AIRCRAFT
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United States of America Patent
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app pub date -
Mar 14, 2013
filing date -
Mar 16, 2012
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
The present invention relates to an aircraft having at least one landing flap arranged at the wing of the aircraft and having at least one drive unit for actuating the landing flap, wherein the aircraft furthermore has at least one control unit which controls the aileron function of the aircraft, wherein the control unit is connected to the named drive unit or units for adjusting the landing flap(s) and is configured such that it carries out the aileron function of the aircraft in at least one flight mode only or also by the operation of the named drive unit(s) and thus by the adjustment of the landing flap(s).
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