AIRCRAFT RETRACTABLE LANDING GEAR LEG Russian patent published in 2015 - IPC B64C25/10 

Abstract RU 2545239 C1

FIELD: aircraft engineering.

SUBSTANCE: this leg comprises lever with wheel articulated with fuselage, extending shock absorber, leg retract-release cylinder, retracted-released position locks, link with one end coupled with gimbal articulated with fuselage and another end with shock absorber. Shock absorber rod is articulated with lever. Said retracted-released position locks are made integral and composed of interarticulated flexible link with retainer and pawl with roller arranged to swing from lock open cylinder arranged inside said link. Pawl roller is arranged to contact with release-retracted position grooves made in shock absorber lug.

EFFECT: simple design and reduced weight.

2 cl, 5 dwg

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RU 2 545 239 C1

Authors

Kozlov Mikhail Dmitrievich

Abrashkin Anatolij Il'Ich

Kostjuchenko Aleksandr Pavlovich

Spivak Evgenij Evgen'Evich

Spivak Sergej Evgen'Evich

Egupov Vitalij Dmitrievich

Dates

2015-03-27Published

2014-01-10Filed