CFETR integration design platform: Development of space analysis module

doi:10.1016/j.fusengdes.2018.06.013

CORC > 合肥物质科学研究院 > 中国科学院合肥物质科学研究院 > 中科院等离子体物理研究所

	CFETR integration design platform: Development of space analysis module
	Deng, J. S.2; Zhu, Z. Y.2; Li, Y.2; Wang, Z. W.1; Mao, S. F.2; Liu, X. F.1; Ye, M. Y.1,2
刊名	FUSION ENGINEERING AND DESIGN
	2018-09-01
卷号	134 页码:29-34
关键词	Integrated design Space analysis Deformation Fusion reactor CFETR
ISSN号	0920-3796
DOI	10.1016/j.fusengdes.2018.06.013
通讯作者	Mao, S. F.(sfmao@ustc.edu.cn)
英文摘要	Space allocation is important in the design of a fusion reactor, where numerous components operate under complex conditions, including a strong magnetic field, high-energy neutron irradiation, and a wide temperature range (4.5 K at the magnet and similar to 300-500 degrees C at the blanket). To ensure the consistency of the China Fusion Engineering Test Reactor (CFETR) design, multi-component interference checks and distance measurements must be routinely performed. In this paper, a space analysis module is developed on the CFETR Integration Design Platform to provide the space analysis function for both rigid and deformed components (using the Representative-Triangles method). The example of the space allocation of a vacuum vessel (VV) and a thermal shield (TS) is demonstrated. The deformation due to heating under the bake-out condition is considered (during operation, heating and swelling due to radiation also cause deformation). With the input from the component design module, the space analysis can be well-performed for both rigid models and thermal deformation results (under the simplified boundary condition). Through iteration between the component design modules and the space analysis module, a preliminary designed clearance of 40 mm between the VV and TS is insufficient owing to the deformation during bake out, and the optimized clearance increases by a factor of two.
资助项目	National Magnetic Confinement Fusion Science Program of China[2014GB110001] ; National Magnetic Confinement Fusion Science Program of China[2014GB110002] ; National Magnetic Confinement Fusion Science Program of China[2014GB110003]
WOS研究方向	Nuclear Science & Technology
语种	英语
出版者	ELSEVIER SCIENCE SA
WOS记录号	WOS:000444927900005
资助机构	National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China ; National Magnetic Confinement Fusion Science Program of China
内容类型	期刊论文
源URL	[http://ir.hfcas.ac.cn:8080/handle/334002/39099]
专题	合肥物质科学研究院_中科院等离子体物理研究所
通讯作者	Mao, S. F.
作者单位	1.Chinese Acad Sci, Inst Plasma Phys, Hefei 230031, Anhui, Peoples R China 2.Univ Sci & Technol China, Dept Engn & Appl Phys, Hefei 230026, Anhui, Peoples R China
推荐引用方式 GB/T 7714	Deng, J. S.,Zhu, Z. Y.,Li, Y.,et al. CFETR integration design platform: Development of space analysis module[J]. FUSION ENGINEERING AND DESIGN,2018,134:29-34.
APA	Deng, J. S..,Zhu, Z. Y..,Li, Y..,Wang, Z. W..,Mao, S. F..,...&Ye, M. Y..(2018).CFETR integration design platform: Development of space analysis module.FUSION ENGINEERING AND DESIGN,134,29-34.
MLA	Deng, J. S.,et al."CFETR integration design platform: Development of space analysis module".FUSION ENGINEERING AND DESIGN 134(2018):29-34.