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	Preliminary Design of Pulse Inductor Applied for 100-kA Quench Protection System 期刊论文 OAI收割 IEEE TRANSACTIONS ON PLASMA SCIENCE, 2020, 卷号: 48 作者: Tong, Wei; Li, Chuan; Song, Zhiquan; Fu, Peng; Qian, Chengjin \| 收藏 \| 浏览/下载：140/0 \| 提交时间：2020/10/26 Inductors Superconducting magnets Magnetomechanical effects Inductance Stress Reliability Strain Finite-element method (FEM) pulse inductor quench protection
	双极器件LPNP辐照损伤效应的并行有限元数值模拟期刊论文 OAI收割系统仿真学报, 2020, 卷号: 32, 期号: 12, 页码: 2376-2382 作者: 王芹; 马召灿; 李鸿亮; 张林波; 卢本卓 \| 收藏 \| 浏览/下载：24/0 \| 提交时间：2021/04/26 Zlamal finite element radiation damage effects LPNP BJT parallel simulation Zlamal有限元辐照损伤效应 LPNP晶体管并行数值模拟
	Influence of low temperature on the surface deformation of deformable mirrors 期刊论文 OAI收割 Chinese Physics B, 2017, 卷号: 26, 期号: 5, 页码: 054215 作者: You, Juncheng; Guan, Chunlin; Zhou, Hong \| 收藏 \| 浏览/下载：25/0 \| 提交时间：2018/11/20 Actuators - Adaptive optics - Delta modulation - Finite element method - Laser pulses - Mirrors - Optical testing - Piezoelectric actuators - Temperature - Testing - Thermal effects - Thermal expansion
	Strain-rate-dependent microplane model for high-rate comminution of concrete under impact based on kinetic energy release theory 期刊论文 OAI收割 PROCEEDINGS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2015, 卷号: 471, 期号: 2182, 页码: 20150535 作者: Kirane K; Su YW(苏业旺); Bazant ZP 收藏 \| 浏览/下载：45/0 \| 提交时间：2016/01/07 projectile impact dynamic overstress strain-rate effects material fragmentation finite-element simulation crack band model
	Micro-electro-mechanical systems capacitive ultrasonic transducer with a higher electromechanical coupling coefficient 期刊论文 OAI收割 Micro & Nano Letters, 2015, 卷号: 10, 期号: 10, 页码: 4 作者: Miao, J(苗静); Shen, WJ(沈文江); He, CD; Xue, CY; Xiong, JJ 收藏 \| 浏览/下载：88/0 \| 提交时间：2015/12/31 silicon elemental semiconductors silicon-on-insulator wafer bonding electromechanical effects ultrasonic transducers capacitive transducers micromechanical devices micromachining vibrations membranes finite element analysis reliability capacitance electromechanical coupling coefficient capacitive micromachined ultrasonic transducer impedance matching propagation medium microelectromechanical system capacitive ultrasonic transducer silicon on insulator wafer bonding optimum geometric dimensions membrane mechanical vibration electrical characteristics finite-element analysis operation mode device safety device reliability equivalent stress operation-collapse voltage bottom electrodes glass substrate surface parallel parasitic capacitance Si SiO2
	Fabrication of an oxidation-resistant beta-NiAl coating on gamma-TiAl 期刊论文 OAI收割 Surface & Coatings Technology, 2012, 卷号: 206, 期号: 8-9, 页码: 2454-2458 H. Zhang; X. Peng; F. Wang 收藏 \| 浏览/下载：25/0 \| 提交时间：2013/02/05 Electrophoretic deposition Hot pressing Coating Oxidation Reactive element effects electrophoretic deposition aluminide coatings reactive elements alloy intermetallics additions behavior compound scale air
	Design of motion compensation mechanism of satellite remote sensing camera (EI CONFERENCE) 会议论文 OAI收割 International Symposium on Photoelectronic Detection and Imaging 2011: Space Exploration Technologies and Applications, May 24, 2011 - May 26, 2011, Beijing, China Gu S.; Yan Y.; Xu K.; Jin G. 收藏 \| 浏览/下载：47/0 \| 提交时间：2013/03/25 With the development of aerospace remote sensing technology the ground resolution of remote sensing camera enhances continuously. Since there is relative motion between camera and ground target when taking pictures the target image recorded in recording media is moved and blurred. In order to enhance the imaging quality and resolution of the camera the image motion had to be compensated. In order to abate the effect of image motion to image quality of space camera and improve the resolution of the camera the compensation method of image motion to space camera is researched. First the reason of producing drift angle and adjustment principle are analyzed in this paper. This paper introduce the composition and transmission principle of image motion compensation mechanism. Second the system adopts 80C31 as controller of drift angle and adopts stepping motor for actuators and adopts absolute photoelectric encoder as the drift Angle measuring element. Then the control mathematical model of the image motion compensation mechanism are deduced and it achieve the closed-loop control of the drift angle position. At the last this paper analyses the transmission precision of the mechanism. Through the experiment we measured the actual precision of the image motion compensation mechanism and compared with the theoretical analysis. There are two major contributions in this paper. First the traditional image motion compensation mechanism is big volume and quality heavy. This has not fit for the development trend of space camera miniaturization and lightweight. But if reduce the volume and quality of mechanism it will bring adverse effects for the precision and stiffness of mechanism. For this problem This paper designed a image motion compensation that have some advantages such as small size light weight at the same time high precision stiffness and so on. This image motion compensation can be applicable to the small optics cameras with high resolution. Second the traditional mechanism control need to corrected fitting and iterative for the control formula of mechanism. Only in this way we can get the optimal control mathematical model. This paper has high precision of the control formula derived. It can achieve the high precision control without fitting It also simplify the difficulty of control mathematical model establishment. This paper designed the range of adjusting of image motion compensation mechanism between -5 +5. Based on choosing-5 -4 -3 -2 -1 0 +1 +2 +3 +4 +4 as the expectation value of the imaginary drift angle we get ten groups of the fact data in adjusting drift angle measured. The test results show that the precision of the drift angle control system can be achieved in 1. It can meet the system requirements that the precision of the control system is less than 3' and it can achieve the high-precision image motion compensation. 2011 SPIE.
	The atomic structure and the properties of Ununbium (Z=112) and Mercury (Z=80) 期刊论文 OAI收割 SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY, 2007, 卷号: 50, 页码: 707-715 作者: Li JiGuang; Dong ChenZhong; Yu YouJun; Ding XiaoBin; Fritzsche, S. \| 收藏 \| 浏览/下载：20/0 \| 提交时间：2018/07/16 super heavy element atomic structure relativistic effects electron correlation effects MCDF method
	Design and analysis of large spaceborne light-weighted primary mirror and its support system (EI CONFERENCE) 会议论文 OAI收割 3rd International Symposium on Advanced Optical Manufacturing and Testing Technologies, AOMATT 2007: Large Mirrors and Telescopes, July 8, 2007 - July 12, 2007, Chengdu, China Yan Y.; Jin G.; Yang H.-B. 收藏 \| 浏览/下载：17/0 \| 提交时间：2013/03/25 With the development of the resolution of spaceborne remote sensor the diameter of the primary mirror of spaceborne telescope becomes larger and larger. The distortion of primary mirror which is influenced by the mirror material structure self-weight support system and temperature environment affects optical image quality finally. In this paper an on-axis TMA high-resolution Cassegrain optical payload with a primary mirror whose diameter is 650mm was designed and the effects of the influence factors of the distortion acts on the on-axis TMA optical system primary mirror had been analyzed by means of Finite Element Analysis. During work the technology of the primary mirror design had been summarized and general consideration of the primary mirror design technology also had been described at the same time. Considering the telescope manufacture and work station a reasonable and optimal structure of the primary mirror sub-assembly is taken finally. In the end the distortion of the primary mirror during its fabrication station and work station had been analyzed by integrated Finite Element Analysis Method. The results implicated the synthesis profile error (P-V value) for the primary mirror is less than /10 and all the indexes of the primary mirror satisfy the requirements of the optical system.