A method and apparatus for providing regulated direct current power for a direct current load on an aircraft. A regulated transformer rectifier unit on an aircraft comprises a plurality of converter modules connected in parallel between an input and an output. Each converter module in the plurality of converter modules comprises a transformer rectifier unit. The plurality of converter modules are controlled by a controller to provide regulated direct current power at the output from alternating current power provided at the input from an alternating current power source on the aircraft.
Regulated Transformer Rectifier Unit for Aircraft Systems
2016-05-26
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02M APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS , Anlagen zur Umformung von Wechselstrom in Wechselstrom, von Wechselstrom in Gleichstrom oder umgekehrt, oder von Gleichstrom in Gleichstrom und zur Verwendung in Netzen oder ähnlichen Stromversorgungssystemen |
Stable Electrical Power System with Regulated Transformer Rectifier Unit
European Patent Office | 2016
|Simulation of a transformer/rectifier unit for aircraft power-supply systems
Tema Archive | 1982
|Development of 200 Ampere Regulated Transformer Rectifier
British Library Conference Proceedings | 1999
|Development of 200 Ampere Regulated Transformer Rectifier
SAE Technical Papers | 1999
|REGULATING TRANSFORMER RECTIFIER UNIT FOR DC POWER APPLICATIONS
European Patent Office | 2017
|