Abstract
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.
| Original language | English |
|---|---|
| Title of host publication | AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 682-685 |
| Number of pages | 4 |
| ISBN (Electronic) | 9781509010875 |
| DOIs | |
| State | Published - 17 Nov 2016 |
| Event | 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 - Beijing, China Duration: 10 Oct 2016 → 12 Oct 2016 |
Publication series
| Name | AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems |
|---|
Conference
| Conference | 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 |
|---|---|
| Country/Territory | China |
| City | Beijing |
| Period | 10/10/16 → 12/10/16 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Keywords
- AMESim simulation
- energy optimization
- loading actuation
- structure test
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