DEVICE FOR CONTROL OF AIRCRAFT LANDING GEAR LOCKS Russian patent published in 2006 - IPC B64C25/30

Abstract RU 2290347 C2

FIELD: aviation; alighting gears; mechanical units for control of aircraft landing gear locks.

SUBSTANCE: proposed device has stick mounted in body secured on control panel; this stick is connected with input shaft of variable gearing mechanism by means of rod passed through intermediate member; variable gearing mechanism is connected with landing gear locks. Body is provided with lugs whose holes are used for mounting the guides; upper ends of these guides are immovably secured on control panel together with bracket and lower ends are received by lugs formed on support secured on control panel. One of guides have holes for locking the body in initial and working positions by means of lock located in respective lug of body.

EFFECT: ease of use during flight due to accessibility of instruments on control panel.

3 dwg

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RU 2 290 347 C2

Authors

Smirnov Evgenij Ivanovich

Dolgov Vladimir Il'Ich

Dates

2006-12-27—Published

2004-03-29—Filed