Analysis, design and simulation of single-phase power supply for rotor excitation of aircraft starter/generator
The demand of electrical power increases rapidly in the new designs of military and civil aircrafts due to its better performance, less maintenance, less weight and high efficiency. To meet this growing demand of electrical power, engine coupled starter/generators coupled w...
Saved in:
Main Author: | Xing, Da |
---|---|
Other Authors: | Tseng King Jet |
Format: | Final Year Project |
Language: | English |
Published: |
2016
|
Subjects: | |
Online Access: | http://hdl.handle.net/10356/68154 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
Power inverter for high speed starter/generator in aircraft applications
by: Geng, Shen
Published: (2016) -
Design of 100 kVA SiC power converter for aircraft electric starter generator
by: Lim, Ziyou, et al.
Published: (2020) -
SIMULATION AND ANALYSIS OF LONGITUDINAL FLIGHT DYNAMICS OF TILT ROTOR AIRCRAFT ON TRANSITION PHASE
by: RAFI HADYTAMA, MUHAMMAD -
Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator
by: Dehghani Tafti, Hossein, et al.
Published: (2015) -
Design and control for rotor-fixed wing hybrid aircraft
by: Wang, X., et al.
Published: (2014)