FIELD: transport.
SUBSTANCE: invention relates to aircraft shock absorbers. Proposed system comprises gas filling source and envelopment with inflatable element with its one base attached to aircraft fuselage bottom at its center of gravity. Envelopment with inflatable element is made up of the main inflatable device made up of closed pneumatic-carcass damping loop filled by gas from said source and consisting of top and bottom inflatable torus-like bases connected by inflatable posts and additional inflatable damping device made up of envelopment communicating with ambient medium via bypass holes arranged on outer lateral surface and arranged inside pneumatic carcass damping loop. Top base of the latter features smaller diameter than bottom base and is attached to aircraft fuselage bottom.
EFFECT: lower load in emergent landing.
7 cl, 3 dwg
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