AIRCRAFT FLAP DEFLECTION MECHANISM Russian patent published in 2007 - IPC B64C3/50 B64C13/00

Abstract RU 2296083 C1

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

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RU 2 296 083 C1

Authors

Apalishin German Timofeevich

Shapoval Vladimir Grigor'Evich

Dates

2007-03-27—Published

2005-08-08—Filed