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	Load-bearing behaviors of the composite gravity-type anchorage: Insights from physical model and numerical tests 期刊论文 OAI收割 ENGINEERING FAILURE ANALYSIS, 2025, 卷号: 167, 页码: 21 作者: Wang, Chengtang; Han, Hongju; Wang, Hao; Zhang, Xiuli; Liu, Xinhua \| 收藏 \| 浏览/下载：15/0 \| 提交时间：2025/06/27 Composite gravity-type anchorage Load-bearing performance Failure process Load sharing ratio Model tests Numerical simulations
	Design of Coordination System for Composite Mobile Robot Platform Oriented to Nuclear Fusion Vessel 期刊论文 OAI收割 JOURNAL OF FUSION ENERGY, 2021, 卷号: 40 作者: Zhang, Qiang; Song, Bo; Cai, Bin; Sun, Yuxiang \| 收藏 \| 浏览/下载：99/0 \| 提交时间：2021/11/15 EAST nuclear fusion reactor vessel Multi-joint remote control system Composite multi-joint remote operation robot platform Bidirectional coordinated control Load-bearing performance test
	Enhancing anti-corrosion and antifouling properties of Cu/GLC composite film for marine application 期刊论文 OAI收割 SURFACE & COATINGS TECHNOLOGY, 2019, 卷号: 375, 页码: 414-426 作者: Zhang, Jingwen; Zhou, Shengguo; Wang, Yongxin; Wang, Yuecheng; Wang, Chunting \| 收藏 \| 浏览/下载：66/0 \| 提交时间：2019/12/18 DIAMOND-LIKE CARBON LOAD-BEARING CAPACITY CORROSION-RESISTANCE TRIBOLOGICAL PERFORMANCE MECHANICAL-PROPERTIES STAINLESS-STEEL THIN-FILMS DLC FILMS COATINGS WEAR
	Lightweight design and analysis of support structure of certain UAV engine (EI CONFERENCE) 会议论文 OAI收割 2012 International Conference on Electrical Insulating Materials and Electrical Engineering, EIMEE 2012, May 25, 2012 - May 27, 2012, Shenyang, Liaoning, China Xing X.; Liu B.; Han X.; Jia H. 收藏 \| 浏览/下载：38/0 \| 提交时间：2013/03/25 Support structure of UAV (Unmanned Aerial Vehicle) engine is the important support for UAV engine playing a support role and bearing extremely complex load so its lightweight strength and dynamic characteristics have a great influence on high performance of UAV. This paper focuses on UAV having the requirement of high performance and stability to the support structure of engine and uses the software of MSC.Patran and MSC.Nastran and topology optimization criterion to lightweight design and analysis the support structure of UAV engine under the premise condition of existing constraints. Then the static strength and modal are analyzed for the result of lightweight design and the strength of the model and dynamic characteristics are verified. (2012) Trans Tech Publications Switzerland.
	Study on the azimuth bearing scheme of a large Alt-azimuth telescope (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: Wang H.; Dai S.; Zhang J.; Wang H.; Zhang J. 收藏 \| 浏览/下载：49/0 \| 提交时间：2013/03/25 The azimuth bearing schemes in typical large Alt-azimuth telescopes especially the 3.5-m APO telescope and the 4.1-m SOAR telescope were analyzed. A scheme of high-angular contacted thrust ball bearing integrated with a radial ball bearing was put forward. According to the Hertz contact theory the corresponding parameters were designed for engineering application. The static performance parameters within the range of 60 85 original contact angle were calculated. Compared with the traditional plane thrust ball bearing the results shows that the high-angular (80) contact thrust ball bearing has more benefits at bearing strength and rigidity for large telescope. The 1500mm diameter prototyping bearing shows good performance including the axial jitter is 0.009mm the radial jitter is 0.006mm the maximum starting torque without load is 30N·m and the load capacity is more than 30t which offers advanced technique path for the buildup of the high precision azimuth shafting and the whole telescope system. 2010 Copyright SPIE - The International Society for Optical Engineering.