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Methods of configuration test and deformation analysis for large airship

Methods of configuration test and deformation analysis for large airship

作     者:ZHAI Yutao SHEN Yongzheng YAN Xiangbin TAN Huifeng ZHAI Yutao;SHEN Yongzheng;YAN Xiangbin;TAN Huifeng

作者机构:School of ManagementHarbin Institute of TechnologyHarbin 150001China State Key Laboratory of Special Environmental Composite Materials TechnologyHarbin Institute of TechnologyHarbin 150001China Beijing Institute of Telemetry TechnologyChina Aerospace Science and Technology CorporationBeijing 100071China 

出 版 物:《Journal of Systems Engineering and Electronics》 (系统工程与电子技术(英文版))

年 卷 期:2022年第33卷第4期

页      面:951-960页

核心收录:

学科分类:08[工学] 082503[工学-航空宇航制造工程] 0825[工学-航空宇航科学与技术] 

基  金:supported by the Foundation for Innovative Research Groups of the National Natural Science Foundation of China (11421091) 

主  题:large airship deformation analysis three-dimensional(3D)laser scanning technology non-uniform rational B-splines(NURBS) system engineering 

摘      要:In recent years, high-altitude aerostats have been increasingly developed in the direction of multi-functionality and large size. Due to the large size and the high flexibility, new challenges for large aerostats have appeared in the configuration test and the deformation analysis. The methods of the configuration test and the deformation analysis for large airship have been researched and discussed. A tested method of the configuration,named internal scanning, is established to quickly obtain the spatial information of all surfaces for the large airship by the three-dimensional(3D) laser scanning technology. By using the surface wrap method, the configuration parameters of the large airship are calculated. According to the test data of the configuration, the structural dimensions such as the distances between the characteristic sections are measured. The method of the deformation analysis for the airship contains the algorithm of nonuniform rational B-splines(NURBS) and the finite element(FE)method. The algorithm of NURBS is used to obtain the reconfiguration model of the large airship. The seams are considered and the seam areas are divided. The FE model of the middle part of the large airship is established. The distributions of the stress and the strain for the large airship are obtained by the FE method. The position of the larger deformation for the airship is found.

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