FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, aircraft wing and aircraft incorporating such wing. Aircraft wing comprises torsion boxes, support fitted on torsion box to turn about flap rotation axis, flap secured to support to turn about rotational axis in support turn about torsion box; transfer mechanism coupled with support to set angular position of flap relative to torsion box, and device to measure flap angular position. Said measuring device incorporates rotation pickup mounted on support and four-link jointing gear to couple turn pickup with transfer mechanism. In compliance with first version, aircraft comprises, at least, one such wing. In compliance with second version, it comprises additionally device to estimate rotation pickup signals, which is connected to two rotation pickups.
EFFECT: higher reliability.
12 cl, 6 dwg
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Authors
Dates
2011-04-10—Published
2006-12-29—Filed