High lift system for an aircraft
An aircraft and lift technology, applied in the field of lift systems, to achieve low maintenance costs and weight savings
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[0064] figure 1 Embodiments of the present invention are shown. figure 1 Shown is an all-electric, internally redundant drive 200 for use in a high-lift system for an aircraft according to the invention. The drive means comprise an electric motor 201a driving the landing flaps (not shown) of the high-lift system. In this context, the electric motor 201a is characterized by internal redundancy created by redundant wiring.
[0065] Internally redundant brakes 202 are also shown; it should be emphasized that only a single brake is required to lock the entire drive system. Also shown are the control electronics 203a actuating the phase groups of the individual sub-motors of the electric motor 201a. In context, for example in Figure 4 As shown in , each sub-motor can also be individually controlled by the corresponding control electronics.
[0066] Also shown is a shaft 206 to which the electric motor 201a transmits all of the torque. Also shown is a reduction gear unit 20...
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