| 摘要: |
| 开展了可靠性与结构一体化设计方法的研究。通过对机载电子设备数字样机进行应力
分析发现设计薄弱环节，并根据薄弱环节对设备进行了设计优化，从而满足设备的环境适应
性要求。在此基础上，进行设备的潜在故障分析与可靠性优化，提升设备的可靠性指标。某
机载电子设备的应用实践与试验验证表明了这种一体化设计方法在电子设备设计中的适用性
。 |
| 关键词: 机载电子设备 结构设计 可靠性设计 应力分析 一体化设计 优化设计 |
| DOI： |
|
| 基金项目: |
|
| Reliability and structure integrated design method for airborne avionics |
| HU Yun |
| () |
| Abstract: |
| Integrated design of reliability and structure is proposed in this pap
er. The requirements for environmental adaptability can be satisfied by optimiza
t
ion design of vulnerability detected through stress analysis. On this base, rel
iability of avionics can be improved by potential fault analysis and reliability
optimization. The method of integrated design has been validated by following a
pplication and tests. |
| Key words: airborne avionics structure design reliability design stress analysis integrated design optimization design |
《电讯技术》编辑部 