首页> 外国专利> Landing arresting system for vertical take-off and landing (VTOL) aerial vehicles, landing and take-off platform for VTOL aerial vehicles and VTOL locking member for aerial vehicles

Landing arresting system for vertical take-off and landing (VTOL) aerial vehicles, landing and take-off platform for VTOL aerial vehicles and VTOL locking member for aerial vehicles

机译:垂直起降(VTOL)飞机的着陆制动系统,VTOL飞机的起降平台和VTOL锁定构件

摘要

A landing arresting system for vertical take-off and landing aerial vehicles. A landing and take-off platform and at least one vertical take-off and landing locking member have a projecting portion arranged at a lower portion of the vehicle. The landing and take-off platform includes a plurality of individually displaceable rolls, arranged substantially in a horizontal direction, and moveable back and forth, such that the projecting portion of the locking member can be entered, retained and released between two adjacent rolls. A landing and take-off platform for vertical take-off and landing aerial vehicles and a vertical take-off and landing locking member for aerial vehicles.
机译:用于垂直起降航空器的着陆制动系统。起降平台和至少一个竖直的起降锁定构件具有布置在车辆下部的突出部分。所述起降平台包括多个可单独移位的辊,所述辊基本上在水平方向上布置并且可前后移动,使得锁定构件的突出部分可进入,保持和释放在两个相邻辊之间。用于垂直起降飞机的起降平台和用于飞行器的垂直起降锁定构件。

著录项

  • 公开/公告号US9499281B2

    专利类型

  • 公开/公告日2016-11-22

    原文格式PDF

  • 申请/专利权人 PER-ERIK CARDELL;KJELL STENBOM;

    申请/专利号US201214408468

  • 发明设计人 PER-ERIK CARDELL;KJELL STENBOM;

    申请日2012-07-05

  • 分类号B64F1/02;B64C25/52;B64C25/68;B64F1;B64F1/12;E01F3;B64C25/32;

  • 国家 US

  • 入库时间 2022-08-21 13:42:07

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