发明名称 |
Aircraft including an electric starter-generator for the or each turbojet, an undercarriage fitted with an electric motor for taxiing, an electricity converter, and an electricity distribution unit connecting the electricity converter to the starter-generator and the electric motor |
摘要 |
An aircraft including an electric starter-generator for each of turbojets, and an undercarriage including an electric motor for taxiing the aircraft, which mutualizes an electricity converter for starting and for taxiing the aircraft. A single electricity converter is configured to be coupled to the electric starter-generator associated with a turbojet or to the electric motor of the undercarriage for taxiing, the coupling take place via an electricity distribution unit. |
申请公布号 |
US9227725(B2) |
申请公布日期 |
2016.01.05 |
申请号 |
US201013518254 |
申请日期 |
2010.12.15 |
申请人 |
LABINAL POWER SYSTEMS |
发明人 |
Berenger Serge;Godart Didier Francois |
分类号 |
B64D31/14;B64C25/40;B64D31/00 |
主分类号 |
B64D31/14 |
代理机构 |
Oblon, McClelland, Maier & Neustadt, L.L.P. |
代理人 |
Oblon, McClelland, Maier & Neustadt, L.L.P. |
主权项 |
1. An aircraft comprising:
a first turbojet engine fitted with a first electric starter-generator; an undercarriage fitted with a taxiing electric motor for taxiing the aircraft on the ground; an external electrical power inlet; an electricity converter; and an electricity distribution unit; wherein an inlet and an outlet of the electricity converter are connected to the electricity distribution unit; and wherein the electricity distribution unit is configured to selectively connect the first electric starter-generator, the taxiing electric motor, and the external electrical power inlet to the electricity converter. |
地址 |
Blagnac FR |