Segmentized flap system
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United States of America Patent
Stats
-
Jan 9, 1990
Grant Date -
N/A
app pub date -
Aug 26, 1986
filing date -
Aug 29, 1985
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
A flap system along the trailing edge of a transonic 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; are controlled 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 on vertical axes, in addition to a regular pivoting about respective horizontal axes.
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