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| 复合材料损伤结构胶接补强修补分析及设计 | |
| 引用本文： | 孟凡颢,陈绍杰,董善艳,童小燕.复合材料损伤结构胶接补强修补分析及设计[J].飞机设计,2002(1):18-21. |
| 作者姓名： | 孟凡颢 陈绍杰 董善艳 童小燕 |
| 作者单位： | 1. 西北工业大学飞行器结构完整性研究所,西安,710072;沈阳飞机设计研究所,沈阳,110035 2. 沈阳飞机设计研究所,沈阳,110035 3. 西北工业大学飞行器结构完整性研究所,西安,710072 |
| 摘 要： | 对复合材料层合板采用20节点等参元、对于胶层采用节理单元建立有限元分析模型，并针对胶接补强修补的两种形式－－贴补和挖补编制了相应的三维有限元分析程序，进行静力分析，获得了修补参数对修补效果的影响曲线，据此来初步确定最佳的修补参数。 |
| 关 键 词： | 设计 复合材料 胶接修补 有限元分析 直升机 飞机结构 |
| 修稿时间： | 2001年9月9日 |
THE ANALYSIS AND DESIGN OF THE ADHESIVE BONDING REPAIR OF THE DAMAGED COMPOSITE COMPONENTS |
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| Meng fanhao ,Chen Shaojie ,Dong Shanyan ,Tong Xiaoyan.THE ANALYSIS AND DESIGN OF THE ADHESIVE BONDING REPAIR OF THE DAMAGED COMPOSITE COMPONENTS[J].Aircraft Design,2002(1):18-21. | |
| Authors: | Meng fanhao Chen Shaojie Dong Shanyan Tong Xiaoyan |
| Institution: | Meng fanhao 1,2,Chen Shaojie 2,Dong Shanyan 1,Tong Xiaoyan 1 |
| Abstract: | In this paper, the author set up a finite element analysis model, in which the author adopts the 20-node is oparametric brick element to plot the composite laminate and adopts the 16-node curved-surface joint element to plot the adhesive. Aiming at two types of bonded adhesive repair-scarf patch repair and extermal patch repair, the author designed a 3-dimension finite element analysis program, conducted static analysis and achieved the curves of the repair effect of the parameters, with which the optimal repair parameters can be primarily determined. |
| Keywords: | composites adhesive bonding patch repair finite elemental analysis |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |