| 飞机结构损伤的复合材料胶接修补技术研究进展 |
| |
| 引用本文： | 童谷生%孙良新%刘英卫.飞机结构损伤的复合材料胶接修补技术研究进展[J].宇航材料工艺,2002,32(5):20-24,29. |
| |
| 作者姓名： | 童谷生%孙良新%刘英卫 |
| |
| 作者单位： | 1. 南京航空航天大学航空宇航学院,南京,210016
2. 洪都航空集团,南昌,330024 |
| |
| 摘 要： | 系统归纳并分析了国内外30年来在复合材料胶接修补研究中所取得的效果，以及最近10年的最新研究动态，涉及损伤修补设计，有限元精确分析，智能修补等，并指出了研究中值得注意的问题。
|
| 关 键 词： | 胶接修补 损伤修复 复合材料 飞机结构 无损检测 智能结构 |
A Review on Composite Bonded Repair Technique for Damaged Aircraft Structures |
| |
| Tong Gusheng,Sun Liangxin.A Review on Composite Bonded Repair Technique for Damaged Aircraft Structures[J].Aerospace Materials & Technology,2002,32(5):20-24,29. |
| |
| Authors: | Tong Gusheng Sun Liangxin |
| |
| Abstract: | To extend the service life of aging or damaged aircraft, the damaged components must be replaced or repaired. A adhesively bonded technique of composite to repair damaged aircraft has been developed since 1970s. By using a series of character of the advanced composites, such as high strength ratio and stiffness ratio, the damaged component can be effectively repaired.Research achievements of the composite bonded repair technique applied to damaged aircraft structure are reviewed,and problems to be solved in the future are presented. |
| |
| Keywords: | Damage repair Composite material Aircraft structure Nondestructive testing Smart structure |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《宇航材料工艺》浏览原始摘要信息 |
| 点击此处可从《宇航材料工艺》下载免费的PDF全文 |
