FIELD: aircraft alighting gears; mechanical units for control of aircraft landing gear locks; emergency landing gear extension systems.
SUBSTANCE: proposed device has handle 1 connected with lock control mechanism which is connected in its turn with ratio control mechanism 17 by means of upper rod 3 and lower rod 13; mechanism 17 is connected with landing gear locks. Mounted between rods is additional member 10 and splined shaft articulated with one of its ends. Other end of additional member is secured to upper lower rod depending on position of axis 7 of rotation of upper part 6 of control panel relative to rods (before or after them); splines of splined shaft are received by splined hole of lower or upper rods in case of deflection of control panel.
EFFECT: enhanced operational reliability; reduced servicing time.
1 dwg
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