LANDING GEAR UP LOCAL Russian patent published in 1997 - IPC

Abstract RU 2076827 C1

FIELD: mechanical engineering; aviation; fixing of loads or constructions in lifted position; fixing of aircraft landing gears in retracted position. SUBSTANCE: landing gear up lock has body consisting of two cheeks 1 connected to each other, hook 2, power hydraulic cylinder 3, resilient member 4. Lock has two-link mechanism whose upper link 5 is made in the form of bell crank hinge connected by one arm with end of resilient member 4 and by other arm, with hook 2. EFFECT: improved reliability. 2 cl, 2 dwg

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RU 2 076 827 C1

Authors

Sokolov V.I.

Dates

1997-04-10—Published

1992-07-03—Filed