公开(公告)号：US09969341B2

公开(公告)日：2018-05-15

申请号：US14895779

申请日：2014-06-06

申请人： Labinal Power Systems

发明人： Pierre Henrard ,  Nicolas Carre ,  Bruno Chapotin

IPC分类号： B60L1/00 ,  B60R16/03 ,  H01H47/04 ,  H02J1/00 ,  H02J3/00 ,  B64D47/00 ,  H02H7/06 ,  H02J4/00 ,  H01H47/22

CPC分类号： B60R16/03 ,  B64D47/00 ,  B64D2221/00 ,  H01H47/04 ,  H01H47/22 ,  H02H7/06 ,  H02J1/00 ,  H02J3/00 ,  H02J4/00

摘要： The invention relates to an assistance device (17) for an electrical power generation system (11) of an aircraft, said system (11) comprising a generator (13), a regulator (14) and a contactor (15) comprising contacts and an actuator for opening/closing the contacts which is controlled by said regulator (14) and arranged between the generator (13) and a distribution architecture (12), the assistance device being characterized in that it is connected to at least one power source (18) which is separate from the generator (13) and the regulator (14), and in that it comprises means for closing the contactor which are suitable for connecting the power source (18) to the actuator (23) of the contactor (15) in order to provide the current necessary for closing said contactor (15).

公开(公告)号：US20160129862A1

公开(公告)日：2016-05-12

申请号：US14895779

申请日：2014-06-06

申请人： Labinal Power Systems

发明人： Pierre Henrard ,  Nicolas Carre ,  Bruno Chapotin

IPC分类号： B60R16/03 ,  H02J4/00 ,  B64D47/00 ,  H02H7/06

CPC分类号： B60R16/03 ,  B64D47/00 ,  B64D2221/00 ,  H01H47/04 ,  H01H47/22 ,  H02H7/06 ,  H02J1/00 ,  H02J3/00 ,  H02J4/00

摘要： The invention relates to an assistance device (17) for an electrical power generation system (11) of an aircraft, said system (11) comprising a generator (13), a regulator (14) and a contactor (15) comprising contacts and an actuator for opening/closing the contacts which is controlled by said regulator (14) and arranged between the generator (13) and a distribution architecture (12), the assistance device being characterised in that it is connected to at least one power source (18) which is separate from the generator (13) and the regulator (14), and in that it comprises means for closing the contactor which are suitable for connecting the power source (18) to the actuator (23) of the contactor (15) in order to provide the current necessary for closing said contactor (15).

摘要翻译： 本发明涉及一种用于飞行器的发电系统（11）的辅助装置（17），所述系统（11）包括发电机（13），调节器（14）和接触器（15），其包括触点和 致动器，其用于打开/关闭由所述调节器（14）控制并且布置在所述发电机（13）和分配架构（12）之间的所述触点，所述辅助装置的特征在于，所述辅助装置连接到至少一个电源 ），其与发电机（13）和调节器（14）分离，并且其包括用于闭合适于将电源（18）连接到接触器（15）的致动器（23）的接触器的装置， 以便提供关闭所述接触器（15）所需的电流。