Calculation of hybrid joints used in modern aerospace structures
The state – of - the art of aeronautical structures show that parts are manufactured and subsequently assembled with the use of fasteners and/ or bonding. Adhesive bonding is a key technology to low weight, high fatigue resistance, robustness and an attractive design for cost structures.The paper re...
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2011-12-01
|
| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/stere_baran_v3_iss_4_full.pdf |
| Summary: | The state – of - the art of aeronautical structures show that parts are manufactured and subsequently assembled with the use of fasteners and/ or bonding. Adhesive bonding is a key technology to low weight, high fatigue resistance, robustness and an attractive design for cost structures.The paper results resolve significant problems for two groups of end-users:1) for the aerospace design office: a robust procedure for the design of the hybrid joint structural components;2) for the aeronautical repair centres: a useful procedure for structural design and analysis with significant cost savings. |
|---|---|
| ISSN: | 2066-8201 2247-4528 |