with self-excited unsteady shock wave oscillation. This unsteady phenomenon generates buffet, high speed impulsive noise, non-synchronous vibration, high cycle f... Transonic internal flow around an airfoil is associated with self-excited unsteady shock wave oscillation. This unsteady phenomenon generates buffet, high speed impulsive noise, non-synchronous vibration, high cycle fatigue failure and so on. Present study investigates the effectiveness of perforated cavity to control this unsteady flow field. The cavity has been incorporated on the airfoil surface. The degree of perforation of the cavity is kept constant as 30%. However, the number of openings(perforation) at the cavity upper wall has been varied. Results showed that this passive control reduces the strength of shock wave compared to that of baseline airfoil. As a result, the intensity of shock wave/boundary layer interaction and the root mean square(RMS) of pressure oscillation around the airfoil have been reduced with the control method. 展开更多
关键词 transonic flow passive control shock wave oscillation
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