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	A Rapid Nondestructive Inspection Method Applied to EAST Lower Divertor by Infrared Thermography 期刊论文 OAI收割 IEEE TRANSACTIONS ON PLASMA SCIENCE, 2018, 卷号: 46, 期号: 5, 页码: 1366-1371 作者: Liu, Yanwei; Xu, Tiejun; Han, Le; Li, Lei; Yao, Damao \| 收藏 \| 浏览/下载：31/0 \| 提交时间：2019/06/04 Assembly quality experimental advanced super-conducting tokamak (EAST) device finite-element analysis (FEA) infrared (IR) thermography lower divertor
	1m红外太阳望远镜镜面位置误差致光轴偏移分析期刊论文 OAI收割红外技术(Infrared Technology), 2016, 卷号: 38, 期号: 10, 页码: 870-876 作者: 董雪岩; 许方宇; 陈骥; 罗永芳收藏 \| 浏览/下载：56/0 \| 提交时间：2017/01/12 红外望远镜(infrared telescope) 光学装调(optical system assembly and alignment) 光轴偏移(optic axis deviation) 像质(image quality) 弯沉(deflection) 灵敏度矩阵(sensitivity matrix)
	Manufacture of 1.2m reaction bonded silicon carbide mirror blank CFID (EI CONFERENCE) 会议论文 OAI收割 5th International Symposium on Advanced Optical Manufacturing and Testing Technologies: Large Mirrors and Telescopes, April 26, 2010 - April 29, 2010, Dalian, China 作者: Zhang G.; Zhang G.; Zhang G. 收藏 \| 浏览/下载：30/0 \| 提交时间：2013/03/25 Silicon carbide (SiC) is a new type candidate material for large-scale lightweight space mirror. Its low thermal distortion high stiffness fine optical quality and dimensional stability make SiC an ideal material for large space born telescope. Since ten years Changchun institute optics fine mechanics and physics (CIOMP) has developed reaction bonded SiC (RB-SiC) technology for space application and can fabricate RB-SiC mirror with scale less than 1.0 meter for telescope. The green body is prepared with gel-casting method which is an attractive new ceramic forming process for making high-quality complex-shaped ceramic parts. And then unmolding drying binder burning out reacting bonded the RB-SiC can be obtained. But with the development of space-born or ground telescope the scale of primary mirror has exceeded 1.0 meter. So CIOMP has developed an assembly technique which called novel reaction-formed joint technology for larger RB-SiC mirror blank. The steps include joining of green bodies with mixture comprised of SiC particles and phenolic resin etc firing machining and sintering. Joining the 1.2 meter RB-SiC mirror blank by the novel reaction-formed joint technology. And testing the welding layer's performance the results show that the thickness of 54-77m the microstructure and thermal property can be comparable to the substrate and the mechanical property are excellent in bending strength of 307MPa. 2010 Copyright SPIE - The International Society for Optical Engineering.
	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.
	The structure design and packaging of the polarization-maintaining dual fiber collimator based on DFT (EI CONFERENCE) 会议论文 OAI收割 2005 Conference on High Density Microsystem Design and Packaging and Component Failure Analysis, HDP'05, June 27, 2005 - June 29, 2005, Shanghai, China 作者: Wang Z.; Qiu J.; Wang Z. 收藏 \| 浏览/下载：24/0 \| 提交时间：2013/03/25 Examinable characteristic is an important parameter to measure and ensure the function and quality of the products. Based on the idea of DFA/M(Design For Assembly/Design For Manufacturability) and the method whether the target for low insertion loss and high reflection loss is implemented the rational structure and assembly technics for the polarization-maintaining dual fiber collimator are discussed and the packaging technology based on DFT of the polarization-maintaining dual fiber collimator is proposed. This method has been utilized in batch manufacture to enhance the efficiency and ensure the eligible ratio.
	Mechanical interleaving assembly of TDICCD focal plane for space camera (EI CONFERENCE) 会议论文 OAI收割 ICO20: Optical Devices and Instruments, August 21, 2005 - August 26, 2005, Changchun, China 作者: Ren J.-Y.; Zhang X.-X. 收藏 \| 浏览/下载：25/0 \| 提交时间：2013/03/25 TDICCD assembly is a major method of acquiring wide field for space camera. For the demand of space camera's wide view field and high resolution the technique of mechanical interleaving assembly is discussed. Its principle method of adjusting and testing as well as the structure of focal plane are described. Using mechanical tangent-screws adjusting method the assembly with TDI CCDs for wide field space camera focal plane is finished on the facility which is composed of a long work-distance microscope and a negative pressure and adsorption guide apparatus. The assembly length of TDICCD focal plane for wide field space camera reaches 560mm and the measuring error is not more than 3.2 m the mechanical interleaving assembly method has effect of zero clearance and can achieve good image quality.