Abstract
The braking system of the aircraft is an important subsystem of the aircraft's landing braking. Flapper-nozzle pressure servo valve is the key hydraulic component of the brake system. The goal of this paper is to establish the mathematical model of flapper-nozzle pressure servo valve, deduce the transfer function, and use the MATLAB/Simulink simulation platform to build a reliable and effective simulation model. It can support the parameter selection of the hydraulic components of the subsequent models of the brake system.
| Original language | English |
|---|---|
| Title of host publication | CSAA/IET International Conference on Aircraft Utility Systems, AUS 2024 |
| Publisher | Institution of Engineering and Technology |
| Pages | 1153-1158 |
| Number of pages | 6 |
| Volume | 2024 |
| Edition | 13 |
| ISBN (Electronic) | 9781837242108 |
| DOIs | |
| State | Published - 2024 |
| Event | 2024 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2024 - Xi�an, China Duration: 16 Aug 2024 → 19 Aug 2024 |
Conference
| Conference | 2024 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2024 |
|---|---|
| Country/Territory | China |
| City | Xi�an |
| Period | 16/08/24 → 19/08/24 |
Keywords
- BRAKE SYSTEM
- DYNAMIC RESPONSE
- FLAPPER-NOZZLE PRESSURE SERVO VALVE
- MATHEMATICAL MODELING
- TRANSFER FUNCTION
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