| 大尺寸复合材料RTM波纹梁设计优化 |
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| 引用本文： | 刘豫,李巧,宋艳华.大尺寸复合材料RTM波纹梁设计优化[J].航空工程进展,2014,5(4):541-546. |
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| 作者姓名： | 刘豫 李巧 宋艳华 |
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| 作者单位： | 中国航空工业集团公司第一飞机设计研究院,西安,710089 |
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| 摘 要： | 为了对使用Resin Transfer Molding(RTM)工艺制造的大尺寸复合材料波纹梁进行结构减重设计优化,运用CATIA软件复合材料设计模块对大尺寸波纹梁进行多厚度分区设计,并编制FORTRAN软件二次开发程序对波纹梁铺层角度和顺序进行优化,进行静强度计算,设计并进行波纹梁剪切试验,制造的波纹梁在某型飞机上成功应用并取得了明显的减重效果。
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| 关 键 词： | RTM 波纹梁 优化设计 CATIA FORTRAN 试验 |
| 收稿时间： | 3/4/2014 12:00:00 AM |
| 修稿时间： | 8/5/2014 12:00:00 AM |
Optimal Design of Composite RTM Waved-Beams with Large Size |
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| Liu yu,Li qiao and Song yanhua.Optimal Design of Composite RTM Waved-Beams with Large Size[J].Advances in Aeronautical Science and Engineering,2014,5(4):541-546. |
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| Authors: | Liu yu Li qiao and Song yanhua |
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| Institution: | (The First Aircraft Institute, Aviation Industry Corporation of China, Xi＇an 710089, China) |
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| Abstract: | In order to reduce structural weight of composite RTM waved-beams with large size,the design work for complex thickness area of waved-beams is done through the software CATIA.The ply angle and stacking sequence of composite laminates is optimized and its static strength is calculated by coding FORTRAN program.The waved-beams shear test is performed.This waved-beam has been successfully applied to a certain aircraft and shows significant effect on reducing the structural weight. |
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| Keywords: | RTM waved-beams optimization design CATIA FORTRAN test |
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