公开(公告)号：US10110015B2

公开(公告)日：2018-10-23

申请号：US15113872

申请日：2015-01-28

申请人： Safran Electrical & Power

发明人： Roland Casimir ,  Djemouaï Hadjidj ,  Vincent Giorgis

IPC分类号： H02J4/00 ,  H02J5/00 ,  H02J7/00 ,  H02J7/14

摘要： The invention relates to an electrical conversion and distribution system for an aircraft, the system comprising at least one synchronous starter-generator (S/G1, S/G2) intended to be coupled to an engine (Engine1) of the aircraft, at least one conversion path comprising a plurality of power converters (CVn, CV′n) associated with switching means suitable for supplying at least one charge (CAC1, CAC2, CAC3, CAC4, P1, P2) from at least one source (S/G1, S/G2, AUX S/G1, AUX S/G2, GPU1, GPU2), and at least one distribution path suitable for supplying electrical charges (CT1n, SW1n, CT2n, SW2n).

公开(公告)号：US10110016B2

公开(公告)日：2018-10-23

申请号：US15115182

申请日：2015-01-28

申请人： Safran Electrical & Power

发明人： Roland Casimir ,  Vincent Giorgis ,  Eric de Wergifosse

IPC分类号： B64D41/00 ,  H02J3/46 ,  H02M7/06 ,  H02M7/217 ,  H02M7/537 ,  H02J5/00 ,  H02J7/02 ,  H02J7/14 ,  H02J7/00

摘要： The invention relates to an electrical conversion and distribution system for an aircraft, the system comprising a synchronous starter-generator (ENG S/G) intended to be coupled to an aircraft engine, a rectifier (R) capable of transforming alternating voltage into direct voltage, an auxiliary synchronous starter-generator (AUX S/G) intended to be coupled to an auxiliary power group, a first, a second and a third power converter (CV1, CV2, CV3) capable of transforming direct voltage into alternating voltage or vice versa, and at least one battery (BATT).

公开(公告)号：US20160352129A1

公开(公告)日：2016-12-01

申请号：US15113872

申请日：2015-01-28

申请人： SAFRAN ELECTRICAL & POWER

发明人： Roland Casimir ,  Djemouaï Hadjidj ,  Vincent Giorgis

IPC分类号： H02J7/00

CPC分类号： H02J5/00 ,  B64D2221/00 ,  F02N11/08 ,  H02J4/00 ,  H02J7/1423 ,  H02J2007/143

摘要： The invention relates to an electrical conversion and distribution system for an aircraft, the system comprising at least one synchronous starter-generator (S/G1, S/G2) intended to be coupled to an engine (Engine1) of the aircraft, at least one conversion path comprising a plurality of power converters (CVn, CV′n) associated with switching means suitable for supplying at least one charge (CAC1, CAC2, CAC3, CAC4, P1, P2) from at least one source (S/G1, S/G2, AUX S/G1, AUX S/G2, GPU1, GPU2), and at least one distribution path suitable for supplying electrical charges (CT1n, SW1n, CT2n, SW2n).

摘要翻译： 本发明涉及一种用于飞行器的电气转换和分配系统，该系统包括旨在耦合到飞行器的发动机（Engine1）的至少一个同步起动器 - 发电机（S / G1，S / G2），至少一个 转换路径包括与适于从至少一个源（S / G1，S）提供至少一个电荷（CAC1，CAC2，CAC3，CAC4，P1，P2）的开关装置相关联的多个功率转换器（CVn，CV'n） / G2，AUX S / G1，AUX S / G2，GPU1，GPU2）和适合于提供电荷（CT1n，SW1n，CT2n，SW2n）的至少一个分配路径。

公开(公告)号：US20160380437A1

公开(公告)日：2016-12-29

申请号：US15115182

申请日：2015-01-28

申请人： Safran Electrical & Power

发明人： Roland Casimir ,  Vincent Giorgis ,  Eric de Wergifosse

IPC分类号： H02J3/46 ,  B64D41/00 ,  H02M7/217 ,  H02M7/06 ,  H02M7/537

CPC分类号： H02J5/00 ,  B64D41/00 ,  B64D2221/00 ,  H02J3/46 ,  H02J7/02 ,  H02J7/1415 ,  H02J7/1492 ,  H02J2007/0059 ,  H02J2007/143 ,  H02M7/06 ,  H02M7/217 ,  H02M7/537

摘要： The invention relates to an electrical conversion and distribution system for an aircraft, the system comprising a synchronous starter-generator (ENG S/G) intended to be coupled to an aircraft engine, a rectifier (R) capable of transforming alternating voltage into direct voltage, an auxiliary synchronous starter-generator (AUX S/G) intended to be coupled to an auxiliary power group, a first, a second and a third power converter (CV1, CV2, CV3) capable of transforming direct voltage into alternating voltage or vice versa, and at least one battery (BATT).

摘要翻译： 本发明涉及一种用于飞行器的电气转换和分配系统，该系统包括旨在耦合到飞机发动机的同步起动器 - 发电机（ENG S / G），能够将交流电压转换为直流电压的整流器 ，用于耦合到辅助电源组的辅助同步起动器 - 发电机（AUX S / G），能够将直流电压转换为交流电压或副变压器的第一，第二和第三功率转换器（CV1，CV2，CV3） 和至少一个电池（BATT）。