版权所有:内蒙古大学图书馆 技术提供:维普资讯• 智图
内蒙古自治区呼和浩特市赛罕区大学西街235号 邮编: 010021
作者机构:German Aerosp Ctr Ctr Lightweight Prod Technol Technol Zentrum 4 D-86159 Augsburg Germany IVU Traff Technol AG Bundesallee 88 D-12161 Berlin Germany
出 版 物:《COMPOSITE STRUCTURES》 (复合材料结构)
年 卷 期:2019年第210卷
页 面:906-913页
核心收录:
学科分类:08[工学] 0805[工学-材料科学与工程(可授工学、理学学位)] 080502[工学-材料学] 0801[工学-力学(可授工学、理学学位)]
基 金:Federal Ministry for Economic Affairs and Energy (BMWi)
主 题:Lightning strike protection material Composite fuselage Automation Offline programming Path generation Doubly curved surface
摘 要:Lighting strike protection is not intrinsically provided on modern composite built aircraft due to the lower electrical conductivity of composite materials. A highly conductive copper foil is manually applied onto the fuselage in multiple overlapping tapes. Known automation processes are not adequate for wide tapes particularly in the case of large double-curved surfaces. One key technology for enabling an automated process is tape trajectory generation with a focus on automation constraints. We are introducing a new tape application mechanism for a single wide tape. Our algorithm generates geometry induced layup trajectories, taking into account geometric conditions. We experimentally demonstrate a wrinkle-free automated application. Based on the first algorithm, a second algorithm addresses the challenging issue of an optimised surface coverage with multiple tapes for a fuselage section. A tape application fitness criterion is defined and implemented. We point out that a computer-based algorithm is advantageous for determining the proper arrangement of multiple tapes. It is thus now possible to create a multiple tape design that can be applied with an automation process. In addition, the optimisation leads to a reduction of consumed and wasted tape material in the fuselage production process.