FIELD: aircraft engineering.
SUBSTANCE: proposed aircraft landing gear lifting mechanism comprises actuating cylinders, drive unit including at least two motors and reduction gear linked up with one or more actuating mechanisms via cardan joint. Aforesaid actuating mechanisms are coupled with floats. Drive unit is rigidly attached to fuselage, while the float is mounted on aircraft fuselage to turn horizontally. Every actuating cylinder incorporates at least two micro switches.
EFFECT: higher reliability of landing gear lifting mechanism and improved chances of moving landing gear floats in horizontal plane.
2 dwg
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