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CAS IR Grid
机构
长春光学精密机械与物... [4]
宁波材料技术与工程研... [2]
兰州化学物理研究所 [2]
金属研究所 [1]
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OAI收割 [9]
内容类型
期刊论文 [6]
会议论文 [3]
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2019 [1]
2018 [2]
2017 [2]
2012 [1]
2010 [2]
2009 [1]
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学科主题
Materials ... [2]
Physics [2]
Science & ... [2]
材料科学与物理化学 [2]
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The research about servo control of 6-DOF workbench based on vacuum environment
期刊论文
OAI收割
Basic & Clinical Pharmacology & Toxicology, 2019, 卷号: 125, 页码: 20-20
作者:
H.Z.Yu
;
Y.Y.Sun
;
G.Wang
;
W.J.Chang
;
L.X.Zhao
  |  
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2020/08/24
Vacuum environment,Servo control,Workbench,Six degrees of freedom,Pharmacology & Pharmacy,Toxicology
Multi-phase carbonaceous coating with super wear resistance
期刊论文
OAI收割
VACUUM, 2018, 卷号: 157, 页码: 442-446
作者:
Wang, Yongxin
;
Shang, Lunlin
;
Zhang, Guangan
;
Zeng, Zhixiang
;
Wang, Liping
  |  
收藏
  |  
浏览/下载:50/0
  |  
提交时间:2018/12/04
Ultra-low Friction
Amorphous-carbon
Films
Fullerene
Behavior
Environment
Mechanism
Fluorine
Dynamics
Vacuum
Multi-phase carbonaceous coating with super wear resistance
期刊论文
OAI收割
VACUUM, 2018, 卷号: 157, 页码: 442-446
作者:
Xue, Qunji
;
Wang, Yongxin
;
Shang, Lunlin
  |  
收藏
  |  
浏览/下载:45/0
  |  
提交时间:2018/12/04
Ultra-low Friction
Amorphous-carbon
Films
Fullerene
Behavior
Environment
Mechanism
Fluorine
Dynamics
Vacuum
制备温度对聚酰亚胺薄膜真空摩擦学性能的影响
期刊论文
OAI收割
化工新型材料, 2017, 卷号: 45, 期号: 5, 页码: 103-105
作者:
刘百幸
;
史晓辉
;
尹建军
;
彭振军
;
梁军
  |  
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2018/01/02
聚酰亚胺
真空环境
制备温度
摩擦磨损性能
Polymide
Vacuum Environment
Preparation Temperature
Friction And Wear Property
润滑材料的空间环境效应
期刊论文
OAI收割
中国材料进展, 2017, 卷号: 36, 期号: 7-8, 页码: 481-491
作者:
高晓明
;
胡明
;
孙嘉奕
;
翁立军
  |  
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2017/11/19
空间环境
真空
热循环
原子氧
润滑材料
Space Environment
Vacuum
Thermal Cycle
Atomic Oxygen
Lubricants
Design and experimental research of a new type focus mechanism used in space-based telescope (EI CONFERENCE)
会议论文
OAI收割
2012 9th IEEE International Conference on Mechatronics and Automation, ICMA 2012, August 5, 2012 - August 8, 2012, Chengdu, China
作者:
Wang D.
收藏
  |  
浏览/下载:40/0
  |  
提交时间:2013/03/25
The position of focal plane will be changed because of temperature fluctuation and vacuum environment. In order to make the telescope work well
positioning accuracy of the mechanism is 0.008mm. The performance satisfies the need of precision
a focusing mechanism is needed. To majority of large space-based telescopes
and the scheme design is reasonable and practicable. 2012 IEEE.
the general way to do this would be to use a reflector
which was located in the backfocal distance. One of typical schemes of this mechanism was introduced
however
because of the big axial size
the mechanism can't be used when the size of the enclosure was limited. A new type of focusing mechanism was introduced
which has such advantages of small size
high accuracy and low mass. The design and test methods had been discussed. According to the results
the repeatability positioning accuracy is 0.0025mm
Inspection focus technology of space tridimensional mapping camera based on astigmatic method (EI CONFERENCE)
会议论文
OAI收割
5th International Symposium on Advanced Optical Manufacturing and Testing Technologies: Optoelectronic Materials and Devices for Detector, Imager, Display, and Energy Conversion Technology, April 26, 2010 - April 29, 2010, Dalian, China
作者:
Wang Z.
;
Wang Z.
;
Zhang L.
;
Zhang L.
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2013/03/25
The CCD plane of the space tridimensional mapping camera will be deviated from the focal plane(including the CCD plane deviated due to camera focal length changed)
under the condition of space environment and vibration
impact when satellite is launching
image resolution ratio will be descended because defocusing. For tridimensional mapping camera
principal point position and focal length variation of the camera affect positioning accuracy of ground target
conventional solution is under the condition of vacuum and focusing range
calibrate the position of CCD plane with code of photoelectric encoder
when the camera defocusing in orbit
the magnitude and direction of defocusing amount are obtained by photoelectric encoder
then the focusing mechanism driven by step motor to compensate defocusing amount of the CCD plane. For tridimensional mapping camera
under the condition of space environment and vibration
impact when satellite is launching
if the camera focal length changes
above focusing method has been meaningless. Thus
the measuring and focusing method was put forward based on astigmation
a quadrant detector was adopted to measure the astigmation caused by the deviation of the CCD plane
refer to calibrated relation between the CCD plane poison and the asrigmation
the deviation vector of the CCD plane can be obtained. This method includes all factors caused deviation of the CCD plane
experimental results show that the focusing resolution of mapping camera focusing mechanism based on astigmatic method can reach 0.25 m. 2010 Copyright SPIE - The International Society for Optical Engineering.
Design and test of focusing mechanism of space camera (EI CONFERENCE)
会议论文
OAI收割
5th International Symposium on Advanced Optical Manufacturing and Testing Technologies: Design, Manufacturing, and Testing of Micro- and Nano-Optical Devices and Systems, April 26, 2010 - April 29, 2010, Dalian, China
作者:
Li Y.
;
Li Y.
;
Li Y.
;
Wang H.
;
Wang H.
收藏
  |  
浏览/下载:33/0
  |  
提交时间:2013/03/25
According to the focal depth and work environment of a space camera
a focusing mechanism is designed
which consists of precision screw ball transmission and linear bearing guidance and accuracy improving. The dynamic- strike- resistance
adaptability to temperature and vacuum are considered into the reliable design method. Furthermore
the linearity error
the structure stability and the mechanism work situation in high and low temperature are tested. The result is that the linearity error of the mechanism is less than 0.003 mm
and the sway error of vertical way and level way of the mirror is less than 20''. The linearity error of the mechanism and the sway error of the mirror remain unchanged after vibration test. The mechanism can work in the complex space environment. 2010 SPIE.
A polysilazane coating protecting polyimide from atomic oxygen and vacuum ultraviolet radiation erosion
期刊论文
OAI收割
Surface & Coatings Technology, 2009, 卷号: 203, 期号: 22, 页码: 3338-3343
L. F. Hu
;
M. S. Li
;
C. H. Xu
;
Y. M. Luo
;
Y. C. Zhou
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2012/04/13
Polysilazane
Low earth orbit
Atomic oxygen
Vacuum ultraviolet
radiation
low-earth-orbit
high-flux source
polymers
environment
spectroscopy
plasma
beam