Segmentized flap system

B - Operations – Transporting – 64 – C

Patent

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B64C 13/26 (2006.01) B64C 9/16 (2006.01) B64C 9/20 (2006.01)

Patent

CA 1319664

SEGMENTIZED FLAP SYSTEM ABSTRACT OF THE DISCLOSURE A flap system along the trailing edge of a transsonic aircraft wing which system includes segments arranged in span direction, a driving system for protraction and retraction of the segments includes a plurality of spindle drives connected to the segments such that each segment is connected to at least two spindle drives; and control means for controlling the spindle drives in such a manner that at least some of the drives are independently controlled from each other so that the segments can pivot vertical axes in addition to normal pivoting about horizontal axes.

516994

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