Actuation system design with electrically powered actuators
This project addresses the actuation system architecture of future All-electric aircraft (AEA) with electrically powered actuators (EPA). Firstly, the information of EPAs is reviewed, and then an electro-hydrostatic actuator (EHA) and electro-mechanical actuator (EMA) are selected for further system...
| Main Author: | |
|---|---|
| Other Authors: | |
| Language: | en |
| Published: |
Cranfield University
2011
|
| Subjects: | |
| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/6282 |