{"title":"复杂曲面飞机骨架模型自动建模系统","authors":"Dangdang Zheng, Bing Han, Geng Liu, R. Tong","doi":"10.1109/ICCCS49078.2020.9118536","DOIUrl":null,"url":null,"abstract":"There are complex and repeated modeling works during the process of aircraft design, which leads to the heavy workload and low working efficiency. In order to improve the quality and efficiency of aircraft structure design, an automatic modeling system for skeleton model of aircraft with complex surfaces is developed based on CATIA VBA. The system can provide the generation of the main structure skeleton model of the aircraft, the creation/output of skeleton model properties and the automatic splitting of the aircraft skin. Besides, an aircraft design template is proposed to formalize the design standardization of aircraft structure and rapid modeling procedure. The efficiency and accuracy of the aircraft structure design are improved, and the finite element pre-processing time is shortened by the system.","PeriodicalId":105556,"journal":{"name":"2020 5th International Conference on Computer and Communication Systems (ICCCS)","volume":"214 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Automatic Modeling System for Skeleton Model of Aircraft with Complex Surfaces\",\"authors\":\"Dangdang Zheng, Bing Han, Geng Liu, R. Tong\",\"doi\":\"10.1109/ICCCS49078.2020.9118536\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"There are complex and repeated modeling works during the process of aircraft design, which leads to the heavy workload and low working efficiency. In order to improve the quality and efficiency of aircraft structure design, an automatic modeling system for skeleton model of aircraft with complex surfaces is developed based on CATIA VBA. The system can provide the generation of the main structure skeleton model of the aircraft, the creation/output of skeleton model properties and the automatic splitting of the aircraft skin. Besides, an aircraft design template is proposed to formalize the design standardization of aircraft structure and rapid modeling procedure. The efficiency and accuracy of the aircraft structure design are improved, and the finite element pre-processing time is shortened by the system.\",\"PeriodicalId\":105556,\"journal\":{\"name\":\"2020 5th International Conference on Computer and Communication Systems (ICCCS)\",\"volume\":\"214 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-05-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 5th International Conference on Computer and Communication Systems (ICCCS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICCCS49078.2020.9118536\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 5th International Conference on Computer and Communication Systems (ICCCS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICCCS49078.2020.9118536","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Automatic Modeling System for Skeleton Model of Aircraft with Complex Surfaces
There are complex and repeated modeling works during the process of aircraft design, which leads to the heavy workload and low working efficiency. In order to improve the quality and efficiency of aircraft structure design, an automatic modeling system for skeleton model of aircraft with complex surfaces is developed based on CATIA VBA. The system can provide the generation of the main structure skeleton model of the aircraft, the creation/output of skeleton model properties and the automatic splitting of the aircraft skin. Besides, an aircraft design template is proposed to formalize the design standardization of aircraft structure and rapid modeling procedure. The efficiency and accuracy of the aircraft structure design are improved, and the finite element pre-processing time is shortened by the system.