| 摘要 |
FIELD: transport. ^ SUBSTANCE: invention relates to aircraft alighting gear shock absorber. Proposed shock absorber comprises two elements 1 and 2 telescoping to constrict inner chamber filled with working fluid and gas and divided into two chambers 7 and 8 by diaphragm 5. Said diaphragm comprises bypass opening 10 for working fluid to flow from one chamber into another. Bypass opening 10 has gas discharge hole 22 for gas to flow from one chamber into another when alighting gear is in operating conditions. Said hole 22 is displaced in height relative to bypass opening 10 and located above it when alighting gear is in operating conditions. ^ EFFECT: fast return of fluid into rated position corresponding to landing. ^ 5 cl, 3 dwg |
