发明名称 航空機の着陸装置用油圧シミーダンパー
摘要 <p>A hydraulic shimmy damper that resolves drawbacks in several known shimmy dampers, such as damping characteristics that are dependent on oil temperature variations. The disclosed shimmy damper includes a hydraulic compensator (40) having an internal fluid volume that is significantly more important than a fluid volume expelled from the body of the shimmy damper when its piston moves fore and aft. The shimmy damper also includes a hydraulic manifold (30) arranged between the body and the hydraulic compensator and defining a transfer channel between chambers in the piston that is connected to the hydraulic compensator. The manifold receives interchangeable hydraulic cartridge-type valves (CV1,RV1;CV2,RV2) for metering the fluid flowing from the chambers to the transfer channel, and allows the fluid to freely enter the chambers from the transfer channel. The present shimmy damper is therefore much less sensitive to oil temperature variation under intense shimmy.</p>
申请公布号 JP5711367(B2) 申请公布日期 2015.04.30
申请号 JP20130520935 申请日期 2011.07.28
申请人 发明人
分类号 F16F9/32;F16F9/20 主分类号 F16F9/32
代理机构 代理人
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