FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to wing flap lift increasing regulator. Proposed regulator comprises one drive 20 of wing flap 2, 102 and several driving devices 3, 4, 5. The latter comprise devices to transmit tensioning and contracting forces for flap 2, 102 to be coupled with wing 1. Two first driving devices 3, 5 direct flap 2, 102 to definite position relative to wing chord direction. One second driving device 4 comprises compensator 10, 110 to allow flap 2, 102 to displace toward wing chord to compensate for relative displacements between flap and wing.
EFFECT: compensation of warping forces caused by relative displacements.
19 cl, 4 dwg
