发明名称 |
HIGH LIFT SYSTEM FOR AN AIRCRAFT |
摘要 |
A high lift system for an aircraft, which extends and retracts the landing flaps of the aircraft in a fully electric manner. In this context, a fully electric drive is used, comprising an electric motor having an internal redundancy, in such a way that the electric motor is configured as a fault-tolerant electric motor. It may thus be possible to do without a coupling gear unit in the electric motor. |
申请公布号 |
EP2694364(A2) |
申请公布日期 |
2014.02.12 |
申请号 |
EP20120715349 |
申请日期 |
2012.04.05 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
CHRISTMANN, MARKUS;GIEBELER, CHRISTOPH;RECKSIEK, MARTIN;DORR, BJOERN |
分类号 |
B64C13/24;B64C13/50 |
主分类号 |
B64C13/24 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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