| title | CFRP一面せん断接着継手の強度 |
| Other Title | Strength of CFRP Single-Lap Joints |
| Author(jpn) | 中村, 俊一郎 |
| Author(eng) | Nakamura, Shunichiro |
| Author Affiliation(jpn) | 第一工業大学航空宇宙工学科 |
| Author Affiliation(eng) | Department of Aeronautics Engineering, Daiichi University of Technology |
| Issue Date | 2010-03 |
| Publisher | 第一工業大学
Daiichi University of Technology |
| Publication title | 第一工業大学研究報告
Research Report |
| Issue | 22 |
| Start page | 53 |
| End page | 56 |
| Publication date | 2010-03 |
| Language | jpn
eng |
| Abstract | The airplane made by composite materials, especially carbon fiber reinforced plastic (CFRP), are often damaged the structure during the operation of it. The damaged areas are repaired by several methods. One of them is adhesively bonded CFRP patch repair. In this paper, four pieces of adhesively bonded CFRP single lap joint are fabricated and tested. Handmade film type adhesive is used for bonding. Different failure modes are observed, which leads to scattered values of their strength. This test results are compared with the other reports. It is difficult to control the failure mode of the bonded joints with the handmade film type adhesives. Manufactured adhesive is recommended to the bonded joints. |
| Description | 形態: カラー図版あり
Physical characteristics: Original contains color illustrations |
| Keywords | composite materials; adhesively bonded repairs; single lap joints; CFRP patches; failure modes |
| Document Type | Departmental Bulletin Paper |
| ISSN | 2187-0462 |
| NCID | AN10303695 |
| SHI-NO | AA0064708004 |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/18105 |
