AIRCRAFT FLAP DEFLECTION MECHANISM

摘要

FIELD: aeronautical engineering. ^ SUBSTANCE: proposed flap deflection mechanism has carriage 1 connected with kinematic members and power rods and with tail member of flap 4 by means of swivel rod 9. Rod 9 has body where stem with adjustable end-piece is mounted in radial thrust ball bearing units. ^ EFFECT: extended capabilities of mechanism. ^ 6 cl, 2 dwg