SYSTEM FOR ON-BOARD GENERATION, CONVERTION, DISTRIBUTION AND ELECTRICALLY STARTING AN AIRCRAFT
The system has electrical distribution channels (B) e.g. three phase alternating system, for high power loads and electrical distribution channels (G1) for conventional loads e.g. fuel pump. The distribution channels are separated and are powered by starter-generators (SG-B, SG-B1) e.g. brushless th...
Saved in:
Main Authors | , , |
---|---|
Format | Patent |
Language | English French German |
Published |
06.09.2017
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | The system has electrical distribution channels (B) e.g. three phase alternating system, for high power loads and electrical distribution channels (G1) for conventional loads e.g. fuel pump. The distribution channels are separated and are powered by starter-generators (SG-B, SG-B1) e.g. brushless three phase synchronous generator, where the channels for high power loads comprise rectifiers (RU-B1, RU-B2) and inverters (MCU-B1, MCU-B2). The generators are driven by a jet engine (Eng1) of an aircraft. |
---|---|
Bibliography: | Application Number: EP20070821838 |