Invention Grant
US09278751B2 High lift system for an aircraft 有权
飞机高升程系统

High lift system for an aircraft
Abstract:
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.
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