发明名称 Emergency Power Supply System, Aircraft Having Such An Emergency Power Supply System And A Method For Providing At Least Electric Power And Hydraulic Power In Case Of An Emergency In An Aircraft
摘要 An emergency power supply system for providing hydraulic power and electric power in an aircraft includes a fuel cell having an electric outlet for providing electric power, a conversion unit couplable with at least one of an AC bus and a DC bus and the electric outlet, and at least one hydraulic pump having a reconfigurable electric motor and a motor control unit and being couplable with a hydraulic system for providing hydraulic power. The conversion unit is adapted for converting a supply voltage of the electrical outlet to at least one of an AC voltage matching a predetermined voltage at the AC bus and a DC voltage matching a predetermined voltage at the DC bus. The reconfigurable electric motor is couplable with the fuel cell and the AC bus and is adapted for being operated by the supply of electric power either from the fuel cell or the AC bus.
申请公布号 US2016090189(A1) 申请公布日期 2016.03.31
申请号 US201514863615 申请日期 2015.09.24
申请人 Airbus Operations GmbH ;Airbus Defence and Space GmbH 发明人 Wangemann Joerg;Leudders Hauke-Peer;Zandstra Sijmen;Drechsel Peer
分类号 B64D41/00;H01M8/02;F04D13/06 主分类号 B64D41/00
代理机构 代理人
主权项 1. An emergency power supply system for providing at least hydraulic power and electric power in an aircraft, the system comprising: at least one fuel cell having an electric outlet for providing electric power; a conversion unit for conversion of electric power couplable with at least one of an AC bus and a DC bus of the aircraft and the electric outlet of the at least one fuel cell; and at least one hydraulic pump having a reconfigurable electric motor and a motor control unit and being couplable with a hydraulic system of the aircraft for providing hydraulic power, wherein the conversion unit is adapted for converting a supply voltage of the electrical outlet of the at least one fuel cell to at least one of an AC voltage matching a predetermined voltage at the AC bus and a DC voltage matching a predetermined voltage at the DC bus, and wherein the reconfigurable electric motor is couplable with the at least one fuel cell and the AC bus, wherein the reconfigurable electric motor is adapted for being operated by the supply of electric power either from the at least one fuel cell or the AC bus.
地址 Hamburg DE