System for generating, converting, distributing and electrically starting on board an aircraft

• Main Authors: DUCES MARC, FOCH ETIENNE, LANDO JEAN LOUIS
• Format: Patent
• Language: Chinese; English
• Published: 11.09.2013
• Subjects: AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER; COSMONAUTICS; ELECTRICITY; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERATION; PARACHUTES; PERFORMING OPERATIONS; SYSTEMS FOR STORING ELECTRIC ENERGY; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS; TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE; TRANSPORTING

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.