原文传递
Lightning Strike Tests of Composite Connectors.
| 题名： | Lightning Strike Tests of Composite Connectors. |
| 作者： | Smith, D. P.;Campbell, F. J.;Bond, C. D.; |
| 关键词： | COMPOSITE AIRCRAFT, CONNECTORS, LIGHTNING, COMPOSITE MATERIALS, AIRCRAFT, COMPARISON, METALS, PULSES, STANDARDS, TEST AND EVALUATION. |
| 摘要： | Test results are presented on the lightning strike effects on composite and hybrid type multipin aircraft connectors in comparison with the standard all metal connectors. These tests were performed using a unipolar double exponential long duration pulse recommended by the SAE-AE4L committee at peak current levels of 3 kA, 10 KA, 15 kA, and 20 kA. Such peak current levels might be found in all-composite or partially composite aircraft or in exposed areas of all-metal aircraft. Lightning Strike, Composite Aircraft, Composite Connectors, Pulse Current Limits. |
| 总页数： | 72 |
| 报告类型： | 科技报告 |
相关文献
- Implementation Project: Strengthening of a Bridge near Hondo, Texas using Post-Installed Shear Connectors
- Strengthening Existing Non-Composite Steel Bridge Girders Using Post-Installed Shear Connectors.
- LABORATORY TESTING OF STRESS-LAMINATED WOOD DECKS ON STEEL BEAMS.
- Open Circuit Resonant (SansEC) Sensor Technology for Lightning Mitigation and Damage Detection and Diagnosis for Composite Aircraft Applications.
- Challenges in Modelling of Lightning-Induced Delamination; Effect of Temperature-Dependent Interfacial Properties
- Challenges in Modelling of Lightning-Induced Delamination; Effect of Temperature-Dependent Interfacial Properties.
检索历史
应用推荐
