发明名称 WINCH SYSTEM FOR VTOL AIRCRAFT
摘要 A winch system includes a cable storage system (34), a drive system (30) and a deployment system to deploy a cable having a hook system attached thereto. A right angle sheave (46) guides the cable between the cable storage system and the drive system. The drive system includes a dual mode transmission that provides high speed capabilities when moderate to no load is being lifted, while also providing high torque for heavy lift operations at low speeds. The deployment system is rated to support a maximum hook load and is mounted to the airframe for pivotable movement about a deployment axis to enable large cable exit angles.
申请公布号 US2010051890(A1) 申请公布日期 2010.03.04
申请号 US20070527612 申请日期 2007.04.19
申请人 LAUDER TIMOTHY F;LOREY JANIECE M;HARRINGTON CHRISTOPHER M 发明人 LAUDER TIMOTHY F.;LOREY JANIECE M.;HARRINGTON CHRISTOPHER M.
分类号 B66D3/00 主分类号 B66D3/00
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