Abstract
A simulation model for the dynamic characteristics of pressure relief valve was established based on AMESim in this paper to solve the problem of the abnormal outlet pressure fluctuation during the -40 environmental test of the pressure relief valve of the booster delivery system of a certain type of launch vehicle. By calibrating the model with test data and parameters of the valve and test system and using the Stribeck friction model, the simulation successfully reproduced the pressure fluctuation phenomenon, located the cause of the failure and showed the main reason for the longterm drop in pressure. To solve the problem, the proposed improvement scheme of the high-pressure sealing structure was simulated and verified by experiments.
| Original language | English |
|---|---|
| Title of host publication | IET Conference Proceedings |
| Publisher | Institution of Engineering and Technology |
| Pages | 636-641 |
| Number of pages | 6 |
| Volume | 2020 |
| Edition | 3 |
| ISBN (Electronic) | 9781839534195 |
| DOIs | |
| State | Published - 2020 |
| Event | 2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020 - Virtual, Online Duration: 18 Sep 2020 → 21 Sep 2020 |
Conference
| Conference | 2020 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2020 |
|---|---|
| City | Virtual, Online |
| Period | 18/09/20 → 21/09/20 |
Keywords
- EXPERIMENT
- FRICTION
- LEAKAGE
- PRESSURE RELIEF VALVE
- SIMULATION
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