首页> 外国专利> Impact Resistant Propeller System, Fast Response Electric Propulsion System And Lightweight Vertical Take-Off And Landing Aircraft Using Same

Impact Resistant Propeller System, Fast Response Electric Propulsion System And Lightweight Vertical Take-Off And Landing Aircraft Using Same

机译:耐冲击螺旋桨系统,快速响应电动推进系统以及使用该系统的轻型垂直起降飞机

摘要

An aerial vehicle adapted for vertical takeoff and landing using pivoting thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to takeoff with thrust units providing vertical thrust and then transitioning to a horizontal flight path. An aerial vehicle with pivoting thrust units with propellers, wherein some or all of the propellers are able to be stowed and fully nested during forward flight. An aerial vehicle adapted to withstand impacts upon its propellers. An aerial vehicle able to quickly alter the thrust of its propellers.
机译:一种适用于垂直起飞和降落的飞行器,其使用枢转推力产生元件进行起飞和降落。一种适于以推力单元起飞的航空器,该推力单元提供垂直推力,然后过渡到水平飞行路径。一种具有带有螺旋桨的枢转推力单元的飞行器,其中一些或全部螺旋桨能够在向前飞行期间收起并完全嵌套。一种适于承受螺旋桨撞击的飞行器。能够快速改变螺旋桨推力的飞行器。

著录项

  • 公开/公告号US2016031556A1

    专利类型

  • 公开/公告日2016-02-04

    原文格式PDF

  • 申请/专利权人 JOBY AVIATION INC.;

    申请/专利号US201514662085

  • 发明设计人 JOEBEN BEVIRT;ALEX STOLL;

    申请日2015-03-18

  • 分类号B64C27/37;B64C27/50;B64C27/30;B64C29;B64D27/24;

  • 国家 US

  • 入库时间 2022-08-21 14:33:03

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