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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Authors
Dates
2015-03-27—Published
2014-01-10—Filed