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长春光学精密机械与物... [9]
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会议论文 [5]
期刊论文 [4]
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2016 [2]
2014 [2]
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2009 [1]
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专题:长春光学精密机械与物理研究所
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Thermal barrier effect analysis of magnesium-fluoride conformal dome and the experimental validation
期刊论文
Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering, 2016, 卷号: 45, 期号: 2
作者:
Zhang, T.
;
Q. Wei
;
C. Wang
;
L. Yu and R. Zhu
收藏
  |  
浏览/下载:15/0
  |  
提交时间:2017/09/11
Technology of large aperture off-axis parabolic mirror with tri-station processing center
期刊论文
Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering, 2016, 卷号: 45, 期号: 8
作者:
Zhang, X.
;
X. Luo
;
L. Yan
;
F. Zhang and X. Zhang
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  |  
浏览/下载:19/0
  |  
提交时间:2017/09/11
Thermal analysis of large telescope structure
期刊论文
Guangzi Xuebao/Acta Photonica Sinica, 2014, 卷号: 43, 期号: 4
Zhou C.
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  |  
浏览/下载:13/0
  |  
提交时间:2015/04/24
Thermal noise analysis and correction of infrared conformal dome
期刊论文
Guangxue Xuebao/Acta Optica Sinica, 2014, 卷号: 34, 期号: 10
Wang C.
;
Chen J.
;
Wei Q.
;
Jia H.
;
Yu L.
;
Zhang T.
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  |  
浏览/下载:12/0
  |  
提交时间:2015/04/24
Thermal-structure Analysis of Supersonic Dome for Mounting
会议论文
魏群
;
贾宏光
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  |  
浏览/下载:7/0
  |  
提交时间:2012/05/12
Thermal-structure analysis of supersonic dome based on three materials
会议论文
艾兴乔
;
魏群
;
刘波
;
贾宏光
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  |  
浏览/下载:15/0
  |  
提交时间:2012/05/12
Thermal analysis on supersonic ellipsoidal dome (EI CONFERENCE)
会议论文
2nd International Conference on Multimedia Technology, ICMT 2011, July 26, 2011 - July 28, 2011, Hangzhou, China
Jiang Z.
;
Wei Q.
;
Jia H.
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  |  
浏览/下载:20/0
  |  
提交时间:2013/03/25
Studied the transient thermal transfer analysis method due to a kind of supersonic ellipsoidal dome
which is a conformal dome. Illuminated the principle of transient thermal transfer analysis. Accomplished the transient thermal analysis based on the model of ellipsoidal dome
and studied the influence about the different material and the different velocity. Considered three materials consist of MgF2
Al2O3
and ZnS
and meanwhile
the velocity was Mach2.5
and the time consists of 10s
20s and 60s. The temperature initial loads were from FLUENT thermal simulation. The thermal conduction analysis and the thermal convection analysis were finished in software ANSYS
in which the entire transient thermal analysis consists of modeling
meshing element
calculating and getting the results. The different temperature distributions based on varied time were gotten about the different materials. The results from analysis showed the temperature distribution of the structure of ellipsoidal dome
which could help the following coupled thermal-structure analysis. 2011 IEEE.
Thermal-structure analysis of supersonic dome based on three materials (EI CONFERENCE)
会议论文
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Jiang Z.
;
Ai X.
;
Wei Q.
;
Liu B.
;
Jia H.
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  |  
浏览/下载:17/0
  |  
提交时间:2013/03/25
To a supersonic missile
a seeker could enhance the aerodynamic ability due to decrease the resistance in flying. At the same time
the primary function of a seeker has been considered as the most important equipment for a missile
due to the importance for cueing of targets and tracking for the final approach. However
the dome of a seeker
which is made up of glass
has poor mechanical performance. Especially
in the higher altitude
for a dome
in which the aerothermal and pressure loads could destroy the structure easily
it is necessary to do the thermal-structure coupled analysis due to varied materials. In the paper
to take the spherical dome of a seeker as a example
the analysis has been completed according to the varied materials consist of MgF2
Al2O3 and ZnS. The temperature loads and the pressure loads derived from the results of fluent analysis has been forced on the surface of dome
which simulates the actual Mach 2.5 in flying. According to the results of coupled analysis
the SEQV stress of the dome radium 80mm based on three materials had reached to 31MPa
which shows that the strength is sufficient for Mach 2.5
and offered the warranty to design the attaching to missile for the dome. At the same time
the results required the flexible mounting for the dome due to the displacements results
which the crystal material couldn't accept. 2011 IEEE.
Dome design and coupled thermal-mechanical analysis of supersonic missile (EI CONFERENCE)
会议论文
2009 International Conference on Optical Instruments and Technology, OIT 2009, October 19, 2009 - October 22, 2009, Shanghai, China
Xing-qiao A.
;
Qun W.
;
Hong-guang J.
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  |  
浏览/下载:40/0
  |  
提交时间:2013/03/25
A review of high-speed flow pressure and aerodynamic heating effect on Supersonic missile's dome is given. The dome should have excellent properties in optical
mechanical and chemical characteristics. A design of dome on supersonic mode is described according to tactical guide line of a missile. The dome made of quartz which is about 8mm thick and 141mm in window diameter. To check up the reliability of the dome
a reasonable finite element model (FEM) of dome is established
and a thermal-mechanical Analysis to the dome by finite element software NASTRAN has carried on
through these can obtained the distribution of temperature field and stress field when the speed is 2.3Ma. The results indicated that the stress was concentrated in the joint of the dome end and the Missile Section
and the maximum stress was 16.4Mpa. The stress of other nodes was smaller than the allowable stress of quartz glass. Reference to the results of the analysis
a lightweight revision to the dome structural dimension and a new method of dome fixing have put forward
which can reduce the stress concentration. 2009 SPIE.
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