发明名称 Landing systems for air vehicles
摘要 An air cushioned landing system for an air vehicle comprises an inflatable and deflatable skirt (113) in the form of a tube having inner (101) and outer (100) walls. The inner wall defines a central plenum (116) within the skirt, the skirt including gas pockets (130) arranged to stiffen one or more regions of at least one of the inner (101) and outer (100) walls during deflation of the skirt.
申请公布号 EP2851251(B1) 申请公布日期 2016.11.30
申请号 EP20140185541 申请日期 2014.09.19
申请人 HYBRID AIR VEHICLES LIMITED 发明人 DURHAM, MICHAEL;MACEY, PAUL
分类号 B60V3/08;B60V1/16 主分类号 B60V3/08
代理机构 代理人
主权项
地址