FIELD: transport.
SUBSTANCE: proposed aircraft control system comprises elevator articulated with feathering surface that permanently tends to get arranged parallel with flow for elevator to follow it. Articulation is configured so that varying pitch causes change in elevator position relative to feather. In compliance with regression version, elevator turns through greater angle compared with feather to lessen control effect in increase in vertical slip. Invention covers also versions of mechanic, hydraulic and electric linkage.
EFFECT: ruling out elevator stall.
16 cl, 11 dwg
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