摘要
Based on the characteristics of loading actuation's work pattern alternately switching between homodromous and converse load during the aircraft structure test especially in the fatigue loading test, an energy optimization type of power-by-wire valve-control integrated loading actuation system for aircraft structure test was designed. The system components and working principle was described. The loading scheme of the main and the minor valves working in different loading pattern was proposed. The modeling and simulation work of the energy optimization loading actuation system was completed. The feasibility of the main and the minor valves working in different loading pattern was proved. The simulation results demonstrate that the designed energy optimization type of power-by-wire valve-control integrated loading actuation system for aircraft structure test can improve the energy efficiency of the system obviously, and can be widely used in aircraft structural loading test system.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems |
| 出版商 | Institute of Electrical and Electronics Engineers Inc. |
| 页 | 682-685 |
| 页数 | 4 |
| ISBN(电子版) | 9781509010875 |
| DOI | |
| 出版状态 | 已出版 - 17 11月 2016 |
| 活动 | 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 - Beijing, 中国 期限: 10 10月 2016 → 12 10月 2016 |
出版系列
| 姓名 | AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems |
|---|
会议
| 会议 | 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 |
|---|---|
| 国家/地区 | 中国 |
| 市 | Beijing |
| 时期 | 10/10/16 → 12/10/16 |
联合国可持续发展目标
此成果有助于实现下列可持续发展目标:
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可持续发展目标 7 经济适用的清洁能源
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